Raytheon Company

United States of America

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        Patent 8,157
        Trademark 231
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        United States 4,984
        World 3,014
        Canada 357
        Europe 33
Owner / Subsidiary
[Owner] Raytheon Company 8,388
Raytheon BBN Technologies Corp. 2
Date
New (last 4 weeks) 24
2025 June (MTD) 11
2025 May 27
2025 April 16
2025 March 19
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IPC Class
H01Q 21/00 - Antenna arrays or systems 170
G06K 9/00 - Methods or arrangements for reading or recognising printed or written characters or for recognising patterns, e.g. fingerprints 139
H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart 137
H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating 137
G01S 13/00 - Systems using the reflection or reradiation of radio waves, e.g. radar systemsAnalogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified 115
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NICE Class
13 - Firearms; explosives 112
09 - Scientific and electric apparatus and instruments 102
12 - Land, air and water vehicles; parts of land vehicles 18
42 - Scientific, technological and industrial services, research and design 15
41 - Education, entertainment, sporting and cultural services 11
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Status
Pending 449
Registered / In Force 7,939
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1.

VIBRATION ISOLATOR WITH TRANSLATION COMPLIANCE

      
Application Number US2024060053
Publication Number 2025/129012
Status In Force
Filing Date 2024-12-13
Publication Date 2025-06-19
Owner RAYTHEON COMPANY (USA)
Inventor Chang, Eric

Abstract

A base isolator for vibration isolation mounting of equipment, includes a pair of rigid (or relatively rigid) tubes, a flexible tube with slots between beams, and a pair of slitted plates. The rigid tubes and the flexible tube may be concentric. The slitted plates couple together ends of the tubes and provide vertical (axial) translational compliance. The flexible tube, which is outside or within the rigid tubes, provides horizontal translational compliance in directions perpendicular to an axis of the isolator. The base isolator, while providing compliance in all three translational directions, provides rotational stiffness, such as for rotational torques about the axis, and more generally for pitch and roll directions.

IPC Classes  ?

  • F16F 15/06 - Suppression of vibrations of non-rotating, e.g. reciprocating, systemsSuppression of vibrations of rotating systems by use of members not moving with the rotating system using elastic means with metal springs
  • F16F 15/073 - Suppression of vibrations of non-rotating, e.g. reciprocating, systemsSuppression of vibrations of rotating systems by use of members not moving with the rotating system using elastic means with metal springs using only leaf springs
  • F16F 3/02 - Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic with springs made of steel or of other material having low internal friction
  • H01Q 1/00 - Details of, or arrangements associated with, antennas
  • H01Q 1/12 - SupportsMounting means
  • H01Q 1/18 - Means for stabilising antennas on an unstable platform
  • G01S 7/481 - Constructional features, e.g. arrangements of optical elements
  • B64D 47/08 - Arrangements of cameras
  • G02B 27/64 - Imaging systems using optical elements for stabilisation of the lateral and angular position of the image

2.

Multi-Spring-Loaded Actuators

      
Application Number 18539254
Status Pending
Filing Date 2023-12-13
First Publication Date 2025-06-19
Owner Raytheon Company (USA)
Inventor
  • Mcvey, Ray E.
  • Foes, Scott R.

Abstract

Multi-spring-loaded actuators can include a rotatable axis arranged to rotate relative to a fixed frame, and multiple loaded springs, each having a rotational potential and being operationally attached to the rotatable axis to cause the rotatable axis to rotate in a first direction (or a second direction) when its rotational potential is released (sequentially). Each loaded spring is associated with a one-time release mechanism operationally coupled to a respective loaded spring to retain the loaded spring with a potential until the one-time release mechanism is spent causing the loaded spring to release. By firing the one-time release mechanism and unloading loaded springs sequentially, a rotatable axis can move a first article relative to a second article, typically in a bi-directional manner.

IPC Classes  ?

  • E05F 1/12 - Mechanisms in the shape of hinges or pivots, operated by springs
  • E05B 15/00 - Other details of locksParts for engagement by bolts of fastening devices
  • E05B 17/00 - Accessories in connection with locks
  • E05B 47/00 - Operating or controlling locks or other fastening devices by electric or magnetic means

3.

VIBRATION ISOLATOR WITH TRANSLATION COMPLIANCE

      
Application Number 18958626
Status Pending
Filing Date 2024-11-25
First Publication Date 2025-06-19
Owner Raytheon Company (USA)
Inventor Chang, Eric E-Lee

Abstract

A base isolator for vibration isolation mounting of equipment, includes a pair of rigid (or relatively rigid) tubes, a flexible tube with slots between beams, and a pair of slitted plates. The rigid tubes and the flexible tube may be concentric. The slitted plates couple together ends of the tubes and provide vertical (axial) translational compliance. The flexible tube, which is outside or within the rigid tubes, provides horizontal translational compliance in directions perpendicular to an axis of the isolator. The base isolator, while providing compliance in all three translational directions, provides rotational stiffness, such as for rotational torques about the axis, and more generally for pitch and roll directions.

IPC Classes  ?

  • B64D 47/08 - Arrangements of cameras
  • F16F 15/073 - Suppression of vibrations of non-rotating, e.g. reciprocating, systemsSuppression of vibrations of rotating systems by use of members not moving with the rotating system using elastic means with metal springs using only leaf springs
  • F16M 11/12 - Means for attachment of apparatusMeans allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction

4.

GROUND MOVING TARGET INDICATOR DETECTION SYSTEM

      
Application Number US2024059382
Publication Number 2025/128574
Status In Force
Filing Date 2024-12-10
Publication Date 2025-06-19
Owner RAYTHEON COMPANY (USA)
Inventor
  • Levin, Ron L.
  • Hushahn, Maximilian Lester-Wilhelm

Abstract

A moving target indicator radar system can include a radar transceiver. The system can further include processing circuitry. The processing circuitry can provide a command to move an antenna beam in an azimuth direction. The processing circuitry can further control the radar transceiver to transmit a series of pulses throughout antenna beam motion such that the series of pulses are assembled into Coherent Processing Intervals (CPIs) and such that for a possible target, sequential sets of CPIs are combined covering at least a 3 dB portion an azimuth beam. The processing circuitry can further detect at least one moving target in at least one CPI. Other apparatuses and methods are also described.

IPC Classes  ?

  • G01S 13/42 - Simultaneous measurement of distance and other coordinates
  • G01S 13/58 - Velocity or trajectory determination systemsSense-of-movement determination systems
  • G01S 13/72 - Radar-tracking systemsAnalogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar

5.

TOPOLOGY- AUGMENTED SYSTEM FOR ALMODEL MISMATCH

      
Application Number US2023077425
Publication Number 2025/128072
Status In Force
Filing Date 2023-10-20
Publication Date 2025-06-19
Owner RAYTHEON COMPANY (USA)
Inventor
  • Sundaramoorthi, Ganesh
  • Salpukas, Michael R.

Abstract

A system and method estimate an uncertainty of an artificial neural network. A topological uncertainty of the artificial neural network is determined by forming a bipartite graph between input and output nodes in a layer of the artificial neural network, and generating a persistence diagram as a function of the bipartite graph. A latent uncertainty of the artificial neural network is then determined, and the uncertainty of the artificial neural network is estimated as a function of the topological uncertainty and the latent uncertainty.

IPC Classes  ?

  • G06N 3/042 - Knowledge-based neural networksLogical representations of neural networks
  • G06N 3/0464 - Convolutional networks [CNN, ConvNet]
  • G06N 3/084 - Backpropagation, e.g. using gradient descent

6.

MULTI-SPRING-LOADED ACTUATORS

      
Application Number US2024053580
Publication Number 2025/128227
Status In Force
Filing Date 2024-10-30
Publication Date 2025-06-19
Owner RAYTHEON COMPANY (USA)
Inventor
  • Mcvey, Ray E.
  • Foes, Scott R.

Abstract

Multi-spring-loaded actuators can include a rotatable axis arranged to rotate relative to a fixed frame, and multiple loaded springs, each having a rotational potential and being operationally attached to the rotatable axis to cause the rotatable axis to rotate in a first direction (or a second direction) when its rotational potential is released (sequentially). Each loaded spring is associated with a one-time release mechanism operationally coupled to a respective loaded spring to retain the loaded spring with a potential until the one-time release mechanism is spent causing the loaded spring to release. By firing the one-time release mechanism and unloading loaded springs sequentially, a rotatable axis can move a first article relative to a second article, typically in a bi-directional manner.

IPC Classes  ?

  • E05F 1/12 - Mechanisms in the shape of hinges or pivots, operated by springs

7.

A WARHEAD AND SEEKER ASSEMBLY

      
Application Number US2024050001
Publication Number 2025/122227
Status In Force
Filing Date 2024-10-04
Publication Date 2025-06-12
Owner RAYTHEON COMPANY (USA)
Inventor
  • Jones, Jaylan S.
  • Koehler, Frederick B.
  • Macdonald, Paul S.
  • Roncone, Ronald L.
  • Leach, John Regis

Abstract

A dual-mode roll/nod gimballed seeker is configured to provide an unobstructed path for a forming-warhead penetrator. A nod assembly includes first and second seekers separately offset from the roll axis whose FOV overlap within a stand-off range to a target. A roll gimbal rotates the dome and nod assembly around the roll axis. A nod gimbal rotates the nod assembly about a nod axis over a nod FOR that causes the seekers to cross the roll axis and obstruct a path along the roll axis. At terminal, the nod gimbal rotates the nod assembly to a nominal nod angle at which the path is unobstructed to detonate the forming warhead and project a penetrator along the path through the dome. This alleviates the need for a precursor charge and saves precious volume in the airframe, which is of particular import for small diameter warheads, in particular those having a diameter of no more than 8 inches.

IPC Classes  ?

  • F42B 10/46 - Streamlined nose conesWindshieldsRadomes
  • F41G 7/00 - Direction control systems for self-propelled missiles
  • F41G 7/22 - Homing guidance systems
  • F42B 12/10 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
  • F42B 15/01 - Arrangements thereon for guidance or control

8.

DUAL-MODE ROLL/NOD GIMBALLED SEEKER FOR A FORMING WARHEAD

      
Application Number 18530942
Status Pending
Filing Date 2023-12-06
First Publication Date 2025-06-12
Owner Raytheon Company (USA)
Inventor
  • Jones, Jaylan S.
  • Koehler, Frederick B.
  • Macdonald, Paul S.
  • Roncone, Ronald L.
  • Leach, John Regis

Abstract

A dual-mode roll/nod gimballed seeker is configured to provide an unobstructed path for a forming-warhead penetrator. A nod assembly includes first and second seekers separately offset from the roll axis whose FOV overlap within a stand-off range to a target. A roll gimbal rotates the dome and nod assembly around the roll axis. A nod gimbal rotates the nod assembly about a nod axis over a nod FOR that causes the seekers to cross the roll axis and obstruct a path along the roll axis. At terminal, the nod gimbal rotates the nod assembly to a nominal nod angle at which the path is unobstructed to detonate the forming warhead and project a penetrator along the path through the dome. This alleviates the need for a precursor charge and saves precious volume in the airframe, which is of particular import for small diameter warheads, in particular those having a diameter of no more than 8 inches.

IPC Classes  ?

  • F41G 7/22 - Homing guidance systems
  • F42B 12/10 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge

9.

GROUND MOVING TARGET INDICATOR DETECTION SYSTEM

      
Application Number 18975911
Status Pending
Filing Date 2024-12-10
First Publication Date 2025-06-12
Owner Raytheon Company (USA)
Inventor
  • Levin, Ron L.
  • Hushahn, Maximilian Lester-Wilhelm

Abstract

A moving target indicator radar system can include a radar transceiver. The system can further include processing circuitry. The processing circuitry can provide a command to move an antenna beam in an azimuth direction. The processing circuitry can further control the radar transceiver to transmit a series of pulses throughout antenna beam motion such that the series of pulses are assembled into Coherent Processing Intervals (CPIs) and such that for a possible target, sequential sets of CPIs are combined covering at least a 3 dB portion an azimuth beam. The processing circuitry can further detect at least one moving target in at least one CPI. Other apparatuses and methods are also described.

IPC Classes  ?

  • G01S 13/524 - Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi
  • G01S 7/282 - Transmitters
  • G01S 7/292 - Extracting wanted echo-signals
  • G01S 7/295 - Means for transforming co-ordinates or for evaluating data, e.g. using computers
  • G01S 13/89 - Radar or analogous systems, specially adapted for specific applications for mapping or imaging

10.

STRUCTURAL ENCLOSURE FOR PROTECTION AGAINST FOREIGN OBJECT DEBRIS AND RESTRAINT OF THERMAL INTERFACE MATERIAL

      
Application Number 18529859
Status Pending
Filing Date 2023-12-05
First Publication Date 2025-06-05
Owner Raytheon Company (USA)
Inventor
  • Chu, Charles
  • Vinttran, Bruce
  • Lopez, Paola V.
  • Lee, Sung H.
  • Burrell, Keith R.
  • Bristol, Andrew J.
  • Miyamoto, Kevin A.

Abstract

A system includes a substrate and an electrical component mounted to the substrate. The system also includes a structural enclosure positioned around lateral edges of the electrical component and mounted to the substrate. The structural enclosure includes raised walls extending away from the substrate and surrounding the electrical component. The raised walls are configured to block foreign object debris from the electrical component. The system further includes a lid connected to the substrate, where the lid covers the electrical component and the structural enclosure. The system also includes a seal positioned between the structural enclosure and the lid, where the seal is configured to be compressed when the lid is connected to the substrate. In addition, the system includes a thermal interface material positioned between and contacting the electrical component and the lid.

IPC Classes  ?

  • H05K 1/18 - Printed circuits structurally associated with non-printed electric components
  • H05K 1/02 - Printed circuits Details
  • H05K 13/04 - Mounting of components

11.

FRAMED GEIGER-MODE LADAR SYSTEM WITH OPTIMAL FRAME RATE SELECTION AND METHOD FOR SELECTION OF OPTIMAL FRAME RATE

      
Application Number 18529838
Status Pending
Filing Date 2023-12-05
First Publication Date 2025-06-05
Owner Raytheon Company (USA)
Inventor Greenberg, Adam Hodge

Abstract

A framed Geiger-mode laser detection and ranging (LADAR) system includes signal processing circuitry configured to select an initial frame rate to maximize sensitivity of a Geiger-mode Avalanche Photodiode (GmAPD) detector. The signal processing circuitry may adjust the initial frame rate to reduce and/or remove system resonances to determine a final (i.e., more-optimal) frame rate. The signal processing circuitry may process LADAR pulse returns using the final frame rate. The initial frame rate may be an initial optimal anti-blocking frame-rate determined from a background rate of the LADAR system, a read-out period of the GmAPD detector, and the Lambert W function. The initial frame rate may be adjusted to remove resonances using an Nth order Farey sequence to determine the final frame rate.

IPC Classes  ?

  • G01S 7/497 - Means for monitoring or calibrating
  • G01S 7/4865 - Time delay measurement, e.g. time-of-flight measurement, time of arrival measurement or determining the exact position of a peak
  • G01S 17/18 - Systems determining position data of a target for measuring distance only using transmission of interrupted, pulse-modulated waves wherein range gates are used

12.

DEPLOYABLE DOORWAY BUMPER

      
Application Number US2024047965
Publication Number 2025/111056
Status In Force
Filing Date 2024-09-23
Publication Date 2025-05-30
Owner RAYTHEON COMPANY (USA)
Inventor
  • Adams, Richard
  • Tracy, Ryan
  • Strickler, James

Abstract

A doorway is provided that includes a door frame, a door and a bumper. The door frame includes a passage, a header, a first jamb and a second jamb. The passage extends laterally between the first jamb and the second jamb. The passage extends vertically along the first jamb and the second jamb to the header. The door is configured to move between a closed position and an open position. The door closes the passage in the closed position. The door opens the passage in the open position. The bumper is configured to move between a deployed position and a stowed position. The bumper is disposed in the passage and covers a portion of the door frame in the deployed position.

IPC Classes  ?

  • E06B 7/28 - Other arrangements on doors or windows, e.g. door-plates, windows adapted to carry plants, hooks for window cleaners

13.

DIGITAL PIXEL ARCHITECTURE SUPPORTING RE-USE OF COMPONENTS FOR IN-PIXEL ANALOG-TO-DIGITAL CONVERSION OF INTEGRATION RESIDUE

      
Application Number 18520258
Status Pending
Filing Date 2023-11-27
First Publication Date 2025-05-29
Owner Raytheon Company (USA)
Inventor
  • Beuville, Eric J.
  • Cantrell, Joshua J.
  • Harris, Micky R.

Abstract

A system includes a focal plane array having multiple pixel circuit elements. Each pixel circuit element includes a photodetector configured to generate an electrical current based on received illumination. Each pixel circuit element also includes an integration capacitor configured to be charged by the electrical current and generate a capacitor voltage and to be discharged. Each pixel circuit element further includes a comparator configured to generate pulses in a digital output based on the capacitor voltage of the integration capacitor. In addition, each pixel circuit element includes a counter configured to (i) in a first configuration, count the pulses in the digital output of the comparator during a sampling period and (ii) in a second configuration, count pulses in a clock signal during a residue digitization period. A counted number of pulses in the clock signal is indicative of a residue stored on the integration capacitor at an end of the sampling period.

IPC Classes  ?

  • H04N 25/772 - Pixel circuitry, e.g. memories, A/D converters, pixel amplifiers, shared circuits or shared components comprising A/D, V/T, V/F, I/T or I/F converters
  • H03K 5/24 - Circuits having more than one input and one output for comparing pulses or pulse trains with each other according to input signal characteristics, e.g. slope, integral the characteristic being amplitude
  • H03K 21/02 - Input circuits
  • H03M 1/56 - Input signal compared with linear ramp

14.

SCALABLE ROUTING TOPOLOGIES THAT ENABLE INCREASED LOADS ON SINGLE-ENDED OR DIFFERENTIAL CHANNELS

      
Application Number 18520181
Status Pending
Filing Date 2023-11-27
First Publication Date 2025-05-29
Owner Raytheon Company (USA)
Inventor
  • Tran, Thanh Thien
  • Mckinney, Colin Michael
  • Henseler, Glenn D.

Abstract

A system includes a driver and multiple loads configured to communicate with the driver. The system also includes a primary signal line configured to transport one or more electrical signals between the driver and the multiple loads. The system further includes multiple branch signal lines each configured to transport at least one of the one or more electrical signals and each coupled to one or more of the multiple loads. In addition, the system includes a splitter coupling the primary signal line and the branch signal lines. The primary signal line has a first characteristic impedance, and the branch signal lines collectively have a second characteristic impedance that matches or substantially matches the first characteristic impedance. In some cases, the primary signal line and the branch signal lines may have equal or substantially equal trace widths.

IPC Classes  ?

15.

UNIFORM THIN FILM DEPOSITION FOR POLY-P-XYLYLENE

      
Application Number 19025048
Status Pending
Filing Date 2025-01-16
First Publication Date 2025-05-29
Owner Raytheon Company (USA)
Inventor
  • Rickman, Amanda
  • Smith, James R.

Abstract

Embodiments of the invention are directed to a deposition chamber for forming a poly-para-xylylene film. A non-limiting example of the deposition chamber includes a chamber body, an inlet coupling the chamber body to a furnace, and an outlet coupling the chamber body to a vacuum pump. The deposition chamber includes at least one heating element arranged on a surface of the chamber body. The heating element is configured to raise an internal temperature of the deposition chamber body to a substantially uniform internal temperature across an entire internal volume of the chamber body.

IPC Classes  ?

  • B05D 1/00 - Processes for applying liquids or other fluent materials
  • C23C 16/46 - Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for heating the substrate

16.

DEVICE FOR OPTIMAL SATELLITE EFFECTS DELIVERY VIA REVERSE TIME HEAT ISOMORPHISM

      
Application Number 19036748
Status Pending
Filing Date 2025-01-24
First Publication Date 2025-05-29
Owner Raytheon Company (USA)
Inventor
  • Imhoff, Scott Allen
  • Hoppes, Brianne R.
  • Teter, Marcus A.
  • Hall, Kendy

Abstract

Apparatus, computer-readable medium, and method for optimal delivery of one or more satellite effects via reverse time heat equation isomorphism including constructing a generalized formulation of the heat equation corresponding to a commander's intent for delivery of the one or more satellite effects, performing a separation of variables to decouple a plurality of variables into a plurality of corresponding separated equations, solving the plurality of separated equations to produce candidate solutions, applying boundary conditions to each candidate solution, filtering the candidate solutions to mitigate ill-posedness of solving the inverse of the heat equation, assessing formal differences between the candidate solutions and the inverse of the heat equation, and generating an optimized schedule of the one or more satellite effects based on the assessment of the formal differences of the candidate solutions.

IPC Classes  ?

  • B64G 1/10 - Artificial satellitesSystems of such satellitesInterplanetary vehicles
  • G06F 17/13 - Differential equations

17.

SELF-CALIBRATING PHASE INTERFEROMETRY USING RANDOM FOREST REGRESSION, NEURAL NETWORK, OR OTHER MACHINE LEARNING MODEL

      
Application Number 18512954
Status Pending
Filing Date 2023-11-17
First Publication Date 2025-05-22
Owner Raytheon Company (USA)
Inventor
  • Nardell, Carl A.
  • Cronin, Brian A.

Abstract

An apparatus includes multiple antennas each configured to receive one or more incoming signals. The apparatus also includes at least one processing device configured to receive antenna measurements associated with the one or more incoming signals, where the antenna measurements include phase measurements associated with the one or more incoming signals. The at least one processing device is also configured to process the antenna measurements using a trained machine learning model to generate a prediction of an angle of arrival associated with the one or more incoming signals. The trained machine learning model is trained to generate the prediction of the angle of arrival even while compensating for phase errors affecting the antenna measurements.

IPC Classes  ?

18.

INTEGRALLY FORMED HIGH-G SHOCK METAL ISOLATOR IN A PROJECTILE

      
Application Number 18513009
Status Pending
Filing Date 2023-11-17
First Publication Date 2025-05-22
Owner Raytheon Company (USA)
Inventor
  • Vo, Peter H.
  • Esplin, Roger C.
  • Byrne, Robert P.

Abstract

A projectile is integrally formed with a high-G shock isolator to isolate a protected device. The isolator includes a pattern of cut-outs formed around a circumference of a metal casing that defines flexures and supports and coupling paths that zigzag therethrough. Symmetry about the longitudinal axis of the projectile defines springs that are colinear with the principal axes of the projectile with a resonant frequency selected to attenuate shock inputs to levels acceptable to the protected device. The isolator is suitably provided with forward and aft stops to ensure isolator survivability. The aft stops are positioned in the cut-outs to prevent the flexures compressing beyond the yield strength of the casing material. The forward stop includes a structure rigidly attached behind the isolator that extends forward to engage a forward-facing surface of the isolator to prevent the flexures from stretching beyond the yield strength of the casing material.

IPC Classes  ?

  • F42B 12/76 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
  • F16F 15/02 - Suppression of vibrations of non-rotating, e.g. reciprocating, systemsSuppression of vibrations of rotating systems by use of members not moving with the rotating system
  • F16F 15/06 - Suppression of vibrations of non-rotating, e.g. reciprocating, systemsSuppression of vibrations of rotating systems by use of members not moving with the rotating system using elastic means with metal springs

19.

COMBINED HIGH ENERGY LASER AUTO-ALIGNMENT SYSTEM, JITTER CORRECTOR, AND BURN-THROUGH DETECTOR SYSTEM

      
Application Number 18517306
Status Pending
Filing Date 2023-11-22
First Publication Date 2025-05-22
Owner RAYTHEON COMPANY (USA)
Inventor
  • Lavine, Jason R.
  • Skoyles, Liam
  • Holten, Roger

Abstract

A beam director system includes a high-energy laser (HEL) beam source for an HEL beam, a primary mirror disposed along an optical path downstream of the HEL beam source, output optics downstream of the primary mirror, an auto-alignment system associated with the HEL beam source, a jitter correction system downstream of the HEL beam source and upstream of the primary mirror, and a burn-through detector associated with the primary mirror.

IPC Classes  ?

  • F41H 13/00 - Means of attack or defence not otherwise provided for
  • G02B 26/08 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
  • H01S 3/00 - Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range

20.

ENHANCED BROADBAND RING RESONATOR FOR IMPROVED SPECTRAL SUPPRESSION

      
Application Number US2024047663
Publication Number 2025/106159
Status In Force
Filing Date 2024-09-20
Publication Date 2025-05-22
Owner RAYTHEON COMPANY (USA)
Inventor
  • Cathrea, Cory William
  • Dewitt, Ryan D.

Abstract

A broadband ring resonator (300, 400, 500, 600, 601) including a substrate, a conductive trace on the substrate comprising a first end and a second end, wherein the conductive trace encloses an interior region except for a gap between the first end and the second end, and at least one radial stub (301, 401, 403, 501, 503, 505, 603, 605, 607, 609, 611, 613) integrated into the conductive trace and a method (700) of enhancing a bandwidth of a split ring resonator including acquiring a substrate, forming a conductive trace on the substrate comprising a first end and a second end, wherein the conductive trace encloses an interior region except for a gap between the first end and the second end, and integrating at least one radial stub (301, 401, 403, 501, 503, 505, 603, 605, 607, 609, 611, 613) into the conductive trace.

IPC Classes  ?

21.

ENHANCED BROADBAND RING RESONATOR FOR IMPROVED SPECTRAL SUPPRESSION

      
Application Number 18512152
Status Pending
Filing Date 2023-11-17
First Publication Date 2025-05-22
Owner Raytheon Company (USA)
Inventor
  • Cathrea, Cory William
  • Dewitt, Ryan D.

Abstract

A broadband ring resonator including a substrate, a conductive trace on the substrate comprising a first end and a second end, wherein the conductive trace encloses an interior region except for a gap between the first end and the second end, and at least one radial stub integrated into the conductive trace and a method of enhancing a bandwidth of a split ring resonator including acquiring a substrate, forming a conductive trace on the substrate comprising a first end and a second end, wherein the conductive trace encloses an interior region except for a gap between the first end and the second end, and integrating at least one radial stub into the conductive trace.

IPC Classes  ?

22.

DIRECTION-FINDING AMBIGUITY RESOLUTION IN LONG BASELINE INTERFEROMETERS USING RANDOM FOREST REGRESSION

      
Application Number 18512900
Status Pending
Filing Date 2023-11-17
First Publication Date 2025-05-22
Owner Raytheon Company (USA)
Inventor Nardell, Carl A.

Abstract

An apparatus includes multiple antennas each configured to receive one or more incoming signals. The apparatus also includes at least one processing device configured to receive antenna measurements associated with the one or more incoming signals, where the antenna measurements include phase measurements associated with the one or more incoming signals. The at least one processing device is also configured to process the antenna measurements using multiple decision trees of a random forest regressor, where the decision trees are configured to generate multiple initial predictions of an angle of arrival associated with the one or more incoming signals. In addition, the at least one processing device is configured to combine the initial predictions in order to generate a final prediction of the angle of arrival associated with the one or more incoming signals.

IPC Classes  ?

  • G01S 3/48 - Systems for determining direction or deviation from predetermined direction using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured
  • G01S 3/04 - Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves Details

23.

DEPLOYABLE DOORWAY BUMPER

      
Application Number 18517982
Status Pending
Filing Date 2023-11-22
First Publication Date 2025-05-22
Owner Raytheon Company (USA)
Inventor
  • Adams, Richard J.
  • Tracy, Ryan D.
  • Strickler, James

Abstract

A doorway is provided that includes a door frame, a door and a bumper. The door frame includes a passage, a header, a first jamb and a second jamb. The passage extends laterally between the first jamb and the second jamb. The passage extends vertically along the first jamb and the second jamb to the header. The door is configured to move between a closed position and an open position. The door closes the passage in the closed position. The door opens the passage in the open position. The bumper is configured to move between a deployed position and a stowed position. The bumper is disposed in the passage and covers a portion of the door frame in the deployed position.

IPC Classes  ?

  • E05F 7/00 - Accessories for wings not provided for in other groups of this subclass

24.

INTEGRALLY FORMED HIGH-G SHOCK METAL ISOLATOR IN A PROJECTILE

      
Application Number US2024047054
Publication Number 2025/106154
Status In Force
Filing Date 2024-09-17
Publication Date 2025-05-22
Owner RAYTHEON COMPANY (USA)
Inventor
  • Vo, Peter H.
  • Esplin, Roger C.
  • Byrne, Robert P.

Abstract

A projectile is integrally formed with a high-G shock isolator to isolate a protected device. The isolator includes a pattern of cut-outs formed around a circumference of a metal casing that defines flexures and supports and coupling paths that zigzag therethrough. Symmetry about the longitudinal axis of the projectile defines springs that are colinear with the principal axes of the projectile with a resonant frequency selected to attenuate shock inputs to levels acceptable to the protected device. The isolator is suitably provided with forward and aft stops to ensure isolator survivability. The aft stops are positioned in the cut-outs to prevent the flexures compressing beyond the yield strength of the casing material. The forward stop includes a structure rigidly attached behind the isolator that extends forward to engage a forward- facing surface of the isolator to prevent the flexures from stretching beyond the yield strength of the casing material.

IPC Classes  ?

  • F16F 1/02 - Springs made of steel or other material having low internal frictionWound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant
  • F42B 15/36 - Means for interconnecting rocket-motor and body sectionMulti-stage connectorsDisconnecting means

25.

Dynamically stabilized hybrid energy storage machinery for power system experiencing torsional oscillations

      
Application Number 18602913
Grant Number 12308782
Status In Force
Filing Date 2024-03-12
First Publication Date 2025-05-20
Grant Date 2025-05-20
Owner Raytheon Company (USA)
Inventor Kuznetsov, Stephen B.

Abstract

A hybrid asynchronous induction machine includes a stator disposed in a stator housing, the stator comprising an input winding for a polyphase input signal, a primary output winding and a secondary output winding. The machine also includes a rotor having a shaft connected to a flywheel of an energy storage unit. The rotor comprises a primary rotor winding for a polyphase AC excitation signal and a secondary rotor winding for bidirectional power flow. The hybrid asynchronous induction machine is further configured to receive a compensation signal for cancelling low-frequency electrical resonances.

IPC Classes  ?

  • H02P 9/10 - Control effected upon generator excitation circuit to reduce harmful effects of overloads or transients, e.g. sudden application of load, sudden removal of load, sudden change of load
  • H02P 103/10 - Controlling arrangements characterised by the type of generator of the asynchronous type

26.

Dynamic stabilizer for hybrid energy storage machinery with power system experiencing torsional oscillations

      
Application Number 18602889
Grant Number 12308781
Status In Force
Filing Date 2024-03-12
First Publication Date 2025-05-20
Grant Date 2025-05-20
Owner Raytheon Company (USA)
Inventor Kuznetsov, Stephen B.

Abstract

A method of stabilizing a power supply includes, receiving, at a controller connected to an alternating current (AC) excitation source, a plurality of system inputs. The method further includes obtaining a harmonic spectrum of the load current on a hybrid asynchronous induction machine, determining based on the harmonic spectrum, a first low frequency spectrum of the load current with a greatest magnitude of oscillations. Additionally, the method includes controlling the AC excitation source to generate a first compensation signal and providing the first compensation signal to the hybrid asynchronous induction machine.

IPC Classes  ?

  • H02P 9/00 - Arrangements for controlling electric generators for the purpose of obtaining a desired output
  • H02P 9/10 - Control effected upon generator excitation circuit to reduce harmful effects of overloads or transients, e.g. sudden application of load, sudden removal of load, sudden change of load
  • H02P 27/06 - Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using DC to AC converters or inverters

27.

VIDEO PORT AUTHENTICATION FOR MULTI-LEVEL SECURITY DEVICES

      
Application Number 18941619
Status Pending
Filing Date 2024-11-08
First Publication Date 2025-05-15
Owner Raytheon Company (USA)
Inventor Solorzano, Paul R.

Abstract

A video receiver receives a security level of a video source. The security level is stored in a blanking region of a video transmission. The video receiver compares the security level of the video transmission with a security level stored in the video receiver. The video transmission is processed as a function of the comparison of the security level of the video transmission with the security level of the video receiver.

IPC Classes  ?

  • H04N 7/083 - Systems for the simultaneous or sequential transmission of more than one television signal, e.g. additional information signals, the signals occupying wholly or partially the same frequency band with signal insertion during the vertical and the horizontal blanking interval
  • H04N 5/067 - Arrangements or circuits at the transmitter end

28.

COMPACT OPTICAL BEAM COMBINER PACKAGE

      
Application Number US2024044037
Publication Number 2025/101249
Status In Force
Filing Date 2024-08-27
Publication Date 2025-05-15
Owner RAYTHEON COMPANY (USA)
Inventor
  • Dichiara, Anthony D.
  • Mccormick, David R.
  • Thielen, Dustin R.

Abstract

An apparatus includes a dichroic combiner array (106) configured to combine multiple input optical beams (104) and generate an output optical beam (108). The dichroic combiner array includes multiple mirrors (112) and multiple dichroic filters (110). A first mirror is configured to reflect a first input optical beam towards a first dichroic filter, which is configured to combine the first input optical beam and a second input optical beam. A second mirror is configured to reflect a combined optical beam from the first dichroic filter to a second dichroic filter. A last dichroic filter is configured to generate the output optical beam. The apparatus also includes a beam dump array having multiple beam dumps (116) configured to terminate stray optical energy. The stray optical energy includes at least one of: (i) optical energy reflecting from at least one of the dichroic filters and (ii) optical energy transmitted through at least one of the dichroic filters.

IPC Classes  ?

  • G02B 27/14 - Beam splitting or combining systems operating by reflection only
  • G02B 5/00 - Optical elements other than lenses

29.

AEROSOL-JETTABLE SILVER NANOPARTICLE-BASED CONVERTIBLE INK

      
Application Number US2024054904
Publication Number 2025/101737
Status In Force
Filing Date 2024-11-07
Publication Date 2025-05-15
Owner
  • RAYTHEON COMPANY (USA)
  • THE UNIVERSITY OF MASSACHUSETTS (USA)
Inventor
  • Alexander, Gavin
  • Luce, Andrew M.
  • Areias, Christopher
  • Armiento, Craig Alfred
  • Trulli, Susan C.
  • Akyurtlu, Alkim
  • Ranasingha, Oshada K.

Abstract

A method of forming a convertible ink. The method includes: performing a polyol process with a metal salt, a capping agent and a solvent to produce encapsulated nanospheres in a first aqueous solution; reducing the amount of capping agent in the solution. The capping agent can be reduced by: adding solvent soluble with the capping agent and agitating the mixture via centrifugation to form a supernatant and a precipitate that includes the encapsulated nanospheres; removing the supernatant; adding a second solvent to the precipitate to form a second solution; agitating the second solution to form a second supernatant and a precipitate that includes the encapsulated nanospheres; and removing the second supernatant.

IPC Classes  ?

30.

VIDEO PORT AUTHENTICATION FOR MULTI-LEVEL SECURITY DEVICES

      
Application Number US2024055105
Publication Number 2025/101887
Status In Force
Filing Date 2024-11-08
Publication Date 2025-05-15
Owner RAYTHEON COMPANY (USA)
Inventor Solorzano, Paul R.

Abstract

A video receiver receives a security level of a video source. The security level is stored in a blanking region of a video transmission. The video receiver compares the security level of the video transmission with a security level stored in the video receiver. The video transmission is processed as a function of the comparison of the security level of the video transmission with the security level of the video receiver.

IPC Classes  ?

  • H04N 21/4363 - Adapting the video stream to a specific local network, e.g. a Bluetooth® network
  • H04L 9/40 - Network security protocols
  • H04N 21/4367 - Establishing a secure communication between the client and a peripheral device or smart card
  • H04N 21/44 - Processing of video elementary streams, e.g. splicing a video clip retrieved from local storage with an incoming video stream or rendering scenes according to encoded video stream scene graphs
  • H04N 21/4627 - Rights management
  • H04L 9/12 - Transmitting and receiving encryption devices synchronised or initially set up in a particular manner
  • H04N 7/16 - Analogue secrecy systemsAnalogue subscription systems
  • G06F 21/84 - Protecting input, output or interconnection devices output devices, e.g. displays or monitors
  • H04N 21/454 - Content filtering, e.g. blocking advertisements
  • H04N 21/258 - Client or end-user data management, e.g. managing client capabilities, user preferences or demographics or processing of multiple end-users preferences to derive collaborative data

31.

INTEGRATED CABLE PACKAGING, DEPLOYMENT AND STRUMMING MITIGATION SYSTEM

      
Application Number 18500255
Status Pending
Filing Date 2023-11-02
First Publication Date 2025-05-08
Owner Raytheon Company (USA)
Inventor Misulia, Joseph M.

Abstract

A cable package for a line array and a method thereof including a first sheet of material, a cable wound in a serpentine shape, where a portion of the cable contacts the first sheet of material, and a second sheet of material attached to the cable and areas of the first sheet of material not occupied by the cable, wherein the areas of the second sheet of material attached to the first sheet of material not occupied by the cable comprises scoring lines to enable separation under tension to form a plurality of strumming mitigation fairings, and wherein the cable with scoring lines in the areas of the second sheet of material attached to the first sheet of material not occupied by the cable is folded onto itself.

IPC Classes  ?

  • B65D 75/30 - Articles or materials enclosed between two opposed sheets or blanks having their margins united, e.g. by pressure-sensitive adhesive, crimping, heat-sealing, or welding
  • B65B 5/04 - Packaging single articles
  • B65B 61/02 - Auxiliary devices, not otherwise provided for, for operating on sheets, blanks, webs, binding material, containers or packages for perforating, scoring, or applying code or date marks on material prior to packaging
  • B65D 75/58 - Opening or contents-removing devices added or incorporated during package manufacture
  • B65D 85/67 - Containers, packaging elements or packages, specially adapted for particular articles or materials for web or tape-like material
  • F16F 7/10 - Vibration-dampersShock-absorbers using inertia effect
  • G01V 1/18 - Receiving elements, e.g. seismometer, geophone
  • G01V 1/38 - SeismologySeismic or acoustic prospecting or detecting specially adapted for water-covered areas

32.

MOSAIC FOCAL PLANE ARRAY

      
Application Number 19015141
Status Pending
Filing Date 2025-01-09
First Publication Date 2025-05-08
Owner Raytheon Company (USA)
Inventor
  • Gulbransen, David J.
  • Kilcoyne, Sean P.
  • Miller, Eric R.
  • Chambers, Matthew D.
  • Beuville, Eric J.
  • Gin, Andrew E.
  • Kennedy, Adam M.

Abstract

A focal plane array includes a mosaic integrated circuit device having a plurality of discrete integrated circuit tiles mounted on a motherboard. The focal plane array includes an optically continuous detector array electrically connected to the mosaic integrated circuit device with an interposer disposed therebetween. The interposer is configured to adjust a pitch of the continuous detector array to match a pitch of each of the plurality of discrete integrated circuit tiles so that the optical gaps between each of the plurality of integrated circuit tiles on the motherboard are minimized and the detector array is optically continuous, having high yield over the large format focal plane array.

IPC Classes  ?

  • H10F 39/00 - Integrated devices, or assemblies of multiple devices, comprising at least one element covered by group , e.g. radiation detectors comprising photodiode arrays
  • H01L 21/66 - Testing or measuring during manufacture or treatment
  • H01L 23/00 - Details of semiconductor or other solid state devices
  • H10F 39/18 - Complementary metal-oxide-semiconductor [CMOS] image sensorsPhotodiode array image sensors

33.

INTEGRATED CABLE PACKAGING, DEPLOYMENT AND STRUMMING MITIGATION SYSTEM

      
Application Number US2024053654
Publication Number 2025/096607
Status In Force
Filing Date 2024-10-30
Publication Date 2025-05-08
Owner RAYTHEON COMPANY (USA)
Inventor Misulia, Joseph M.

Abstract

A cable package for a line array and a method thereof including a first sheet of material, a cable wound in a serpentine shape, where a portion of the cable contacts the first sheet of material, and a second sheet of material attached to the cable and areas of the first sheet of material not occupied by the cable, wherein the areas of the second sheet of material attached to the first sheet of material not occupied by the cable comprises scoring lines to enable separation under tension to form a plurality of strumming mitigation fairings, and wherein the cable with scoring lines in the areas of the second sheet of material attached to the first sheet of material not occupied by the cable is folded onto itself.

IPC Classes  ?

  • G01V 1/18 - Receiving elements, e.g. seismometer, geophone
  • G01V 1/20 - Arrangements of receiving elements, e.g. geophone pattern
  • G01V 1/38 - SeismologySeismic or acoustic prospecting or detecting specially adapted for water-covered areas
  • B63B 21/66 - Equipment specially adapted for towing underwater objects or vessels, e.g. fairings for tow-cables

34.

AUTOMATED CONVERSION BETWEEN BEHAVIORAL TESTS AND INTEGRATION TESTS FOR SOFTWARE TESTING

      
Application Number US2024054400
Publication Number 2025/097128
Status In Force
Filing Date 2024-11-04
Publication Date 2025-05-08
Owner RAYTHEON COMPANY (USA)
Inventor Churchill, Benjamin Christopher

Abstract

A method includes performing (302) one or more behavioral tests (114) of software code. The method also includes, during the one or more behavioral tests, recording (304) interactions associated with the software code. The interactions include simulated incoming interactions to the software code and actual outgoing interactions from the software code. The method further includes converting (306) the interactions into contracts (604), where each contract includes information defining how at least one interaction involving the software code occurs. In addition, the method includes generating (308) one or more integration tests (116) for the software code based on the contracts. The one or more behavioral tests are configured to test functional behaviors of the software code. The one or more integration tests are configured to test integration of the software code with at least one external component.

IPC Classes  ?

35.

AUTOMATED CONVERSION BETWEEN BEHAVIORAL TESTS AND INTEGRATION TESTS FOR SOFTWARE TESTING

      
Application Number 18501599
Status Pending
Filing Date 2023-11-03
First Publication Date 2025-05-08
Owner Raytheon Company (USA)
Inventor Churchill, Benjamin Christopher

Abstract

A method includes performing one or more behavioral tests of software code. The method also includes, during the one or more behavioral tests, recording interactions associated with the software code. The interactions include simulated incoming interactions to the software code and actual outgoing interactions from the software code. The method further includes converting the interactions into contracts, where each contract includes information defining how at least one interaction involving the software code occurs. In addition, the method includes generating one or more integration tests for the software code based on the contracts. The one or more behavioral tests are configured to test functional behaviors of the software code. The one or more integration tests are configured to test integration of the software code with at least one external component.

IPC Classes  ?

  • G06F 11/36 - Prevention of errors by analysis, debugging or testing of software

36.

AEROSOL-JETTABLE SILVER NANOPARTICLE-BASED CONVERTIBLE INK

      
Application Number 18504518
Status Pending
Filing Date 2023-11-08
First Publication Date 2025-05-08
Owner
  • Raytheon Company (USA)
  • The University of Massachusetts (USA)
Inventor
  • Alexander, Gavin
  • Luce, Andrew M.
  • Areias, Christopher
  • Armiento, Craig Alfred
  • Trulli, Susan C.
  • Akyurtlu, Alkim
  • Ranasingha, Oshada K.

Abstract

A method of forming a convertible ink. The method includes: performing a polyol process with a metal salt, a capping agent and a solvent to produce encapsulated nanospheres in a first aqueous solution; reducing the amount of capping agent in the solution. The capping agent can be reduced by: adding solvent soluble with the capping agent and agitating the mixture via centrifugation to form a supernatant and a precipitate that includes the encapsulated nanospheres; removing the supernatant; adding a second solvent to the precipitate to form a second solution; agitating the second solution to form a second supernatant and a precipitate that includes the encapsulated nanospheres; and removing the second supernatant.

IPC Classes  ?

  • C09D 11/38 - Inkjet printing inks characterised by non-macromolecular additives other than solvents, pigments or dyes
  • C09D 11/52 - Electrically conductive inks

37.

COMPACT OPTICAL BEAM COMBINER PACKAGE

      
Application Number 18816799
Status Pending
Filing Date 2024-08-27
First Publication Date 2025-05-08
Owner Raytheon Company (USA)
Inventor
  • Dichiara, Anthony D.
  • Mccormick, David R.
  • Thielen, Dustin R.

Abstract

An apparatus includes a dichroic combiner array configured to combine multiple input optical beams and generate an output optical beam. The dichroic combiner array includes multiple mirrors and multiple dichroic filters. A first mirror is configured to reflect a first input optical beam towards a first dichroic filter, which is configured to combine the first input optical beam and a second input optical beam. A second mirror is configured to reflect a combined optical beam from the first dichroic filter to a second dichroic filter. A last dichroic filter is configured to generate the output optical beam. The apparatus also includes a beam dump array having multiple beam dumps configured to terminate stray optical energy. The stray optical energy includes at least one of: (i) optical energy reflecting from at least one of the dichroic filters and (ii) optical energy transmitted through at least one of the dichroic filters.

IPC Classes  ?

  • G02B 6/293 - Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means

38.

TANDEM CHARGE FOR UNDERWATER TARGETS

      
Application Number 18498587
Status Pending
Filing Date 2023-10-31
First Publication Date 2025-05-01
Owner Raytheon Company (USA)
Inventor Sadler, Coulton T.

Abstract

A tandem charge for prosecution of underwater targets includes both a precursor charge (PC) and a follow through charge (FTC) oriented within and along an axis of a charge casing with the FTC positioned in front of the precursor charge. The precursor charge includes an explosive charge and a liner configured such that upon detonation of the explosive charge the liner forms an annular explosively formed penetrator (EFP) that is projected along the axis and passes around the FTC to cut a first hole in an outer surface of the target. The FTC is configured to be carried through the first hole in the outer surface of the target by the flow of water therethrough for detonation on the other side of the outer surface of the target, perhaps forming a second hole in an inner surface of the target.

IPC Classes  ?

  • F42B 12/18 - Hollow charges in tandem arrangement
  • F42B 1/028 - Shaped or hollow charges characterised by the form of the liner

39.

BEAM COMBINING GRATING WITH INTEGRATED APODIZER

      
Application Number 18491392
Status Pending
Filing Date 2023-10-20
First Publication Date 2025-04-24
Owner Raytheon Company (USA)
Inventor
  • Mitchell, Bradley A.
  • Orrell, Hannan S.

Abstract

An apparatus includes an optical surface configured to receive multiple input optical beams. The optical surface includes a grating configured to diffract first portions of the input optical beams in a first direction to form a combined optical beam. The grating is also configured to reflect second portions of the input optical beams in a second direction. The optical surface also includes a reflective surface at least partially surrounding the grating. The reflective surface is configured to reflect third portions of the input optical beams in the second direction.

IPC Classes  ?

40.

GATE REDUCTION AT DISTRIBUTED EDGE DEVICES OR OTHER DEVICES

      
Application Number 18816736
Status Pending
Filing Date 2024-08-27
First Publication Date 2025-04-24
Owner Raytheon Company (USA)
Inventor
  • Hershey, Paul C.
  • Prasad, Vikram A.
  • Teter, Marcus A.
  • Hoppes, Brianne R.
  • Bahns, Michael T.

Abstract

A method includes obtaining, using at least one processing device of an electronic device, information defining a combinatorial logic gate design for a combinatorial logic circuit. The method also includes generating, using the at least one processing device, one or more polynomials representing operation of the combinatorial logic gate design. The method further includes mapping, using the at least one processing device, the one or more polynomials to one or more quantum polynomials, where each quantum polynomial has terms that are orthonormal. In addition, the method includes generating, using the at least one processing device, a quantum gate logic design based on the one or more quantum polynomials, where the quantum gate logic design is functionally equivalent to or better than the combinatorial logic gate design for the combinatorial logic circuit.

IPC Classes  ?

  • G06N 10/20 - Models of quantum computing, e.g. quantum circuits or universal quantum computers

41.

BEAM COMBINING GRATING WITH INTEGRATED APODIZER

      
Application Number US2024039850
Publication Number 2025/085144
Status In Force
Filing Date 2024-07-26
Publication Date 2025-04-24
Owner RAYTHEON COMPANY (USA)
Inventor
  • Mitchell, Bradley A.
  • Orrell, Hannan S.

Abstract

An apparatus (100) includes an optical surface (106) configured to receive multiple input optical beams (304). The optical surface includes a grating (202) configured to diffract first portions of the input optical beams in a first direction to form a combined optical beam (308). The grating is also configured to reflect second portions of the input optical beams in a second direction. The optical surface also includes a reflective surface (204) at least partially surrounding the grating. The reflective surface is configured to reflect third portions of the input optical beams in the second direction.

IPC Classes  ?

  • G02B 5/18 - Diffracting gratings
  • G02B 6/293 - Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means
  • G02B 27/09 - Beam shaping, e.g. changing the cross-sectioned area, not otherwise provided for
  • G02B 27/10 - Beam splitting or combining systems

42.

COURSE OF ACTION SUPPORT TECHNOLOGY ARCHITECTURES

      
Application Number 18487755
Status Pending
Filing Date 2023-10-16
First Publication Date 2025-04-17
Owner Raytheon Company (USA)
Inventor
  • Hershey, Paul C.
  • Taylor, Charles L.
  • Morrison, David
  • Coston, Jennifer N.
  • Coston, Rachel D.

Abstract

Systems, devices, methods, and computer-readable media for course of action (COA) analysis and execution. A method can include receiving COA data, coordinating, by an orchestrator service, simulation of performing COAs associated with the COA data, generating a graphical view of the simulation of the COAs including scores associated with each COA, implementing a COA of the COAs selected by the commander, receiving, from multiple applications information regarding a state of executing the COA, and providing a graphical view of the state of executing the COA including an overall map of a geographical region in which the COA is implemented, the graphical view including a dynamic location of the threat and threat mitigation activities, and a dynamic view of the LOS updated as the COA is implemented.

IPC Classes  ?

  • G06N 3/006 - Artificial life, i.e. computing arrangements simulating life based on simulated virtual individual or collective life forms, e.g. social simulations or particle swarm optimisation [PSO]

43.

PRODUCT IDENTIFICATION AND TRACKING SYSTEMS AND METHODS

      
Application Number US2024050376
Publication Number 2025/080582
Status In Force
Filing Date 2024-10-08
Publication Date 2025-04-17
Owner RAYTHEON COMPANY (USA)
Inventor
  • Campinell, Brian F.
  • Cavalcanti, Paulo Meireles
  • Di Carlo, Robert

Abstract

In accordance with at least one aspect of this disclosure, a product identification and tracking interface system includes an interface unit. The interface unit includes an input/output configured and adapted to be coupled to at least one of a tracking system or an identification system, a memory configured to store instructions, and a processor disposed in communication with said memory. The processor upon execution of the instructions is configured to receive a trigger command from a tracking system, send a read command to an identification system, receive a respective identifier from the identification system, package the respective identifier into a packaged identifier in a format readable by the tracking system, and send the packaged identifier to the tracking system.

IPC Classes  ?

  • G06Q 10/08 - Logistics, e.g. warehousing, loading or distributionInventory or stock management
  • G06V 10/96 - Management of image or video recognition tasks
  • G06V 10/70 - Arrangements for image or video recognition or understanding using pattern recognition or machine learning

44.

Lightweight, thermally stable disk for a coaxial travelling wave tube (CoTWT)

      
Application Number 17836626
Grant Number 12278079
Status In Force
Filing Date 2022-06-09
First Publication Date 2025-04-15
Grant Date 2025-04-15
Owner Raytheon Company (USA)
Inventor Sar, David R.

Abstract

A lightweight, thermally stable disk for use in a slow wave structure (SWS) of CoTWT is configurated without sacrificing thermal management, structural integrity, or RF performance. Refractory metal is removed from regions of the disk where no RF interaction is expected and replaced with resistive ceramic material. The disk includes one or more central ribs positioned about the periphery of a central hub. A plurality of U-shaped receptacles may extend from the one or more central ribs. The disk is plated with a patterned metal to define laminar conductive tabs spaced around the periphery that are separated by solid resistive ceramic tabs and to electromagnetically connect all exposed refractory metal surfaces. The plating metal must be capable of being deposited and patterned in a thin layer of 10 to 100 microns, exhibit a Young's Modulus of <100 GPa to provide both the ductility and malleability to plastically deform and exhibit an electrical conductivity at least and preferably greater than that of the refractory metal.

IPC Classes  ?

  • H01J 23/12 - VesselsContainers
  • H01J 25/34 - Travelling-wave tubesTubes in which a travelling wave is simulated at spaced gaps

45.

PRODUCT IDENTIFICATION AND TRACKING SYSTEMS AND METHODS

      
Application Number 18378078
Status Pending
Filing Date 2023-10-09
First Publication Date 2025-04-10
Owner Raytheon Company (USA)
Inventor
  • Campinell, Brian F.
  • Cavalcanti, Paulo Meireles
  • Carlo, Robert Di

Abstract

In accordance with at least one aspect of this disclosure, a product identification and tracking interface system includes an interface unit. The interface unit includes an input/output configured and adapted to be coupled to at least one of a tracking system or an identification system, a memory configured to store instructions, and a processor disposed in communication with said memory. The processor upon execution of the instructions is configured to receive a trigger command from a tracking system, send a read command to an identification system, receive a respective identifier from the identification system, package the respective identifier into a packaged identifier in a format readable by the tracking system, and send the packaged identifier to the tracking system.

IPC Classes  ?

  • G05B 19/418 - Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS] or computer integrated manufacturing [CIM]

46.

REIMAGING LENS ASSEMBLY WITH ANGLED OPTIC

      
Application Number 18482588
Status Pending
Filing Date 2023-10-06
First Publication Date 2025-04-10
Owner Raytheon Company (USA)
Inventor
  • Sinclair, Matthew A.
  • Chipper, Robert B.

Abstract

A reimaging lens assembly includes a pentaprismatic optic that includes two reflective surfaces and two refractive surfaces. The reflective surfaces are powered surfaces, and the reflective surfaces may be spherical, aspherical, and/or freeform reflective surfaces. The pentaprismatic optic may receive light from a wide field of view (WFOV), and may change the angle of the output light from that of the input light, for example by 90 degrees. The pentaprismatic optic may be coupled to an image receiver, such as a cooled or uncooled camera. The reimaging lens assembly may include further optical elements between the pentaprismatic optic and the image receiver, such as one or more lenses, filters, and/or cold stops. The lens assembly provides a compact system, with a small number of optical elements, and with desensitized output that reduces image jitter.

IPC Classes  ?

47.

MICRO-ELECTROMECHANICAL SYSTEMS SWITCH WITH BEAM MOVEMENT ORTHOGONAL TO FORCE

      
Application Number 18483892
Status Pending
Filing Date 2023-10-10
First Publication Date 2025-04-10
Owner Raytheon Company (USA)
Inventor Ghodsian, Bahram

Abstract

A micro-electromechanical systems (MEMS) switch and method of fabricating the same including at least one comb drive having a first input and a second input, at least one conductive beam connected across the at least one comb drive, a first contact, and a second contact, wherein no voltage difference between the first input and the second input does not result in any movement of the MEMS switch, and wherein a voltage difference between the first input and the second input causes an electrostatic force to be generated that causes the at least one conductive beam to move in a direction orthogonal to a direction of the electrostatic force.

IPC Classes  ?

  • H01H 1/00 - Contacts
  • H01H 1/06 - Contacts characterised by the shape or structure of the contact-making surface, e.g. grooved
  • H01H 11/00 - Apparatus or processes specially adapted for the manufacture of electric switches

48.

AUTOMATED AND VALIDATED COMPUTER DEVICE DISABLING

      
Application Number US2024049610
Publication Number 2025/076098
Status In Force
Filing Date 2024-10-02
Publication Date 2025-04-10
Owner RAYTHEON COMPANY (USA)
Inventor
  • Rothgerber, Brent
  • Norwood, Nicholas
  • Perrotta, Lucy
  • Elsaw, Kareem
  • Kneip, Raymond

Abstract

A method of operation is provided during which a plurality of hardware devices of a computer are disabled on a firmware level during a reboot of the computer in response to receiving a disable command prior to the reboot. A validation is run to determine whether or not the hardware devices are disabled. A validation signal is provided indicative of whether or not the hardware devices are validated as being disabled.

IPC Classes  ?

  • G06F 21/50 - Monitoring users, programs or devices to maintain the integrity of platforms, e.g. of processors, firmware or operating systems
  • G06F 21/57 - Certifying or maintaining trusted computer platforms, e.g. secure boots or power-downs, version controls, system software checks, secure updates or assessing vulnerabilities
  • G06F 21/82 - Protecting input, output or interconnection devices

49.

MUNITION WITH DIRECTIONAL PROJECTION EXPLOSIVE

      
Application Number US2024026218
Publication Number 2025/075674
Status In Force
Filing Date 2024-04-25
Publication Date 2025-04-10
Owner RAYTHEON COMPANY (USA)
Inventor
  • Sadler, Coulton T.
  • Lukow, Brian J.
  • Turner, Christopher Matthew

Abstract

A munition has an explosive charge with direction explosive characteristics, such as a nonuniform detonation velocities. The explosive charge may have multiple portions of explosives with nonuniform characteristics, and/or may have portions with graded nonuniform characteristics. The explosive charge may be used to propel a material from the munition in a desired manner. For example the material may be fragments that are part of a fragmentation munition. Alternatively the material may be a layer of a material, such as a metal, that produces an explosively formed penetrator or shaped charge. The explosive charge may be configured to control the spread and/or direction of the material to be propelled from the munition.

50.

REIMAGING LENS ASSEMBLY WITH ANGLED OPTIC

      
Application Number US2024039797
Publication Number 2025/075702
Status In Force
Filing Date 2024-07-26
Publication Date 2025-04-10
Owner RAYTHEON COMPANY (USA)
Inventor
  • Sinclair, Matthew A.
  • Chipper, Robert B.

Abstract

A reimaging lens assembly (100, 200, 300) includes a pentaprismatic optic (10) that includes two reflective surfaces (12, 14) and two refractive surfaces (16, 18). The reflective surfaces are powered surfaces, and the reflective surfaces may be spherical, aspherical, and/or freeform reflective surfaces. The pentaprismatic optic may receive light (22) from a wide field of view (WFOV), and may change the angle of the output light from that of the input light, for example by 90 degrees. The pentaprismatic optic may be coupled to an image receiver (116), such as a cooled or uncooled camera (130, 220, 230). The reimaging lens assembly may include further optical elements between the pentaprismatic optic and the image receiver, such as one or more lenses (102-106, 310), filters (114), and/or cold stops (112). The lens assembly provides a compact system, with a small number of optical elements, and with desensitized output that reduces image jitter.

IPC Classes  ?

  • G02B 5/04 - Prisms
  • G02B 13/06 - Panoramic objectivesSo-called "sky lenses"
  • G02B 17/04 - Catoptric systems, e.g. image erecting and reversing system using prisms only
  • G02B 17/08 - Catadioptric systems

51.

WIDEBAND ANTENNA WITH MODULAR ASSEMBLY

      
Application Number 18477594
Status Pending
Filing Date 2023-09-29
First Publication Date 2025-04-03
Owner Raytheon Company (USA)
Inventor
  • Isom, Robert S.
  • Smith, Randy L.
  • Viani-Wittwer, Kelsey Joe
  • Winniford, Paul Raymond

Abstract

A wideband antenna array includes a wide angle impedance matching (waim) board, a manifold board including multiple tower receiving features and at least one conductive tower extending outward from the manifold board and received in a corresponding tower receiving feature. Each of the at least one conductive towers including at least one metalized component. The metalized component forms a circuit connecting the manifold board to the waim board. The waim board is adhered to a first end of the at least one conductive tower opposite the manifold board.

IPC Classes  ?

  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 5/335 - Individual or coupled radiating elements, each element being fed in an unspecified way using frequency dependent circuits or components, e.g. trap circuits or capacitors at the feed, e.g. for impedance matching

52.

SOFTWARE RELEASE WORKFLOW AND RELEASABILITY DECISION ENGINE

      
Application Number 18899439
Status Pending
Filing Date 2024-09-27
First Publication Date 2025-04-03
Owner Raytheon Company (USA)
Inventor
  • Romero-Mariona, Jose
  • Dierickx, Michael
  • Poo, Kwok Liang
  • Kong, Jason
  • Le, Evanelyne
  • Poirier, James
  • Lee, Amy
  • Mckittrick, Scott
  • Reyes, Klarisa

Abstract

A computing device and method including, receiving a request for a software build and, responsive to receipt of the request for the software build, retrieving source code for the software build and retrieving a software build file for the software build, the software build file defining a build pipeline. The method also includes, by the computing device, executing a workflow to implement the software build file, generating a provenance bundle based on a monitoring of the workflow, and executing a decision engine to evaluate the provenance bundle based on one or more predetermined policies to thereby generate a recommendation regarding releasability of the software build. The method further includes providing the recommendation regarding releasability of the software build to another computing device. In some cases, executing the decision engine includes evaluating cyber threat intelligence.

IPC Classes  ?

  • G06F 8/71 - Version control Configuration management
  • H04L 9/40 - Network security protocols

53.

ASYMMETRIC EXPLOSIVE REACTIVE ARMOR (ERA)

      
Application Number US2024023847
Publication Number 2025/071670
Status In Force
Filing Date 2024-04-10
Publication Date 2025-04-03
Owner RAYTHEON COMPANY (USA)
Inventor Sadler, Coulton T.

Abstract

An asymmetric ERA box improves the disruption of a shape-charge jet for a high-explosive projectile for a given mass requirement and stand-off distance. Mass is asymmetrically redistributed from the outer plate to the rear plate in the form of increased thickness of the rear plate. This is offset by forming the outer plate of a low-density material that provides an impedance mismatch sufficient to attenuate the shockwave of low velocity projectiles (e.g., 50 caliber bullets) so that they embed in but do not detonate the explosive. The outer plate provides negligible disruption of the shape-charge jet with substantially all the disruption being provided by the thicker high density rear plate. Placement of substantially all the mass toward the front of the shape-charge jet improves overall performance of the ERA. This asymmetric configuration provides the same performance as known symmetric ERA configurations against kinetic-energy projectiles as the total mass in the outer and rear plates remains essentially the same.

54.

AUTOMATED AND VALIDATED COMPUTER DEVICE DISABLING

      
Application Number 18375783
Status Pending
Filing Date 2023-10-02
First Publication Date 2025-04-03
Owner Raytheon Company (USA)
Inventor
  • Rothgerber, Brent A.
  • Norwood, Nicholas
  • Perrotta, Lucy
  • Elsaw, Kareem D.
  • Kneip, Raymond E.

Abstract

A method of operation is provided during which a plurality of hardware devices of a computer are disabled on a firmware level during a reboot of the computer in response to receiving a disable command prior to the reboot. A validation is run to determine whether or not the hardware devices are disabled. A validation signal is provided indicative of whether or not the hardware devices are validated as being disabled.

IPC Classes  ?

55.

RF COVER LAYER

      
Application Number 18471385
Status Pending
Filing Date 2023-09-21
First Publication Date 2025-03-27
Owner Raytheon Company (USA)
Inventor
  • Puzella, Angelo M.
  • Henault, Philip M.
  • Brailovsky, Alexander B.

Abstract

A printed circuit board comprises a support structure, a conductive layer operably coupled to the support structure, a mask structure formed on the conductive layer, and a cover layer. The conductive layer comprises first and second portions of conductive material separated by a gap that defines a spacing between the first and second portions that does not contain conductive material. The mask structure defines first and second regions on the conductive layer. The first region is enclosed by a first boundary defined by the mask structure and includes the gap. The second region lies outside of the first boundary. The cover layer is sized to fit within the first region and comprises a laminatible insulating material that flows within the first region during lamination. During lamination, the first boundary prevents the laminatible insulating material from flowing into the second region, and the laminatible insulating material flows to fill the gap.

IPC Classes  ?

  • H05K 3/00 - Apparatus or processes for manufacturing printed circuits
  • H01Q 9/04 - Resonant antennas
  • H05K 1/02 - Printed circuits Details
  • H05K 3/24 - Reinforcing of the conductive pattern

56.

RF COVER LAYER

      
Application Number US2024035417
Publication Number 2025/064028
Status In Force
Filing Date 2024-06-25
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Puzella, Angelo M.
  • Henault, Philip M.
  • Brailovsky, Alexander B.

Abstract

A printed circuit board comprises a support structure (302), a conductive layer (304) operably coupled to the support structure, a mask structure (507) formed on the conductive layer, and a cover layer (508). The conductive layer comprises first and second portions (304A, 304B) of conductive material separated by a gap (608) that defines a spacing between the first and second portions that does not contain conductive material. The mask structure defines first and second regions on the conductive layer. The first region is enclosed by a first boundary defined by the mask structure and includes the gap. The second region lies outside of the first boundary. The cover layer is sized to fit within the first region and comprises a laminatible insulating material that flows within the first region during lamination. During lamination, the first boundary prevents the laminatible insulating material from flowing into the second region, and the laminatible insulating material flows to fill the gap.

IPC Classes  ?

  • H05K 1/02 - Printed circuits Details
  • H01Q 1/40 - Radiating elements coated with, or embedded in, protective material
  • H01P 3/02 - WaveguidesTransmission lines of the waveguide type with two longitudinal conductors
  • H01P 11/00 - Apparatus or processes specially adapted for manufacturing waveguides or resonators, lines, or other devices of the waveguide type
  • H01Q 1/00 - Details of, or arrangements associated with, antennas
  • H01Q 1/38 - Structural form of radiating elements, e.g. cone, spiral, umbrella formed by a conductive layer on an insulating support
  • H01Q 13/08 - Radiating ends of two-conductor microwave transmission lines, e.g. of coaxial lines, of microstrip lines
  • H05K 3/06 - Apparatus or processes for manufacturing printed circuits in which the conductive material is applied to the surface of the insulating support and is thereafter removed from such areas of the surface which are not intended for current conducting or shielding the conductive material being removed chemically or electrolytically, e.g. by photo-etch process
  • H05K 3/10 - Apparatus or processes for manufacturing printed circuits in which conductive material is applied to the insulating support in such a manner as to form the desired conductive pattern
  • H05K 3/28 - Applying non-metallic protective coatings

57.

VACUUM INSULATED WARHEAD

      
Application Number US2024047325
Publication Number 2025/064576
Status In Force
Filing Date 2024-09-18
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Rascon, John
  • Leach, John Regis
  • French, Jonathan Charles
  • Gonzales, Manuel E.

Abstract

A vacuum insulation layer is wrapped around the length of a warhead to thermally insulate the warhead from fire or aerodynamic heating. The vacuum insulation layer may be integrally formed into the warhead casing or provided as a sleeve that may be permanently or removably positioned about the warhead casing. The vacuum insulation layer is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond vac of less than one-third of the thermal conductivity of air Tcond air.

IPC Classes  ?

  • F42B 15/34 - Protection against overheating or radiation, e.g. heat shieldsAdditional cooling arrangements
  • F42B 39/18 - Heat shieldsThermal insulation

58.

HEAVY INERT GAS INSULATED WARHEAD

      
Application Number US2024047326
Publication Number 2025/064577
Status In Force
Filing Date 2024-09-18
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Rascon, John
  • Meisner, Mark J.
  • Gonzales, Manuel E.

Abstract

A heavy inert gas insulation layer is wrapped around the length of a warhead to thermally insulate the warhead from fire or aerodynamic heating. The insulation layer may be integrally formed into the warhead casing or provided as a sleeve that may be permanently or removably positioned about the warhead casing. The insulation layer contains an inert gas such as Argon, Krypton, Xenon or a synthetic gas having a density of at least 1.5 kg/m3 and a thermal conductivity Tcond_gas no greater than two-thirds of the thermal conductivity of air Tcond _air.

IPC Classes  ?

  • F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
  • F42B 12/22 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
  • F42B 12/32 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein
  • F42B 39/14 - Explosion or fire protection arrangements on packages or ammunition
  • F42B 39/18 - Heat shieldsThermal insulation

59.

EVENT DETECTION SYSTEM RESPONSE CONTROLLER

      
Application Number 18371895
Status Pending
Filing Date 2023-09-22
First Publication Date 2025-03-27
Owner Raytheon Company (USA)
Inventor
  • Bass, Gregory L.
  • Pinedo, Vincent A.

Abstract

An event detection system response controller for an electrical system includes at least one event detector (ED) digital filter submodule having a signal input and a signal output. The at least one ED digital filter submodule is configured to receive at least one event signal output from one or more event detectors at the signal input. Each of the at least one ED digital filter submodule includes a signal synchronizer, a signal filter, an interface validator, an interface validation filter, and a pulse shaper sequentially arranged from the signal input to the signal output.

IPC Classes  ?

  • G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer

60.

Vacuum insulated warhead

      
Application Number 18471828
Grant Number 12298115
Status In Force
Filing Date 2023-09-21
First Publication Date 2025-03-27
Grant Date 2025-05-13
Owner Raytheon Company (USA)
Inventor
  • Rascon, John
  • Leach, John Regis
  • French, Jonathan Charles
  • Gonzales, Manuel E.

Abstract

A vacuum insulation layer is wrapped around the length of a warhead to thermally insulate the warhead from fire or aerodynamic heating. The vacuum insulation layer may be integrally formed into the warhead casing or provided as a sleeve that may be permanently or removably positioned about the warhead casing. The vacuum insulation layer is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond_vac of less than one-third of the thermal conductivity of air Tcond_air.

IPC Classes  ?

  • F42B 39/18 - Heat shieldsThermal insulation
  • F42B 12/22 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction

61.

VACUUM INSULATED BLAST TUBE

      
Application Number 18471908
Status Pending
Filing Date 2023-09-21
First Publication Date 2025-03-27
Owner Raytheon Company (USA)
Inventor
  • Rascon, John
  • Formica, Anthony V.
  • Leach, John Regis

Abstract

A vacuum insulated blast tube includes an insulating layer of a burn resistant material such as phenolic resin formed on an interior surface of the blast tube to provide the necessary erosion and thermal insulation properties to protect the blast tube and a vacuum insulated layer formed in the walls of the blast tube itself to provide the additional thermal insulation properties to protect any non-propulsive sub-systems positioned in the void space around the blast tube. A void space in the walls of the blast tube is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond_vac of less than one-third of the thermal conductivity of air Tcond_air to form the vacuum insulation layer.

IPC Classes  ?

  • F02K 9/34 - CasingsCombustion chambersLiners thereof

62.

TRANSPORTING ULTRA-HIGH DEFINITION VIDEO FROM MULTIPLE SOURCES

      
Application Number 18912153
Status Pending
Filing Date 2024-10-10
First Publication Date 2025-03-27
Owner Raytheon Company (USA)
Inventor
  • Woody, Carl A.
  • Hook, Tyler Layne

Abstract

A sensor data processing apparatus can be coupled to multiple image sensors of different types. The apparatus adjusts frame transmission rates based on the number of sensors and type of image data sourced by the sensors to optimize utilization of bandwidth on a number of transport channels. The apparatus can be configured to transport selected frames in the image data that are identified as critical frames at a higher rate than non-selected frames in the image data.

IPC Classes  ?

  • H04N 5/77 - Interface circuits between an apparatus for recording and another apparatus between a recording apparatus and a television camera
  • H04N 5/268 - Signal distribution or switching
  • H04N 7/01 - Conversion of standards
  • H04N 7/015 - High-definition television systems
  • H04N 7/08 - Systems for the simultaneous or sequential transmission of more than one television signal, e.g. additional information signals, the signals occupying wholly or partially the same frequency band
  • H04N 21/234 - Processing of video elementary streams, e.g. splicing of video streams or manipulating encoded video stream scene graphs
  • H04N 21/236 - Assembling of a multiplex stream, e.g. transport stream, by combining a video stream with other content or additional data, e.g. inserting a URL [Uniform Resource Locator ] into a video stream, multiplexing software data into a video streamRemultiplexing of multiplex streamsInsertion of stuffing bits into the multiplex stream, e.g. to obtain a constant bit-rateAssembling of a packetised elementary stream
  • H04N 21/63 - Control signaling between client, server and network componentsNetwork processes for video distribution between server and clients, e.g. transmitting basic layer and enhancement layers over different transmission paths, setting up a peer-to-peer communication via Internet between remote STB'sCommunication protocolsAddressing

63.

FLANGE CLAMPING DEVICE FOR SMALL ANTENNA PEDESTALS

      
Application Number US2024037817
Publication Number 2025/064037
Status In Force
Filing Date 2024-07-12
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Marchetti, Paul, J.
  • Richardson, Craig
  • Toomey, Michael, A.

Abstract

A clamping device (16) for securing a first component (12) to a second component (14) is disclosed. The clamping device includes a mounting flange (18) coupled to the first component, a mounting seat (24) coupled to the second component, and a clamping ring (22) configured to be rotatably seated on the mounting flange such that the mounting flange is disposed axially between a first end of the clamping ring and the mounting seat upon assembly. The mounting seat includes a plurality of first locking ramps disposed about a circumference of the mounting seat and extending radially outward from the mounting seat. The clamping ring includes a plurality of second locking ramps (68) disposed about an inner circumference and extending radially inward from a second end of the clamping ring. The plurality of second locking ramps is configured to engage the plurality of first locking ramps upon securing the first component to the second component.

IPC Classes  ?

  • F16M 11/04 - Means for attachment of apparatusMeans allowing adjustment of the apparatus relatively to the stand
  • F16B 7/00 - Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
  • F16M 11/16 - Details concerning attachment of head-supporting legs, with or without actuation of locking members therefor
  • F16M 11/24 - Undercarriages with or without wheels changeable in height or length of legs, also for transport only
  • F16B 21/04 - Releasable fastening devices locking by rotation with bayonet catch

64.

EVENT DETECTION SYSTEM RESPONSE CONTROLLER

      
Application Number US2024039023
Publication Number 2025/064044
Status In Force
Filing Date 2024-07-22
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Bass, Gregory
  • Pinedo, Vincent

Abstract

An event detection system response controller for an electrical system includes at least one event detector (ED) digital filter submodule having a signal input and a signal output. The at least one ED digital filter submodule is configured to receive at least one event signal output from one or more event detectors at the signal input. Each of the at least one ED digital filter submodule includes a signal synchronizer, a signal filter, an interface validator, an interface validation filter, and a pulse shaper sequentially arranged from the signal input to the signal output.

IPC Classes  ?

65.

HEAVY INERT GAS INSULATED ROCKET ENGINE BLAST TUBE

      
Application Number US2024047327
Publication Number 2025/064578
Status In Force
Filing Date 2024-09-18
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Rascon, John
  • Formica, Anthony V.
  • Meisner, Mark J.

Abstract

An insulated blast tube includes an insulating layer of a burn resistant material such as phenolic resin formed on an interior surface of the blast tube to provide the necessary erosion and thermal insulation properties to protect the blast tube and a heavy inert gas insulated layer formed in the walls of the blast tube itself to provide the additional thermal insulation properties to protect any non-propulsive sub-systems positioned in the void space around the blast tube. A void space in the walls of the blast tube contains an inert gas such as Argon, Krypton, Xenon or a synthetic inert gas having a density of at least 1.5 kg/m3 and a thermal conductivity Tcond_gas of no greater than two-thirds the thermal conductivity of air Tcond_air to form the heavy inert gas insulation layer.

IPC Classes  ?

66.

VACUUM INSULATED BLAST TUBE

      
Application Number US2024047329
Publication Number 2025/064580
Status In Force
Filing Date 2024-09-18
Publication Date 2025-03-27
Owner RAYTHEON COMPANY (USA)
Inventor
  • Rascon, John
  • Formica, Anthony V.
  • Leach, John Regis

Abstract

A vacuum insulated blast tube (200) includes an insulating layer (206) of a burn resistant material such as phenolic resin formed on an interior surface of the blast tube to provide the necessary erosion and thermal insulation properties to protect the blast tube and a vacuum insulation layer (208) formed in the walls of the blast tube itself to provide the additional thermal insulation properties to protect any non-propulsive sub-systems positioned in the void space around the blast tube. A void space (204) in the walls of the blast tube is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond _vac of less than one-third of the thermal conductivity of air Tcond_air to form the vacuum insulation layer.

IPC Classes  ?

  • F42B 15/34 - Protection against overheating or radiation, e.g. heat shieldsAdditional cooling arrangements
  • F02K 9/32 - Constructional partsDetails not otherwise provided for

67.

FLANGE CLAMPING DEVICE FOR SMALL ANTENNA PEDESTALS

      
Application Number 18370102
Status Pending
Filing Date 2023-09-19
First Publication Date 2025-03-20
Owner Raytheon Company (USA)
Inventor
  • Marchetti, Paul J.
  • Richardson, Craig
  • Toomey, Michael A.

Abstract

A clamping device for securing a first component to a second component is disclosed. The clamping device includes a mounting flange coupled to the first component, a mounting seat coupled to the second component, and a clamping ring configured to be rotatably seated on the mounting flange such that the mounting flange is disposed axially between a first end of the clamping ring and the mounting seat upon assembly. The mounting seat includes a plurality of first locking ramps disposed about a circumference of the mounting seat and extending radially outward from the mounting seat. The clamping ring includes a plurality of second locking ramps disposed about an inner circumference and extending radially inward from a second end of the clamping ring. The plurality of second locking ramps is configured to engage the plurality of first locking ramps upon securing the first component to the second component.

IPC Classes  ?

68.

METHOD FOR MANUFACTURING BRUSHLESS DC MOTOR

      
Application Number 18368368
Status Pending
Filing Date 2023-09-14
First Publication Date 2025-03-20
Owner Raytheon Company (USA)
Inventor Sutton, Gary Joseph

Abstract

A method for making a brushless DC motor includes the steps of: applying coils to a plurality of teeth that extend radially outwardly from an inner ring; mounting an outer ring to radially outer ends of the plurality of teeth; and removing segments of the inner ring.

IPC Classes  ?

  • H02K 15/08 - Forming windings by laying conductors into or around core parts
  • H02K 1/02 - Details of the magnetic circuit characterised by the magnetic material
  • H02K 1/18 - Means for mounting or fastening magnetic stationary parts on to, or to, the stator structures
  • H02K 15/02 - Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies
  • H02K 15/06 - Embedding prefabricated windings in the machines

69.

METHOD FOR MANUFACTURING BRUSHLESS DC MOTOR

      
Application Number US2024046374
Publication Number 2025/059292
Status In Force
Filing Date 2024-09-12
Publication Date 2025-03-20
Owner RAYTHEON COMPANY (USA)
Inventor Sutton, Gary Joseph

Abstract

A method for making a brushless DC motor includes the steps of: applying coils to a plurality of teeth that extend radially outwardly from an inner ring; mounting an outer ring to radially outer ends of the plurality of teeth; and removing segments of the inner ring.

IPC Classes  ?

  • H02K 1/14 - Stator cores with salient poles
  • H02K 15/02 - Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies
  • H02K 15/06 - Embedding prefabricated windings in the machines
  • H02K 15/095 - Forming windings by laying conductors into or around core parts by laying conductors around salient poles

70.

ANONYMIZED INDICATION AND/OR IDENTIFICATION OF EXCLUSION ZONES FOR UNCREWED AERIAL VEHICLES OR OTHER FLIGHT VEHICLES

      
Application Number 18791606
Status Pending
Filing Date 2024-08-01
First Publication Date 2025-03-13
Owner Raytheon Company (USA)
Inventor
  • Rogers, Christopher J.
  • Edry, Mark J.

Abstract

A method includes obtaining data associated with a specified airspace indicating or identifying manned flights within the specified airspace and identifying one or more exclusion zones associated with one or more manned flights within the specified airspace based on the data. Each exclusion zone identifies a volume from which one or more flight vehicles are excluded from operating within the specified airspace. The method also includes modifying each exclusion zone in order to randomly change a shape of exclusion zone and generate one or more modified exclusion zones. In addition, the method includes providing information defining the modified exclusion zone(s) to one or more flight vehicle operators so that the one or more flight vehicle operators are able to avoid operating the flight vehicle(s) in the modified exclusion zone(s). The information defining modified exclusion zone(s) lacks information identifying the manned flights within the exclusion zone(s).

IPC Classes  ?

71.

HIGH STIFFNESS TRIPOD FOR MAN TRANSPORTABLE SATCOM ANTENNA

      
Application Number 18457828
Status Pending
Filing Date 2023-08-29
First Publication Date 2025-03-06
Owner Raytheon Company (USA)
Inventor
  • Toomey, Michael A.
  • Marchetti, Paul J.
  • Richardson, Craig
  • Flick, Jonathan J.
  • Thomann, Derik S.

Abstract

A tripod for a transportable SATCOM antenna includes a base with a frame centered on a center axis. A first leg is connected to the frame of the base by a first hinge, a second leg is connected to the frame of the base by a second hinge, and a third leg is connected to the frame of the base by a third hinge. A first strut extends from the first leg to the second leg, a second strut extends from the second leg to the third leg, and a third strut extends from the third leg to the first leg. The first strut, the second strut, and the third strut each include a first strut segment, a second strut segment, and a hinge connecting the first strut segment and the second strut segment. A locking collar is on the first strut segment and extends over the hinge.

IPC Classes  ?

  • H01Q 1/12 - SupportsMounting means
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons

72.

Bidirectionally Integrated Guiding Metasurface Angle Compactor

      
Application Number 18458145
Status Pending
Filing Date 2023-08-29
First Publication Date 2025-03-06
Owner Raytheon Company (USA)
Inventor
  • Sorbel, Scott Randall
  • Hatch, Tamara A.

Abstract

A system that allows for electromagnetic energy to be “re-routed” around normally occlusive structures. The system comprises a first multilayer metasurface device and a second multilayer metasurface device. The first multilayer metasurface device has a plurality of wave refractors fabricated on a first metasurface and a plurality of wave combiners fabricated on a second metasurface. The second multilayer metasurface device has a plurality of wave splitters fabricated on a first metasurface and a plurality of wave refractors fabricated on a second metasurface. The occlusive structures are disposed between the first multilayer metasurface device and the second multilayer metasurface device such that energy is re-routed around the occlusive structures.

IPC Classes  ?

  • H01Q 15/02 - Refracting or diffracting devices, e.g. lens, prism
  • H01Q 1/36 - Structural form of radiating elements, e.g. cone, spiral, umbrella

73.

DEVICE FOR AND METHOD OF FREQUENCY TESTING PRINTED CIRCUIT BOARD UNDER THERMAL STRESS

      
Application Number US2024043089
Publication Number 2025/049177
Status In Force
Filing Date 2024-08-20
Publication Date 2025-03-06
Owner RAYTHEON COMPANY (USA)
Inventor
  • Northrup, Mark Ryan
  • Rodack, Andrew Ryan
  • Riley, Matthew E.
  • Hamilton, Maxwell John

Abstract

A printed circuit board (PCB) test system and method including temperature chamber including at least one slot to accommodate at least one PCB test coupon, input bus connected to inputs of the at least one slot, and output bus connected to outputs of the at least one slot, wherein temperature chamber is configured to apply a temperature to the at least one PCB test coupon; signal generator including output bus connected to the input bus of the at least one slot, frequency meter comprising an input bus connected to the output bus of the at least one slot and an output bus, and a comparator connected to the output bus of the signal generator and the output bus of the frequency meter for comparing corresponding outputs of the signal generator and the frequency meter.

IPC Classes  ?

  • G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer

74.

IMAGE REGISTRATION TO A 3D POINT SET

      
Application Number 18455400
Status Pending
Filing Date 2023-08-24
First Publication Date 2025-02-27
Owner Rayheon Company (USA)
Inventor Ely, Richard W.

Abstract

Devices, systems, and methods for image processing; wherein a method can include generating a synthetic image based on the 3D point set of a same geographical region as the 2D real image and performing a coarse registration to grossly register the synthetic image to the 2D real image, the coarse registration including determining, for a plurality of synthetic image tiles that span the synthetic and at each of a plurality of offsets in a search region, a correlation score resulting in a plurality of correlation score arrays, determining a weighted combination of scores in the correlation score arrays resulting in a combined correlation score array, identifying an offset of the plurality of offsets based on the combined correlation score array, and moving the synthetic image relative to the 2D real image by the identified offset.

IPC Classes  ?

  • G06T 7/33 - Determination of transform parameters for the alignment of images, i.e. image registration using feature-based methods
  • G06T 7/32 - Determination of transform parameters for the alignment of images, i.e. image registration using correlation-based methods

75.

EXTRACTION OF 3D EVALUATION POINTS FOR IMAGE CONJUGATES

      
Application Number 18455416
Status Pending
Filing Date 2023-08-24
First Publication Date 2025-02-27
Owner Raytheon Company (USA)
Inventor
  • Ely, Richard W.
  • Verret, Jody D.

Abstract

Devices, systems, and methods for three-dimensional (3D) evaluation point (3DEP) identification; wherein a method can include receiving a first conjugate point of a first real two-dimensional (2D) image, receiving a second conjugate point of a second real 2D image, the first and second conjugate points corresponding to a same geographical location, determining a first set of points of a 3D point set that project to within a specified distance of the first conjugate point in the first real 2D image, determining a second set of points of the 3D point set that project to within the specified distance of the second conjugate point in the second real 2D image, identifying a common point in both the first set of points and the second set of points that satisfies a specified heuristic relative to all other points in both the first set of points and the second set of points, and using the point as the 3DEP.

IPC Classes  ?

  • G06T 17/05 - Geographic models
  • G06V 10/74 - Image or video pattern matchingProximity measures in feature spaces

76.

DEVICE FOR AND METHOD OF FREQUENCY TESTING PRINTED CIRCUIT BOARD UNDER THERMAL STRESS

      
Application Number 18456010
Status Pending
Filing Date 2023-08-25
First Publication Date 2025-02-27
Owner Raytheon Company (USA)
Inventor
  • Northrup, Mark Ryan
  • Rodack, Andrew Ryan
  • Riley, Matthew E.
  • Hamilton, Maxwell John

Abstract

A printed circuit board (PCB) test system and method including temperature chamber including at least one slot to accommodate at least one PCB test coupon, input bus connected to inputs of the at least one slot, and output bus connected to outputs of the at least one slot, wherein temperature chamber is configured to apply a temperature to the at least one PCB test coupon; signal generator including output bus connected to the input bus of the at least one slot, frequency meter comprising an input bus connected to the output bus of the at least one slot and an output bus, and a comparator connected to the output bus of the signal generator and the output bus of the frequency meter for comparing corresponding outputs of the signal generator and the frequency meter.

IPC Classes  ?

  • G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer

77.

Refractory Material with Supercritical Fluid-Deposited Interface Coatings

      
Application Number 18455568
Status Pending
Filing Date 2023-08-24
First Publication Date 2025-02-27
Owner Raytheon Company (USA)
Inventor Foreman, James E.

Abstract

A refractory material can include a refractory filament and an interface coating applied to the refractory filament. The interface coating can include a refractory metal or semi-metal oxide, metal or semi-metal nitride, metal or semi-metal carbide, metal or semi-metal oxynitride, metal or semi-metal carbonitride, and/or metal or semi metal oxycarbide formed by depositing an organometallic precursor onto the refractory filament by supercritical fluid deposition and heat treating the organometallic precursor in the presence of an atmospheric condition so that the organometallic precursor forms an interface coating that is an oxidized, pyrolyzed, or carbidized form of the organometallic precursor and is present at a surface and beneath the surface of the refractory filament.

IPC Classes  ?

  • C04B 41/45 - Coating or impregnating
  • C04B 35/76 - Fibres, filaments, whiskers, platelets, or the like
  • C04B 41/00 - After-treatment of mortars, concrete, artificial stone or ceramicsTreatment of natural stone

78.

IMAGE REGISTRATION TO A 3D POINT SET

      
Application Number US2024043081
Publication Number 2025/042911
Status In Force
Filing Date 2024-08-20
Publication Date 2025-02-27
Owner RAYTHEON COMPANY (USA)
Inventor Ely, Richard W.

Abstract

Devices, systems, and methods for image processing; wherein a method can include generating a synthetic image based on the 3D point set of a same geographical region as the 2D real image and performing a coarse registration to grossly register the synthetic image to the 2D real image, the coarse registration including determining, for a plurality of synthetic image tiles that span the synthetic and at each of a plurality of offsets in a search region, a correlation score resulting in a plurality of correlation score arrays, determining a weighted combination of scores in the correlation score arrays resulting in a combined correlation score array, identifying an offset of the plurality of offsets based on the combined correlation score array, and moving the synthetic image relative to the 2D real image by the identified offset.

IPC Classes  ?

  • G06T 7/32 - Determination of transform parameters for the alignment of images, i.e. image registration using correlation-based methods

79.

Vibration compensated interferometric noise suppressed oscillator (INSO)

      
Application Number 18364981
Grant Number 12237810
Status In Force
Filing Date 2023-08-03
First Publication Date 2025-02-25
Grant Date 2025-02-25
Owner Raytheon Company (USA)
Inventor
  • Dervay, James Andrew
  • Moore, Gary Ian

Abstract

Vibration compensation is provided for Interferometric Noise Suppressed Oscillators (INSOs). In an INSO the error signal at the mixer output responds linearly to changes in carrier frequency. A vibration compensation signal is summed with the error signal at the input to the feedback amplifier to provide the control signal to the loop phase shifter to suppress close-in phase noise near the carrier frequency and to reduce the effects of mechanical vibrations on oscillator phase noise. The addition of the vibration compensation signal does degrade carrier suppression, hence increases the flicker noise contributed by the INSO's LNA but does so without degrading overall oscillator phase noise. In a frequency tuned configuration, the vibration compensation signal reduces the effects of mechanical vibrations on oscillator phase noise independent of the tuning voltage applied to the phase shifter.

IPC Classes  ?

  • H03B 5/36 - Generation of oscillations using amplifier with regenerative feedback from output to input with frequency-determining element being electromechanical resonator being a piezoelectric resonator active element in amplifier being semiconductor device
  • H03B 5/18 - Generation of oscillations using amplifier with regenerative feedback from output to input with frequency-determining element comprising distributed inductance and capacitance
  • H03L 1/00 - Stabilisation of generator output against variations of physical values, e.g. power supply
  • H03L 7/099 - Details of the phase-locked loop concerning mainly the controlled oscillator of the loop

80.

DIFFRACTIVE OPTICAL STRUCTURES AND METHODS FOR MANUFACTURING SAME

      
Application Number 18450503
Status Pending
Filing Date 2023-08-16
First Publication Date 2025-02-20
Owner Raytheon Company (USA)
Inventor
  • Crifasi, Joseph
  • Schaefer, John P.

Abstract

An diffractive optical element article and a method for manufacturing the diffractive optical element article is disclosed where the optical grating article includes a bulk material substrate having a bulk material surface and a Bulk Material (BM) index of refraction, an amorphous material film layer deposited onto the bulk material surface, the amorphous material film layer having a film thickness and an amorphous material film layer index of refraction and a plurality of diffractive optical elements machined into the amorphous material film layer, wherein each of the plurality of diffractive optical elements include a diffractive optical element thickness and a diffractive optical element profile.

IPC Classes  ?

  • G02B 27/42 - Diffraction optics
  • G02B 1/10 - Optical coatings produced by application to, or surface treatment of, optical elements
  • G02B 5/18 - Diffracting gratings

81.

CONFORMAL WAVEFRONT TRANSFORMER AND METHOD OF MAKING

      
Application Number 18451893
Status Pending
Filing Date 2023-08-18
First Publication Date 2025-02-20
Owner Raytheon Company (USA)
Inventor
  • Crouch, David D.
  • Kazemi, Hooman
  • Brailovsky, Alexander B.

Abstract

A wavefront transformer for reflecting and transforming an incident electromagnetic wavefront includes an electrically-conductive substrate with spaced perforations (cavities), which may have uniform spacing and varying depth. The perforations may have a radius that is close to and greater than a cutoff radius for one or more intended incident frequencies of the incident wavefront. The spaced perforations may be filled with air or may be filled with a dielectric solid material. The substrate may be covered with a cover made of a dielectric solid material. The transformer may be made by drilling holes in the substrate. Alternatively a plate having protrusions on it corresponding to the desired perforations may be used to form the perforations on the substrate. The plate may be removed or left in place after the formation of the perforations.

IPC Classes  ?

  • H01Q 19/10 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
  • H01Q 15/14 - Reflecting surfacesEquivalent structures

82.

REAL-TIME IN-SITU ADDITIVE CIRCUIT TUNING FOR RF/MICROWAVE ELECTRONICS

      
Application Number 18233596
Status Pending
Filing Date 2023-08-14
First Publication Date 2025-02-20
Owner Raytheon Company (USA)
Inventor
  • Areias, Christopher
  • Luce, Andrew M.
  • Alexander, Gavin
  • Ranasingha, Oshada K.
  • Akyurtlu, Alkim
  • Trulli, Susan C.

Abstract

A method of tuning a circuit includes measuring an electrical characteristic of the circuit and forming, by an automated process, a conductive trace connected to the circuit to adjust the electrical characteristic of the circuit. The steps of measuring the electrical characteristic and forming the conductive trace are conducted simultaneously. The automated process involves adjusting a physical characteristic of the conductive trace in real-time in response to results of measuring the electrical characteristic of the circuit until the electrical characteristic of the circuit complies with a selected criterion.

IPC Classes  ?

  • H05K 3/12 - Apparatus or processes for manufacturing printed circuits in which conductive material is applied to the insulating support in such a manner as to form the desired conductive pattern using printing techniques to apply the conductive material
  • H05K 1/09 - Use of materials for the metallic pattern

83.

REAL-TIME IN-SITU ADDITIVE CIRCUIT TUNING FOR RF/MICROWAVE ELECTRONICS

      
Application Number US2024040513
Publication Number 2025/038290
Status In Force
Filing Date 2024-08-01
Publication Date 2025-02-20
Owner RAYTHEON COMPANY (USA)
Inventor
  • Areias, Christopher
  • Luce, Andrew, M.
  • Alexander, Gavin
  • Ranasingha, Oshada, K.
  • Akyurtlu, Alkim
  • Trulli, Susan, C.

Abstract

A method of tuning a circuit includes measuring an electrical characteristic of the circuit and forming, by an automated process, a conductive trace connected to the circuit to adjust the electrical characteristic of the circuit. The steps of measuring the electrical characteristic and forming the conductive trace are conducted simultaneously. The automated process involves adjusting a physical characteristic of the conductive trace in real-time in response to results of measuring the electrical characteristic of the circuit until the electrical characteristic of the circuit complies with a selected criterion.

IPC Classes  ?

  • H05K 1/02 - Printed circuits Details
  • H05K 1/09 - Use of materials for the metallic pattern
  • H05K 3/10 - Apparatus or processes for manufacturing printed circuits in which conductive material is applied to the insulating support in such a manner as to form the desired conductive pattern
  • H05K 3/12 - Apparatus or processes for manufacturing printed circuits in which conductive material is applied to the insulating support in such a manner as to form the desired conductive pattern using printing techniques to apply the conductive material
  • H05K 3/22 - Secondary treatment of printed circuits

84.

PIERCER

      
Serial Number 99041534
Status Pending
Filing Date 2025-02-14
Owner Raytheon Company ()
NICE Classes  ? 13 - Firearms; explosives

Goods & Services

Missiles; projectiles; spare parts for missiles; munitions for missiles; warheads for missiles

85.

Adaptive structure for thermal regulation and optimization

      
Application Number 17499040
Grant Number 12224223
Status In Force
Filing Date 2021-10-12
First Publication Date 2025-02-11
Grant Date 2025-02-11
Owner Raytheon Company (USA)
Inventor
  • Hieb, Edward L.
  • Day, Nicholas C.
  • Nobrega, Ken Salas

Abstract

A method includes forming an initial structure having voids, where the initial structure includes one or more first materials. The method also includes infiltrating one or more second materials into the initial structure, where the one or more second materials are different from the one or more first materials. The method further includes forming a finished structure configured to receive and support one or more heat-generating components. A combination of the first and second materials provides a coefficient of thermal expansion in a portion of the finished structure that substantially matches a coefficient of thermal expansion of the one or more heat-generating components. The finished structure is configured to provide a path to remove thermal energy from the one or more heat-generating components.

IPC Classes  ?

  • H01L 23/367 - Cooling facilitated by shape of device
  • B22F 10/28 - Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 40/20 - Post-treatment, e.g. curing, coating or polishing
  • B33Y 80/00 - Products made by additive manufacturing
  • H01L 21/48 - Manufacture or treatment of parts, e.g. containers, prior to assembly of the devices, using processes not provided for in a single one of the groups or
  • H01L 23/373 - Cooling facilitated by selection of materials for the device

86.

Passive bypass for mitigation of inlet buzz in supersonic or hypersonic air-breathing engines

      
Application Number 18635986
Grant Number 12221925
Status In Force
Filing Date 2024-04-15
First Publication Date 2025-02-11
Grant Date 2025-02-11
Owner Raytheon Company (USA)
Inventor O'Brien, Timothy

Abstract

A passive bypass for an inlet to a supersonic or hypersonic air-breathing engine allows airflow in the inlet to exit through the cowling when the inlet supplies more airflow than the air-breathing engine demands. The air-breathing engine may be the only form of propulsion or a secondary form of propulsion to reach higher speeds. The passive bypass includes a plurality of lower channels in the cowling that are operatively coupled to the inlet diffuser at an inner surface of the cowling and swept forward towards the throat, a plenum in the cowling operatively coupled to the plurality of lower openings and a plurality of upper channels in the cowling that are operatively coupled to the plenum and swept back away from the throat to an outer surface of the cowling. A serpentine path through the plurality of lower openings, the plenum and the plurality of upper openings allows airflow in the inlet to exit through the cowling when the inlet supplies more airflow than the air-breathing engine demands.

IPC Classes  ?

  • F02C 7/04 - Air intakes for gas-turbine plants or jet-propulsion plants
  • B64D 33/02 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
  • F02C 7/045 - Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
  • F02C 7/057 - Control or regulation
  • F02C 7/24 - Heat or noise insulation
  • F02K 1/82 - Jet pipe walls, e.g. liners
  • F02K 7/10 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fanControl thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
  • F02K 7/14 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fanControl thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
  • F02K 7/18 - Composite ram-jet/rocket engines

87.

Systems and methods for modular radar systems

      
Application Number 18485029
Grant Number 12222438
Status In Force
Filing Date 2023-10-11
First Publication Date 2025-02-11
Grant Date 2025-02-11
Owner Raytheon Company (USA)
Inventor
  • Rocca, Derek P.
  • Borkowski, Michael T.
  • Lulsdorf, Thomas
  • Walsh, Jr., Kenneth P.
  • Yafrate, Christopher J.
  • Martinez, Michael P.
  • Nolan, Erin K.
  • Bellahrossi, Kassam K.
  • Cavener, Bryan J.

Abstract

A system and apparatus is provided for a modular radar system. The modular radar system can include a plurality of radar system modules that can be detachably coupled and can include a configurable number of radio-frequency (RF) transmit and receive assemblies. The RF transmit and receive assemblies can include radiating element(s) that emit electromagnetic radiation. The plurality of radar system modules can also include at least one processor coupled to control power of the electromagnetic radiation and/or at least one controller to control the RF transmit and receive assembly, the power unit and the digital receiver and exciter module, at least one digital receiver and exciter to convert RF to digital in receive mode, and digital to RF in transmit mode, and/or at least one RF beamformer to generate one or more RF beams.

IPC Classes  ?

  • G01S 7/03 - Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating
  • G01S 7/02 - Details of systems according to groups , , of systems according to group

88.

SYSTEM AND METHOD OF HYPERSONIC OBJECT TRACKING

      
Application Number 18797114
Status Pending
Filing Date 2024-08-07
First Publication Date 2025-02-06
Owner Raytheon Company (USA)
Inventor Koblick, Darin C.

Abstract

A system and method of tracking a hypersonic object over a flightpath includes at least one observer having at least one sensor. The sensor is configured to provide measurements of the hypersonic object that are geometrically diverse such that each observer may independently measure any combination of range, angles, Doppler, and angle rates. The observers transmit measurements to a processing unit as the hypersonic object undergoes three phases including a boost phase, a ballistic phase, and a hypersonic glide phase. The hypersonic object is tracked over many time steps by first selecting a dynamics model representative of expected object kinematics during said phase. Then, an unscented Kalman filter is used to predict a future state and a covariance using the dynamics model that was selected. Finally, the unscented Kalman filter updates the future state and covariance that were predicted based on the geometrically diverse measurements of the sensors.

IPC Classes  ?

  • G01S 13/72 - Radar-tracking systemsAnalogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar
  • F41G 7/30 - Command link guidance systems
  • G01C 21/20 - Instruments for performing navigational calculations
  • G01S 5/02 - Position-fixing by co-ordinating two or more direction or position-line determinationsPosition-fixing by co-ordinating two or more distance determinations using radio waves
  • G01S 13/58 - Velocity or trajectory determination systemsSense-of-movement determination systems

89.

TACTICAL HIGH POWER MICROWAVE ANTENNA PEDESTAL

      
Application Number 18357422
Status Pending
Filing Date 2023-07-24
First Publication Date 2025-01-30
Owner Raytheon Company (USA)
Inventor
  • Toomey, Michael A.
  • Marchetti, Paul J.
  • Kemp, Steven P.
  • Rocca, Derek P.
  • Dressel, Earl M.

Abstract

An antenna system comprises a reflector subsystem, a rotatable support structure and a support member. The reflector subsystem receives an input beam and reflects the input beam to produce an output beam steered in elevation by an elevation reflector and in azimuth by an azimuth reflector, towards a target. The rotatable support structure is operably coupled to the azimuth reflector and to the elevation reflector and is configured to rotate them simultaneously. The support member comprises a lengthwise portion coupled to the rotatable support structure and an offset portion coupled to the elevation reflector, the offset portion configured to offset the elevation reflector from the lengthwise portion. The offset portion is configured to enable clearance of the elevation reflector during beam steering of the output beam to extreme ends of a range of motion of the elevation reflector.

IPC Classes  ?

  • F41H 13/00 - Means of attack or defence not otherwise provided for
  • H01Q 1/32 - Adaptation for use in or on road or rail vehicles
  • H01Q 3/08 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation

90.

TACTICAL HIGH POWER MICROWAVE ANTENNA PEDESTAL

      
Application Number US2024039137
Publication Number 2025/024434
Status In Force
Filing Date 2024-07-23
Publication Date 2025-01-30
Owner RAYTHEON COMPANY (USA)
Inventor
  • Toomey, Michael A.
  • Marchetti, Paul J.
  • Kemp, Steven P.
  • Rocca, Derek P.
  • Dressel, Earl M.

Abstract

An antenna system comprises a reflector subsystem, a rotatable support structure and a support member. The reflector subsystem receives an input beam and reflects the input beam to produce an output beam steered in elevation by an elevation reflector and in azimuth by an azimuth reflector, towards a target. The rotatable support structure is operably coupled to the azimuth reflector and to the elevation reflector and is configured to rotate them simultaneously. The support member comprises a lengthwise portion coupled to the rotatable support structure and an offset portion coupled to the elevation reflector, the offset portion configured to offset the elevation reflector from the lengthwise portion. The offset portion is configured to enable clearance of the elevation reflector during beam steering of the output beam to extreme ends of a range of motion of the elevation reflector.

IPC Classes  ?

  • H01Q 1/12 - SupportsMounting means
  • F41H 13/00 - Means of attack or defence not otherwise provided for
  • H01Q 1/32 - Adaptation for use in or on road or rail vehicles
  • H01Q 3/06 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation over a restricted angle
  • H01Q 3/08 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
  • H01Q 19/13 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
  • H01Q 19/18 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces
  • H01Q 19/19 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface

91.

DEEPSTRIKE

      
Serial Number 99022723
Status Pending
Filing Date 2025-01-29
Owner Raytheon Company ()
NICE Classes  ? 13 - Firearms; explosives

Goods & Services

Weapon systems, namely missiles, rockets, surface-to-surface missiles, long-range precision fire missiles, missile launchers, submunitions

92.

ELECTRO-MECHANICAL QUICK CONNECTOR WITH INTEGRAL ACCESS TOOL

      
Application Number 18353499
Status Pending
Filing Date 2023-07-17
First Publication Date 2025-01-23
Owner Raytheon Company (USA)
Inventor Leapley, Brian D.

Abstract

An electro-mechanical tool includes a handheld housing, an electrical cable, and an electro-mechanical head. The electro-mechanical head includes an electrical connector and a tool subassembly. The electrical connector includes pins, each pin connected to a lead of the electrical cable. The tool subassembly includes a bit attached to a cap, which is distally located relative to the electrical connector.

IPC Classes  ?

  • H01R 43/26 - Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for engaging or disengaging the two parts of a coupling device
  • H01R 13/447 - Shutter or cover plate

93.

COMPACT INTEGRATED CIRCUIT INPUT WITH LEVEL-SHIFTING TO SUPPORT RANGE OF I/O VOLTAGES

      
Application Number 18353996
Status Pending
Filing Date 2023-07-18
First Publication Date 2025-01-23
Owner Raytheon Company (USA)
Inventor
  • Harris, Micky R.
  • Willis, Magathi J.

Abstract

An apparatus includes an input circuit configured to level-shift an input signal and generate an output signal having a voltage range different than a voltage range of the input signal. The input circuit includes (i) a blocking gate configured to level shift the input signal and (ii) an inverter or buffer configured to generate the output signal based on an output of the blocking gate. The input circuit is configured to generate the output signal such that the voltage range of the output signal spans between a first voltage provided to the inverter or buffer and a second voltage provided to the inverter or buffer. The blocking gate may include a transistor, a source or drain of the transistor may be configured to receive the input signal, and a gate of the transistor may be configured to receive the first voltage. The first voltage may include a core voltage of an integrated circuit device.

IPC Classes  ?

  • H03K 19/0185 - Coupling arrangementsInterface arrangements using field-effect transistors only

94.

INTERFACE BUILT IN TEST FAILURE DETECTION APPARATUS

      
Application Number 18354808
Status Pending
Filing Date 2023-07-19
First Publication Date 2025-01-23
Owner Raytheon Company (USA)
Inventor
  • Harris, Micky
  • Willis, Magathi J.

Abstract

An interface BIT failure detection circuit includes a sequencing circuit and a multiplexer. The sequencing circuit configured to generate the sequence selection signal. The multiplexer is in signal communication with the sequencing circuit, and includes a plurality of interface input. Each interface input corresponds to an interface of a device under test. The sequence selection signal is configured to control the MUX to sequentially select each of the interface inputs. The MUX includes an output terminal configured to output a test signal configured to indicate whether or not at least one fault corresponding to one or more of the interface inputs or a main power supply exists.

IPC Classes  ?

  • G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer

95.

AIR GUN SHOCK TEST APPARATUS

      
Application Number 18354992
Status Pending
Filing Date 2023-07-19
First Publication Date 2025-01-23
Owner Raytheon Company (USA)
Inventor
  • Vo, Peter H.
  • Klensin, Michael
  • Esplin, Roger C.
  • Elmer, Steven Alejandro
  • Henderson, James Paul

Abstract

A test assembly and method for performing a shock test of an article includes a pneumatic gun assembly, a Hopkinson bar assembly, a magnetic catch, and a support assembly. The support assembly suspends the article in alignment with the magnetic catch. The magnetic catch retains the article against the Hopkinson bar assembly. The pneumatic gun assembly includes a striker for propagating a shock through the Hopkinson bar assembly into the article.

IPC Classes  ?

  • G01M 7/08 - Shock-testing
  • G01N 3/307 - Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force generated by a compressed or tensile-stressed springInvestigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force generated by pneumatic or hydraulic means

96.

ELECTRONIC DEVICE TRACKING OR VERIFICATION

      
Application Number 18355957
Status Pending
Filing Date 2023-07-20
First Publication Date 2025-01-23
Owner Raytheon Company (USA)
Inventor
  • Hoffman, Colby K.
  • Angelo, Nick
  • Reid, Cheryl
  • Austin, Sr., Steven J.
  • Hird, Trevor B.
  • Moholt, Michelle

Abstract

Systems, devices, and methods for device or bio-organism authenticity verification are provided. A method can include identifying (i) respective challenges indicating respective stimuli and (ii) a root node hash value, generating the respective stimuli, recording respective responses to the respective electrical stimuli, hashing the respective responses resulting in respective hashed responses, hashing a combination of hashed responses of the respective hashed responses resulting in a key, and comparing the key to the root node hash value.

IPC Classes  ?

  • H04L 9/32 - Arrangements for secret or secure communicationsNetwork security protocols including means for verifying the identity or authority of a user of the system
  • H04L 9/08 - Key distribution

97.

Channel based configurable CML, LVDS, open drain output

      
Application Number 18223371
Grant Number 12328118
Status In Force
Filing Date 2023-07-18
First Publication Date 2025-01-23
Grant Date 2025-06-10
Owner Raytheon Company (USA)
Inventor
  • Willis, Magathi
  • Harris, Micky R.

Abstract

A configurable driver is presented, comprising: a first transistor of a first type coupled to a first node; a second transistor of the first type coupled to a second node; a first transistor of a second type coupled to the first node; a second transistor of a second type coupled to the second node; a first multiplexer coupled to a gate of the first transistor of the first type; a second multiplexer coupled to a gate of the second transistor of the first type; a third multiplexer coupled to a gate of the first transistor of the second type; a fourth multiplexer coupled to a gate of the second transistor of the second type; and one or more switching devices coupled between the first node and the second node.

IPC Classes  ?

  • H03K 19/0175 - Coupling arrangementsInterface arrangements

98.

AIR GUN SHOCK TEST APPARATUS

      
Application Number US2024028624
Publication Number 2025/019055
Status In Force
Filing Date 2024-05-09
Publication Date 2025-01-23
Owner RAYTHEON COMPANY (USA)
Inventor
  • Vo, Peter, H.
  • Klensin, Michael
  • Esplin, Roger, C.
  • Elmer, Steven Alejandro
  • Henderson, James Paul

Abstract

A test assembly and method for performing a shock test of an article includes a pneumatic gun assembly, a Hopkinson bar assembly, a magnetic catch, and a support assembly. The support assembly suspends the article in alignment with the magnetic catch. The magnetic catch retains the article against the Hopkinson bar assembly. The pneumatic gun assembly includes a striker for propagating a shock through the Hopkinson bar assembly into the article.

IPC Classes  ?

99.

ELECTRO-MECHANICAL QUICK CONNECTOR WITH INTEGRAL ACCESS TOOL

      
Application Number US2024028626
Publication Number 2025/019056
Status In Force
Filing Date 2024-05-09
Publication Date 2025-01-23
Owner RAYTHEON COMPANY (USA)
Inventor Leapley, Brian, D.

Abstract

An electro-mechanical tool includes a handheld housing, an electrical cable, and an electro-mechanical head. The electro-mechanical head includes an electrical connector and a tool subassembly. The electrical connector includes pins, each pin connected to a lead of the electrical cable. The tool subassembly includes a bit attached to a cap, which is distally located relative to the electrical connector. The bit can be employed to remove the access cover of an electrical receptacle in the body of a munition such as a missile. The electrical connector can be adapted to transfer power and data to the munition via the electrical receptacle.

IPC Classes  ?

  • F42C 17/04 - Fuze-setting apparatus for electric fuzes
  • H01R 13/627 - Snap-action fastening
  • H01R 13/24 - Contacts for co-operating by abutting resilientContacts for co-operating by abutting resiliently mounted
  • H01R 13/52 - Dustproof, splashproof, drip-proof, waterproof, or flameproof cases
  • H01R 24/38 - Two-part coupling devices, or either of their cooperating parts, characterised by their overall structure having concentrically or coaxially arranged contacts
  • H01R 24/86 - Parallel contacts arranged about a common axis

100.

INTEGRATED CIRCUIT OUTPUTS WITH SWITCHED SOURCE FOLLOWERS TO SUPPORT VARIABLE OUTPUT LEVELS WITHOUT DEDICATED SUPPLIES

      
Application Number 18354034
Status Pending
Filing Date 2023-07-18
First Publication Date 2025-01-23
Owner Raytheon Company (USA)
Inventor
  • Harris, Micky R.
  • Willis, Magathi J.

Abstract

An apparatus includes an output circuit configured to level-shift an incoming signal and generate an output signal having a voltage range different than a voltage range of the incoming signal. The output circuit includes an output driver configured to receive the incoming signal and generate the output signal at a specified voltage level. The output circuit also includes a switched source follower coupled to the output driver. The switched source follower is configured to receive the incoming signal and set the specified voltage level. The switched source follower may include first and second transistors, and the output driver may include a third transistor. The first and third transistors may be configured to be driven by the incoming signal. The second transistor may be configured to be driven by a gate voltage, and the specified voltage level for the output driver may be based on the gate voltage.

IPC Classes  ?

  • H03K 19/0185 - Coupling arrangementsInterface arrangements using field-effect transistors only
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