Rtx Corporation
États‑Unis d’Amérique
Nouveaux brevets et marques déposées la semaine dernière
Dernière mise à jour : 2026-08-01
Sommaire
Brevets |
Marques |
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29 | 0 |
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Viewing 1 - 31 of 31
marques
brevets
| # | ID | Juridiction | Title |
|---|---|---|---|
| 1 | 19041802 |
|
Variable Vane Lever Arm |
| 2 | 19039976 |
|
AIRCRAFT PROPULSION SYSTEM WITH MODULAR OPEN PROPULSOR ROTOR ASSEMBLY |
| 3 | 19041812 |
|
Variable Vane Lever Arm |
| 4 | 19041823 |
|
Variable Vane Lever Arm |
| 5 | 19041827 |
|
Variable Vane Lever Arm |
| 6 | 19039926 |
|
MIXTURE SEPARATION IN BOTTOMING CYCLE |
| 7 | 19036670 |
|
COLD SPRAYING COATING ONTO TURBINE ENGINE COMPONENT |
| 8 | 19041671 |
|
LASER ETCHED CERAMIC-CONTAINING MATERIALS |
| 9 | 19041609 |
|
CERAMIC MATRIX COMPOSITE BLADE OUTER AIR SEAL FEATHER SEAL CONFIGURATION AND METHOD |
| 10 | 19036644 |
|
DEPOSITION OF MATERIAL ONTO CERAMIC MATRIX COMPOSITES |
| 11 | 19037271 |
|
PROPULSION SYSTEM WITH ADJUSTABLE CORE INLET GUIDE VANE |
| 12 | 19041780 |
|
EXTERNALLY SOURCED COOLING FOR PROBE AND LEAD AND METHOD OF DELIVERY |
| 13 | 19041756 |
|
ENVELOPED MIXTURE OF EXPERTS MODEL |
| 14 | 19041080 |
|
DUAL PASSAGE HEAT EXCHANGER FOR REDUCING COLD WALL STRESS AND METHOD THEREOF |
| 15 | 19036744 |
|
TARGETED LOCATION CORRECTION OF THERMAL BARRIER COATED DIFFUSERS |
| 16 | 19429243 |
|
REPAIR OF CERAMIC VANE USING OVER-WRAP FIBER PLY AND RE-STAGGER |
| 17 | G12692797 |
|
Ceramic matrix composite seal repair |
| 18 | 19037990 |
|
REPAIR OF CERAMIC MATRIX COMPOSITE GAS TURBINE ENGINE ARTICLE WITH MONOLITHIC CERAMIC REPAIR ELEMENT |
| 19 | 19040548 |
|
METHODS AND SYSTEMS FOR UTILIZING BLOCKCHAIN FOR MANUFACTURING METADATA AND PRODUCTION DATA |
| 20 | 19036631 |
|
COLD SPRAYING COATING ONTO TURBINE ENGINE COMPONENT |
| 21 | 19037272 |
|
AIRCRAFT PROPULSION SYSTEM WITH AUXILIARY FLOWPATH SYSTEM |
| 22 | 19040447 |
|
STABILITY OF MACHINING OF THIN-WALL PARTS |
| 23 | 19037229 |
|
AIRCRAFT PROPULSION SYSTEM WITH ACOUSTIC TREATMENT ALONG BYPASS FLOWPATH |
| 24 | 19041722 |
|
COMPLIANT BROACH FIXTURE DESIGN TO SUPPORT MORE REPRESENTATIVE FAN BLADE BIRD IMPACT DESIGN |
| 25 | 19040667 |
|
ARTICULATED PROXIMITY MEASUREMENT |
| 26 | 19575422 |
|
OPEN ROTOR GAS TURBINE ENGINE WITH ADAPTIVE TURBINE CLEARANCE CONTROL SYSTEM AND METHOD |
| 27 | 19644125 |
|
FAN EXIT GUIDE VANE WITH LOAD CARRYING TENSION MEMBER |
| 28 | US2025037868 |
|
LASER TEXTURING OF PISTON SEAL GROOVES |
| 29 | US2026012347 |
|
SLURRY INFILTRATION PROCESS |
| 30 | G12693016 |
|
Mesh based fuel flow guide |
| 31 | G12693015 |
|
Combustor liner having cooling ring with fin having space filling curve |
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