This charging system is connected between the two terminals of at least one capacitor in the input of a plurality of power converters and charges the capacitor when a first switching element and a second switching element are turned off.
The present disclosure intends to improve energy efficiency. A biomass gasifier (10) includes: a biomass gasification furnace (11) that produces a biomass gas from biomass fuel and a gasifying agent; a filter (13) that separates char from the biomass gas discharged from the biomass gasification furnace (11); and a char cooler (16) that performs heat exchange between the char separated by the filter (13) and at least a part of the gasifying agent to be supplied to the biomass gasification furnace (11) and heats the gasifying agent.
C10B 57/00 - Other carbonising or coking processesFeatures of destructive distillation processes in general
C10B 53/02 - Destructive distillation, specially adapted for particular solid raw materials or solid raw materials in special form of cellulose-containing material
C10L 3/00 - Gaseous fuelsNatural gasSynthetic natural gas obtained by processes not covered by subclasses , Liquefied petroleum gas
F01K 7/16 - Steam engine plants characterised by the use of specific types of enginePlants or engines characterised by their use of special steam systems, cycles or processesControl means specially adapted for such systems, cycles or processesUse of withdrawn or exhaust steam for feed-water heating the engines being only of turbine type
A power module according to the present disclosure comprises: a circuit board disposed on a main surface of a base plate; a main terminal part capable of inputting power to a circuit pattern of the circuit board; an output terminal part capable of outputting the power converted by a power semiconductor element connected to the circuit pattern; a case having a side wall part that while being disposed on the main surface, surrounds the circuit board in a main surface-widening direction to define a housing space for housing the circuit board, and a lid part that is disposed on the side wall part to close off the housing space, thereby blocking off the inside of the housing space; an insulating part disposed inside the housing space to bury the circuit board; and an optical detection part disposed in the case and capable of detecting the light generated inside the housing space due to the entrance of the light from a distal end surface. A plurality of distal end surfaces of the optical detection part are arranged side by side along a side edge part of the circuit pattern opposed to an inner surface of the side wall part in the housing space so that an optical detection range includes the side edge part.
G01R 31/311 - Contactless testing using non-ionising electromagnetic radiation, e.g. optical radiation of integrated circuits
G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer
H01L 23/538 - Arrangements for conducting electric current within the device in operation from one component to another the interconnection structure between a plurality of semiconductor chips being formed on, or in, insulating substrates
H01L 25/16 - Assemblies consisting of a plurality of individual semiconductor or other solid-state devices the devices being of types provided for in two or more different subclasses of , , , , or , e.g. forming hybrid circuits
H10F 39/95 - Assemblies of multiple devices comprising at least one integrated device covered by group , e.g. comprising integrated image sensors
4.
METHOD FOR SETTING FLIGHT PATH OF UNMANNED AERIAL VEHICLE
A method for setting a flight path of an unmanned aerial vehicle includes calculating an availability state, in an unmanned aerial vehicle, of artificial satellites based on a positional relationship between the artificial satellites constituting a global navigation satellite system and the unmanned aerial vehicle at any of points in a scheduled path of the unmanned aerial vehicle flying autonomously. The method further includes comparing the availability state calculated and a reference availability state required for flight control of the unmanned aerial vehicle.
G05D 1/80 - Arrangements for reacting to or preventing system or operator failure
G05D 1/248 - Arrangements for determining position or orientation using signals provided by artificial sources external to the vehicle, e.g. navigation beacons generated by satellites, e.g. GPS
G05D 1/646 - Following a predefined trajectory, e.g. a line marked on the floor or a flight path
There are provided an engineering device includes: a storage unit configured to store a virtual data format which is commonly used by a first type of module in which definition data for defining a module installed in a control system is provided as data of a predetermined common format; and an object data generating unit configured to secure a storage area in which details of the virtual data format are reflected in the storage unit on the basis of the virtual data format when an installed module is the first type of module, to write entries indicated by the definition data according to the data format indicated by the definition data of the installed module to the secured storage area, and to write a module name of the installed module to the secured storage area to generate object data.
A turbine rotor blade according to at least one embodiment of the present disclosure comprises a blade root in which a first internal passage extending in a blade height direction is formed and a first opening on one-end side of the first internal passage is formed at the bottom, and an adjustment member attached to the bottom and having formed therein a first through hole overlapping the first opening when viewed from the blade height direction. The first through hole intersects with the first opening when viewed from the blade height direction, and has a first overlapping area that overlaps the first opening and a first non-overlapping area that does not overlap the first opening.
A system includes a hydrogen gas production system and a power generation system. The hydrogen gas production system includes a heated gas supply line configured for flow of a heated gas, a hydrocarbon supply line, a catalytic pyrolysis reactor configured to be in thermal contact with the heated gas of the heated gas supply line and produce a hydrogen containing gas by pyrolyzing a hydrocarbon introduced therein via the hydrocarbon supply line, and a separator configured to extract a hydrogen gas from the hydrogen containing gas discharged from the catalytic pyrolysis reactor. The power generation system includes a heated gas collection line configured to collect the heated gas after the thermal contact with the catalytic pyrolysis reactor and supply the heated gas to the power generation system, and a gas turbine having a combustor configured to burn the hydrogen gas introduced therein from the separator via a hydrogen supply line.
F01K 3/18 - Plants characterised by the use of steam or heat accumulators, or intermediate steam heaters, therein having heaters
C01B 3/26 - Production of hydrogen or of gaseous mixtures containing hydrogen by decomposition of gaseous or liquid organic compounds of hydrocarbons using catalysts
F01K 25/00 - Plants or engines characterised by use of special working fluids, not otherwise provided forPlants operating in closed cycles and not otherwise provided for
A power module of the present disclosure includes a main terminal portion including a first conductor including a P terminal at one end thereof, and a second conductor including an N terminal at one end thereof, connected to a capacitor together with the first conductor, and arranged side by side with the first conductor with a gap interposed therebetween; a circuit board including a power semiconductor element configured to convert a DC voltage from the main terminal portion into an AC voltage; an output terminal portion configured to output an AC voltage from the power semiconductor element; a pair of fastening portions connecting the P terminal and a positive-electrode-side terminal of the capacitor to each other and connecting the N terminal and a negative-electrode-side terminal of the capacitor to each other; a base plate to which the circuit board is fixed; a case fixed to a front surface of the base plate and including an accommodation space accommodating the P terminal, the N terminal, and the pair of fastening portions; and a first insulating portion disposed in the accommodation space and covering a first main surface of the P terminal, a second main surface of the N terminal, and the pair of fastening portions from a side opposite to the base plate, in a state of the gap is filled therewith.
H01L 23/049 - ContainersSeals characterised by the shape the container being a hollow construction and having a conductive base as a mounting as well as a lead for the semiconductor body the other leads being perpendicular to the base
H01L 25/07 - Assemblies consisting of a plurality of individual semiconductor or other solid-state devices all the devices being of a type provided for in a single subclass of subclasses , , , , or , e.g. assemblies of rectifier diodes the devices not having separate containers the devices being of a type provided for in subclass
H02M 7/00 - Conversion of AC power input into DC power outputConversion of DC power input into AC power output
H02M 7/537 - Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters
A combustor that causes compressed air supplied from a compressor to combust together with fuel. The combustor includes at least one fuel nozzle having a fuel flow path for supplying fuel and a purge air flow path for ejecting purge air. The combustor further includes a nozzle-securing part for securing at least one fuel nozzle; and a top hat body located on the outer peripheral side of at least part of the nozzle-securing part. The top hat body has a first internal flow path capable of supplying compressed air to the nozzle-securing part from a space on the outer peripheral side of the top hat body. The nozzle-securing part has a second internal flow path capable of supplying compressed air supplied from the first internal flow path to the purge air flow path of the fuel nozzle.
A control method for a gas turbine combustor including an air-hole plate having a plurality of air holes formed therein, and a plurality of fuel nozzles corresponding to respective ones of the plurality of air holes. The gas turbine combustor is operable to combust a hydrogen fuel and a fuel other than the hydrogen fuel. The air holes include: first air holes having, among passageways from an entry end to an exit end, an inclined passageway extending in a direction inclined with respect to the central axis of the air-hole plate in a region including at least the exit end; and second air holes extending in parallel to the central axis. The fuel nozzles include first fuel nozzles corresponding to respective first air holes, and second fuel nozzles corresponding to respective second air holes. During hydrogen fuel firing, the hydrogen fuel is not supplied to the first fuel nozzles.
F02C 9/40 - Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
F02C 3/22 - Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
F02C 9/32 - Control of fuel supply characterised by throttling of fuel
An acoustic device for a gas turbine combustor includes: a first region positioned at a downstream side of a combustion cylinder, the first region existing at a position which is at least one of a pair of positions across the combustion cylinder in a radial direction of the combustion cylinder; a pair of second regions whose axial-direction position with respect to the combustion cylinder overlaps at least partially with the pair of positions, and whose circumferential-direction position with respect to the combustion cylinder is different from that of the pair of positions, the pair of second regions existing at positions across the combustion cylinder in the radial direction; and a third region positioned at an upstream side of the first region and the second region with respect to the combustion cylinder.
A gas turbine combustor provided with: a combustion cylinder having a combustion chamber and a plurality of through-holes that open to the combustion chamber; a housing disposed peripherally outwards of the combustion cylinder and defining an acoustic attenuation space that communicates with the combustion chamber via the through-holes; an air hole plate having a plurality of air holes and being positioned upstream of the combustion cylinder; a plurality of fuel nozzles respectively corresponding to the air holes; an air passage provided between the inner peripheral surface of the combustion cylinder and the outer peripheral surface of the air hole plate and extending in the axial direction of the combustion cylinder; and an air supply flow path for supplying air flowing outside the combustion cylinder to the acoustic attenuation space. At least one of the through holes is provided directly below the air hole plate in the axial direction.
A joining method using heat fusion includes layering a first joining body and a second joining body having a smaller plane area than the first joining body; and performing heating and pressurization with a heater from a side of the second joining body. The method further includes a resin dam interposed between the second joining body and the heater. The resin dam includes a base body having one of front and back surfaces in contact with the heater and the other of front and back surfaces in contact with the second joining body; and a dam main body extending from a circumferential edge of the base body in a direction away from the base body and having a shape control surface facing a side surface of the second joining body.
B29C 65/00 - Joining of preformed partsApparatus therefor
B29C 65/02 - Joining of preformed partsApparatus therefor by heating, with or without pressure
B29K 105/12 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles
A system operator side computer includes: a supply amount acquirer configured to acquire a maximum suppliable power amount from a power generation operator at a predetermined time later; a demand specifier configured to specify a power demand at the predetermined time later; and a shortage amount calculator configured to calculate a power shortage amount based on the power demand and the maximum suppliable power amount.
H02J 3/14 - Circuit arrangements for ac mains or ac distribution networks for adjusting voltage in ac networks by changing a characteristic of the network load by switching loads on to, or off from, network, e.g. progressively balanced loading
H02J 3/00 - Circuit arrangements for ac mains or ac distribution networks
H02J 3/38 - Arrangements for parallelly feeding a single network by two or more generators, converters or transformers
H02J 13/00 - Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the networkCircuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network
15.
ADDITIVE MANUFACTURED OBJECT PRODUCTION METHOD, AND ADDITIVE MANUFACTURED OBJECT PRODUCTION SYSTEM
An additive manufactured object production method includes: a core portion forming step of additively forming a core portion as an inner portion of an additive manufactured object by stacking first weld beads each size of which is corresponding to a first resolution; and a shell portion forming step of additively forming a shell portion as an outer portion of the additive manufactured object on a surface of the core portion by stacking second weld beads each size of which is corresponding to a second resolution higher than the first resolution after the core portion forming step.
A heating device includes: a heat generator configured to generate heat when supplied with electric power; a first insulator and a second insulator respectively layered on a front surface and a back surface of the heat generator and covering the heat generator; a first heat transfer body layered on the first insulator so as to cover the first insulator and a second heat transfer body layered on the second insulator and covering the second insulator; and a circumferential edge structure configured to seal circumferential edges of the first insulator and the second insulator. In the circumferential edge structure, the circumferential edges are sealed by direct or indirect joining of the first heat transfer body and the second heat transfer body.
H05B 3/26 - Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor mounted on insulating base
H05B 3/14 - Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material the material being non-metallic
H05B 3/16 - Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor the conductor being mounted on an insulating base
A takeoff and landing pad apparatus for an unmanned aerial vehicle includes: a pad including a takeoff and landing surface; a mooring mechanism configured to moor the unmanned aerial vehicle on the pad; a drive source configured to rotate the pad together with the mooring mechanism; and a controller configured to control operation with the mooring mechanism and the drive source. The controller drives, based on information about a wind direction to be acquired, the drive source to rotate such that a nose of the unmanned aerial vehicle on the takeoff and landing surface faces the wind direction.
A gas turbine includes a combustor that can combust fuel, which can be heated by a heater, by mixing the fuel with compressed air generated by a compressor. The compressor includes an inlet guide vane for adjusting an amount of intake air. When a deviation between the temperature of the fuel at an outlet section of the heater and a set temperature of the heater exceeds a threshold value, the gas turbine control device controls the opening degree of the inlet guide vane to become larger than the opening degree when the deviation is equal to or smaller than the threshold value.
This inspection device includes an infrared acquisition unit for acquiring infrared light detected by an infrared camera for detecting infrared light from an inspected object that includes an electroconductive member, an intensity-determining unit for determining the detection intensity of the infrared light, and a scratch-determining unit for determining whether or not there is a scratch on the electroconductive member on the basis of the detection intensity of the infrared light.
A turbine blade includes a blade part and an oscillator mounted on the blade part and configured to vibrate the blade part. The blade part may be formed with a hollow part, and the oscillator may be mounted inside the hollow part. The turbine blade may be a stator blade, and the blade part may include a blade and a blade ring supporting the blade.
F01D 25/00 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
F01D 1/04 - Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor traversed by the working-fluid substantially axially
F01D 1/10 - Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor having two or more stages subjected to working-fluid flow without essential intermediate pressure change, i.e. with velocity stages
Regarding a method of collecting a target object falling through the air by using an unmanned aerial vehicle, the method including: an information transmission step of transmitting state information of the target object falling through the air from the target object; and a collection step of capturing the target object by an unmanned aerial vehicle flying in accordance with command information generated based on the state information.
An inspection device includes a base facing, in a first direction, a surface to be inspected, a contact section mounted on the base and configured to contact with a seal on the surface, a biasing device mounted on the base and configured to bias the contact section in a second direction, and a reciprocating mechanism at an end portion of the base on the one side and configured to move the base in the second direction. The biasing device includes a rotary shaft extending in a third direction, an arm being rotatable about the rotary shaft, extending at both sides in the second direction with respect to the rotary shaft, and included with the contact section at an end portion on the one side, and a biasing member at an end portion of the arm on the other side and configured to move the contact section in the second direction.
A metal-air battery system includes: an inlet chamber into which an electrolyte solution flows; an outlet chamber from which the electrolyte solution flows out; a hollow outer electrode having an interior space via which the inlet chamber and the outlet chamber communicate with each other; and an inner electrode disposed to be inserted into the interior space concentrically with the outer electrode. One of the outer electrode and the inner electrode is a negative electrode containing metal, and the other is a porous positive electrode allowing oxygen to diffuse. A flow path through which the electrolyte solution flows from the inlet chamber toward the outlet chamber is formed between the outer electrode and the inner electrode, and the flow path is configured such that a flow-path cross-sectional area thereof decreases from a side of the inlet chamber toward a side of the outlet chamber.
H01M 12/06 - Hybrid cellsManufacture thereof composed of a half-cell of the fuel-cell type and of a half-cell of the primary-cell type with one metallic and one gaseous electrode
AUTOMATIC TAKEOFF/LANDING SYSTEM FOR VERTICAL TAKEOFF/LANDING AIRCRAFT, VERTICAL TAKEOFF/LANDING AIRCRAFT, AND CONTROL METHOD FOR TAKEOFF/LANDING OF VERTICAL TAKEOFF/LANDING AIRCRAFT
This automatic takeoff/landing system for a vertical takeoff/landing aircraft comprises: a relative wind information acquisition unit that acquires the direction of relative wind at a moving object; and a control unit that executes takeoff/landing control to cause the vertical takeoff/landing aircraft to takeoff/land at a landing target point provided on the moving object. The control unit, during takeoff/landing of the vertical takeoff/landing aircraft, executes the takeoff/landing control on the basis of the direction of the relative wind acquired by the relative wind information acquisition unit, in a state in which the aircraft heading of the vertical takeoff/landing aircraft is caused to face the direction of the relative wind.
A seal application method of applying a sealing material in a narrow portion serving as a hollow portion being formed inside a target object and communicating with outside, the seal application method including: arranging the target object such that a target surface inside the narrow portion faces downward; forming a brush coat by inserting into the narrow portion a brush coating device including at an upper portion thereof a brush portion with the sealing material adhered thereto, pressing the brush portion upward and rubbing the brush portion against the target surface, thereby applying the sealing material to the target surface; after forming the brush coat, inverting the target object such that the target surface faces upward; and, after inverting the target object, forming an edge seal being thicker than the brush coat by inserting an edge sealing device into the narrow portion and causing the edge sealing device to apply the sealing material onto the brush coat from above.
A sealant forming nozzle is a sealant forming nozzle that forms sealant by being moved along a target surface, and includes: a main body portion covering the target surface and forming a cavity, the cavity including an opening that opens only toward a rear side in a movement direction and a closing surface provided on a front side in the movement direction; and a discharge hole that is formed in the main body portion and guides a sealing material supplied from outside into the cavity. The closing surface extends so as to approach the target surface toward the front side in the movement direction in a cross-sectional view in a direction orthogonal to the movement direction and along the target surface.
B05C 17/005 - Hand tools or apparatus using hand-held tools, for applying liquids or other fluent materials to, for spreading applied liquids or other fluent materials on, or for partially removing applied liquids or other fluent materials from, surfaces for discharging material through an outlet orifice by pressure
An anthraquinone-based active material for a redox flow battery includes a first compound represented by the following chemical formula:
An anthraquinone-based active material for a redox flow battery includes a first compound represented by the following chemical formula:
where at least one of the R1 to R8 is a hydroxy group, and at least one of the R1 to R8 is an alkoxy group.
Provided is a method for quantitatively diagnosing damage to TBC. A diagnosis method is a method for diagnosing a damage state of a coating material coated on a surface of a member and includes: a step of setting a diagnosis target portion in an image obtained by capturing the surface of the member; a step of specifying a reference portion in the image; a step of individually calculating L*a*b* values of the diagnosis target portion and the reference portion; a step of calculating a color difference between the L*a*b* values of the diagnosis target portion and the L*a*b* values of the reference portion; and a step of diagnosing the damage state of the diagnosis target portion from the color difference.
A pressing device includes: a plurality of pressing portions each configured to generate a pressing force toward a treatment target surface facing in a first direction and arranged in a direction intersecting the first direction; and an interlocking mechanism configured to interlock the plurality of pressing portions and control a pressing amount of each of the pressing portions in the first direction. For example, each of the pressing portions is a fluid device configured to be deformed by a pressure of an internal fluid to generate the pressing force in the first direction, and the interlocking mechanism includes a fluid supply portion configured to supply a fluid to a plurality of the fluid devices and a plurality of speed control valves provided for the respective plurality of the fluid devices and configured to adjust a supply rate of the fluid to each of the fluid devices.
B30B 15/16 - Control arrangements for fluid-driven presses
B30B 15/24 - Control arrangements for fluid-driven presses controlling the movement of a plurality of actuating members to maintain parallel movement of the platen or press beam
A repair device includes a casing having a box shape, being open in a first direction, and extending in a second direction intersecting the first direction, a brush device housed in the casing from the first direction, and a jack unit positioned between a bottom surface of the casing and the brush device and configured to adjust a position of the brush device in the first direction relative to the bottom surface of the casing, in which the brush device includes a base, a guide positioned at a fixed position relative to the base and protruding from an opening in the casing in the first direction, multiple brushes attached to the base, protruding from the opening in the casing in the first direction beyond the guide, and configured to apply sealant to a surface to be treated facing the first direction, and an actuator configured to adjust positions of the multiple brushes in a third direction intersecting the first direction and the second direction by moving the base in the third direction.
B29C 73/02 - Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass using liquid or paste-like material
B29C 73/24 - Apparatus or accessories not otherwise provided for
A method of producing an anthraquinone-based substance represented by the following chemical formula:
A method of producing an anthraquinone-based substance represented by the following chemical formula:
A method of producing an anthraquinone-based substance represented by the following chemical formula:
where at least one of R1 to R8 is a hydroxy group, and at least one of R1 to R8 is an alkoxy group, includes the steps of: preparing a starting material represented by the following chemical formula:
A method of producing an anthraquinone-based substance represented by the following chemical formula:
where at least one of R1 to R8 is a hydroxy group, and at least one of R1 to R8 is an alkoxy group, includes the steps of: preparing a starting material represented by the following chemical formula:
A method of producing an anthraquinone-based substance represented by the following chemical formula:
where at least one of R1 to R8 is a hydroxy group, and at least one of R1 to R8 is an alkoxy group, includes the steps of: preparing a starting material represented by the following chemical formula:
where at least two of the R1′ to R8′ are hydroxy groups; and reacting the starting material with an organic alkylating agent. The amount of the organic alkylating agent to be reacted with the starting material is more than or equal to 0.05 mol and less than n mol per 1 mol of the starting material, where n is the number of hydroxy groups contained in the starting material.
A gas turbine control device according to at least one embodiment of the present disclosure comprises a purge gas flow rate control unit that controls the flow rate of purge gas for discharging fuel gas remaining inside the gas turbine to the outside of the gas turbine. The purge gas flow rate control unit controls the flow rate of the purge gas on the basis of a parameter related to the intake air quantity from a gas turbine inlet.
Provided is a turbine static blade composed of a blade body and shrouds respectively formed on both ends in the blade height direction of the blade body. The shroud includes: a main member having a heat-resistance coat film section which extends from the axial upstream end to the axial downstream end of a gas passing surface; and a protruding section which protrudes from a side end section on the front edge side of the main member toward the axial upstream side. The protruding section comprises a plurality of cooling paths which are disposed in an annular shape at predetermined intervals in the circumferential direction, and connect an inlet opening which is formed in an inner circumferential surface of the protruding section and an inner surface of the main member, and an outlet opening which is formed in an outer circumferential surface of the protruding section.
A method for calculating an SN ratio gain, in which the magnitude level of the SN ratio gain based on an orthogonal array size for each unit space in a multi-MT method is corrected. The method for calculating an SN ratio gain involves creating a plurality of unit spaces by using data detected by a plurality of sensors provided to a plant, and evaluating the state of the plant using the unit spaces by a multi-MT method, and includes: a step for allocating, for each of the unit spaces, one of the sensors used for creating the unit space to a 2-level orthogonal array, and generating orthogonal arrays for the respective unit spaces; a step for calculating, for each of the orthogonal arrays for the respective unit spaces, an SN ratio for each line of the orthogonal array; and a step for calculating an SN ratio gain.
In a method of transporting cargo suspended by multiple UAVs, each of the multiple UAVs flies such that a relative positional relationship of each of the multiple UAVs to the cargo is maintained. This method of transporting cargo is achieved by one or both of a ground position control mode in which flight of each of the multiple UAVs is controlled to follow a change in a position of the cargo relative to the ground, and an interval control mode in which the flight of each of the multiple UAVs is controlled so as to maintain an interval of each of the multiple UAVs to the cargo.
G05D 1/695 - Coordinated control of the position or course of two or more vehicles for maintaining a fixed relative position of the vehicles, e.g. for convoy travelling or formation flight
G05D 1/248 - Arrangements for determining position or orientation using signals provided by artificial sources external to the vehicle, e.g. navigation beacons generated by satellites, e.g. GPS
G05D 105/20 - Specific applications of the controlled vehicles for transportation
A CO2 recovery device includes: a cooling tower into which an exhaust gas containing carbon dioxide is introduced to cool the exhaust gas; and an absorption tower into which the exhaust gas cooled in the cooling tower is introduced and which brings the exhaust gas into contact with an absorption liquid to remove the carbon dioxide from the exhaust gas, in which the absorption tower has an absorption tower body through which the exhaust gas is flowable and which has a tubular shape, and a demister that is disposed inside the absorption tower body and is configured to remove mist contained in the exhaust gas as the exhaust gas flows therethrough, and the CO2 recovery device further comprises a flow velocity regulating section that regulates the flow velocity of the exhaust gas flowing through the demister to be within a predetermined range.
B01D 53/14 - Separation of gases or vapoursRecovering vapours of volatile solvents from gasesChemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases or aerosols by absorption
A rotor blade including: a blade body extending in a blade height direction that is a direction perpendicular to an airfoil cross-section; and a platform provided to an end at a hub side, from between a tip side and the hub side which are of the blade height direction. The blade body includes: an anterior edge and a posterior edge; a ventral surface and a dorsal surface linking the anterior edge and the posterior edge together; and a cooling passage extending in the blade height direction between the ventral surface and the dorsal surface. The ventral/dorsal wall thickness ratio at any position between the hub-side position and the middle position in the cooling passage is smaller than the ventral/dorsal wall thickness ratio at any position between the middle position and the tip-side position.
An electric propulsion device includes a hollow shaft having a shaft flow path, which extends in a direction of an axis, formed therein, a boss portion having a space formed therein, a plurality of blades having a blade flow path, which communicates with the space of the boss portion, formed therein, an electric motor, and a casing having an accommodation space, which communicates with the shaft flow path, formed therein. A suction port is formed to communicate between an outside of the casing and the accommodation space, in a position of the casing between each of the plurality of blades and the electric motor. A blowing port is formed to communicate between the blade flow path and the outside, in a region including an end portion of each of the plurality of blades on an outer side in the radial direction.
H02K 9/06 - Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium with fans or impellers driven by the machine shaft
B64D 27/30 - Aircraft characterised by electric power plants
H02K 5/20 - Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
H02K 7/00 - Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
H02K 21/14 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures
39.
ADDITIVE MANUFACTURING METHOD AND ADDITIVE MANUFACTURING DEVICE
An additive manufacturing method according to one or more embodiments includes a step for feeding a raw-material powder and forming a layer of the raw-material powder and a step for irradiating the layer with a light beam to cause the raw-material powder in the layer to melt and solidify, and thereby molding a part of a molded object. In the molding step, the beam diameter of the light beam on the molding surface is changed partway through molding, within the same layer.
A gas turbine includes a purge gas supply system for supplying purge gas to a fuel oil injection nozzle for injecting fuel oil to a combustion chamber. A gas turbine control device sets a supply pressure target value of purge gas, based on the operating state acquired from the gas turbine, and controls a purge gas supply pressure adjustment part so that supply pressure of purge gas becomes the supply pressure target value. The increase rate of the supply pressure target value is limited to be less than or equal to an increase rate upper limit. The increase rate upper limit is corrected so that the increase rate upper limit is increased when it is determined that the correction is necessary based on the operating state.
A composite material structure includes a composite material including a carbon fiber and a resin; a conductive primer including a carbon nanofiber and applied at least on a surface of the edge of the composite material; and a conductive sealant including a conductive material and applied on the surface of the conductive primer.
B05D 7/00 - Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
An electrolytic cell according to the present disclosure includes: a first separator; a second separator disposed with a space between the second separator and the first separator; an ion exchange membrane disposed between the first separator and the second separator and configured to partition at least part of the space into an anode chamber and a cathode chamber; and a sealing part disposed between the first separator and the second separator, located on an outer side from an outer edge portion of the ion exchange membrane, and configured to seal the space.
An electric fan includes: an electric motor that includes an output shaft extending along an axis line and a tubular housing centered on the axis line; an inner duct provided on a downstream side of the electric motor; a plurality of blades mounted on the output shaft; and a cooling member having a plurality of fins provided on an outer peripheral surface of the housing.
A manufacturing model creation device includes: a unit configured to create, on the basis of a design model as design information of a completed product to be manufactured by assembling a plurality of components, a plan model in which instruction information for manufacturing necessary for assembling the components is set for each of the components; and a unit configured to create a manufacturing model including a manufacturing instruction for a manufacturing target component by extracting component information of the manufacturing target component from the design model and adding, to the component information extracted, the instruction information of the manufacturing target component extracted from the plan model.
G06F 30/12 - Geometric CAD characterised by design entry means specially adapted for CAD, e.g. graphical user interfaces [GUI] specially adapted for CAD
A waste treatment facility includes a storage unit configured to store waste, at least one treatment facility configured to perform intermediate treatment of part of the waste stored in the storage unit, a hydrothermal treatment device configured to hydrolyze remaining part of the waste stored in the storage unit with steam to produce a modified substance, and a treatment condition setting device configured to acquire process data of the hydrothermal treatment device, estimate an index for setting a treatment condition for intermediate treatment of the waste in the at least one treatment facility in accordance with the process data, and set the treatment condition in accordance with the index.
A turbine stator vane according to at least one embodiment of the present disclosure comprises an airfoil, an inner shroud provided on the inner-peripheral side of the airfoil, and an outer shroud provided on the outer-peripheral side of the airfoil. The inner shroud has a first recess formed in the surface on the side opposite the airfoil across a gas path surface of the inner shroud. The outer shroud has a second recess formed in the surface on the side opposite the airfoil across a gas path surface of the outer shroud, and at least one outer passage that communicates with the second recess and does not communicate with the space inside the airfoil. The number of outer passages is greater than the number of inner passages that communicate with the first recess in the inner shroud and do not communicate with the space inside the airfoil.
A gas turbine plant includes a gas turbine, a liquefaction facility capable of liquefying air, and a liquefaction controller. A compressor has an intake amount adjuster capable of adjusting an intake amount into a compressor casing. The liquefaction facility includes: a bleed line capable of bleeding compressed air from the compressor; a liquefaction system capable of liquefying the compressed air, a bleed amount adjustment valve; a return air line capable of guiding return air into a flow passage through which compressed air flows in the gas turbine; and a return amount adjusting valve. The liquefaction controller opens the bleed amount adjustment valve if an opening degree of the intake amount adjuster is a first opening degree, and opens the return amount adjusting valve if the opening degree of the intake amount adjuster is a second opening degree, which is an opening degree greater than the first opening degree.
F02C 9/18 - Control of working fluid flow by bleeding, by-passing or acting on variable working fluid interconnections between turbines or compressors or their stages
F02C 6/18 - Plural gas-turbine plantsCombinations of gas-turbine plants with other apparatusAdaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
F02C 7/141 - Cooling of plants of fluids in the plant of working fluid
F25J 1/00 - Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
F25J 1/02 - Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen
48.
FUEL SUPPLY METHOD, FUEL SUPPLY SYSTEM, FUEL COMBUSTION SYSTEM PROVIDED WITH FUEL SUPPLY SYSTEM, AND GAS TURBINE PLANT
Provided is a fuel supply system including a main ammonia line through which liquid ammonia flows; a vaporizer connected to an end of the main ammonia line and configured to heat and vaporize the liquid ammonia via heat exchange between a heating medium and the liquid ammonia; a gaseous ammonia line connected to the vaporizer, the gaseous ammonia line configured to guide a gaseous ammonia, which is ammonia vaporized by the vaporizer, as fuel to a combustor of a gas turbine; a liquid ammonia line configured to guide liquid ammonia which has not undergone heat exchange with the heating medium at the vaporizer as fuel to the combustor; and a switching device configured to switch an ammonia supply state between a first state in which the gaseous ammonia is guided from the gaseous ammonia line to the combustor and a second state in which the liquid ammonia is guided from the liquid ammonia line to the combustor.
F02C 3/22 - Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
F02C 7/224 - Heating fuel before feeding to the burner
A turbine blade includes a blade body, cooling passages extending in the blade height direction inside the blade body and connected to each other via folded portions, and a bypass portion that is provided in a partition wall portion partitioning a pair of adjacent cooling passages and that allows the pair of cooling passages to communicate with each other. The pair of cooling passages includes an upstream passage and a downstream passage. The turbine blade is provided with: a plurality of cooling holes formed in the blade body so as to be arranged along the blade height direction, that communicate with the downstream passage, and open in the surface of the blade body; a plurality of turbulators provided on the inner wall surface of the downstream passage and arranged along the blade height direction; or a thermal barrier coating that covers the surface of the blade body.
A reefer container configured to cool a gas inside a container body, including: the container body; a circulation line with a suction port and a blowout port each of which is disposed inside the container body; a compressor disposed in the circulation line and configured to compress the gas suctioned from inside the container body to the circulation line through the suction port; a heat exchanger disposed in the circulation line and configured to cool the gas compressed in the compressor; an expander disposed in the circulation line and configured to expand the gas cooled in the heat exchanger; and a liquefied gas tank housed inside the container body and configured to store a liquefied gas.
F25B 1/00 - Compression machines, plants or systems with non-reversible cycle
F25D 11/00 - Self-contained movable devices associated with refrigerating machinery, e.g. domestic refrigerators
52.
MONITORING AND CONTROL DEVICE FOR ROTATING MACHINE, ROTATING MACHINE EQUIPMENT, MONITORING AND CONTROL METHOD FOR ROTATING MACHINE, AND MONITORING AND CONTROL PROGRAM FOR ROTATING MACHINE
A monitoring and control device for monitoring or controlling the clearance of a rotating machine including a vehicle cabin containing rotating and stationary parts comprises: an acquisition unit configured to acquire a plurality of temperatures at a plurality of locations in the vehicle cabin; and an index calculation unit configured to calculate an index indicating the vertical displacement of the vehicle cabin on the basis of the plurality of temperatures.
F01D 21/00 - Shutting-down of machines or engines, e.g. in emergencyRegulating, controlling, or safety means not otherwise provided for
F01D 21/12 - Shutting-down of machines or engines, e.g. in emergencyRegulating, controlling, or safety means not otherwise provided for responsive to temperature
F01D 25/10 - Heating, e.g. warming-up before starting
Provided are a threat-countering system and a threat-countering method for efficiently countering incoming threats by using laser irradiation. The threat-countering system comprises a countering device, a deterrent device, and a decision device. The countering device detects incoming threats and counters the threats by using laser irradiation. The deterrent device is installed to prevent threats from approaching a protected object through a deterrent region in which the power of the laser irradiation is assumed to be lower than a predetermined threshold. The decision device decides the position of the upper end of the deterrent device on the basis of the upper end of the deterrent region.
Provided are a target tracking device that efficiently tracks a target, a target tracking method, and a recording medium for storing a target tracking program. This target tracking device comprises a determination condition selector and a tracker. The determination condition selector selects a tracking mode for tracking a detected target from among a plurality of tracking modes on the basis of a group of determination conditions related to the position of the target. The tracker tracks the target in the selected tracking mode. The plurality of tracking modes include a first tracking mode that focuses on the vulnerable portion of the target and a second tracking mode that focuses on the center of gravity of the target. The target tracking device further comprises a coping device that irradiates the focused portion of the target with a laser beam to cope with the target.
H04N 23/67 - Focus control based on electronic image sensor signals
G06V 10/98 - Detection or correction of errors, e.g. by rescanning the pattern or by human interventionEvaluation of the quality of the acquired patterns
H04N 23/667 - Camera operation mode switching, e.g. between still and video, sport and normal or high and low resolution modes
A steam turbine according to at least one embodiment of the present disclosure includes an outer casing. The steam turbine according to at least one embodiment of the present disclosure includes an annular member, which is a single member provided radially inward of the outer casing, and formed in the annular member are a seal region in which a sealing device for sealing a gap between said member and the outer peripheral surface of a rotor is located, a rear-stage-stator-vane-holding region where a rear-stage stator vane is held, and an inner casing region connecting the seal region and the rear-stage-stator-vane-holding region. The steam turbine according to at least one embodiment of the present disclosure includes a front-stage vane ring that is attached to the annular member and that holds a front-stage stator vane.
A CO2 recovery system includes: a combustion facility; a CO2 absorption tower that brings an exhaust gas containing CO2, which is discharged from the combustion facility and introduced into the CO2 absorption tower, into contact with a CO2 absorption liquid to remove the CO2 from the exhaust gas; and a decarbonated gas introduction line that is connected to the CO2 absorption tower and the combustion facility and allows at least a portion of a decarbonated gas, which is the exhaust gas from which the CO2 has been removed in the CO2 absorption tower, to be introduced into the combustion facility.
B01D 53/14 - Separation of gases or vapoursRecovering vapours of volatile solvents from gasesChemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases or aerosols by absorption
A production method for fine metal particles includes a step of preparing metal particles and a step of supplying the metal particles with a feed gas containing a hydrocarbon, wherein the contact between the feed gas and the metal particles is carried out at a temperature of 600° C. to 900° C.
B22F 1/05 - Metallic powder characterised by the size or surface area of the particles
B22F 9/04 - Making metallic powder or suspensions thereofApparatus or devices specially adapted therefor using physical processes starting from solid material, e.g. by crushing, grinding or milling
58.
Piping support structure, intake duct, and gas turbine
The support structure of the present disclosure is a piping support structure that supports piping comprising: a header pipe extending in a first direction within a cross section of a duct and having an inlet formed therein through which a high-temperature fluid flows; and a plurality of nozzle pipes integrally provided with the header pipe, extending in a second direction orthogonal to the first direction, and arranged in the first direction. The support structure comprises: ridges protruding from surfaces on at least one side of the outer peripheral surfaces of the nozzle pipes in a third direction orthogonal to the first direction and the second direction; and a support member fixed to the duct and having formed therein a guide groove to which the ridge is fitted and which guides the ridge in the direction of heat extension of the header pipe and the nozzle pipes.
F02C 7/055 - Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
F16L 3/20 - Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets with special provision allowing movement of the pipe allowing movement in transverse direction
This control device comprises: an acquiring unit for acquiring, as a first inlet pressure, a pressure value of first steam on a first inlet side as seen from a first regulating valve of a first turbine that rotates using the first steam, which is supplied from the first inlet via the first regulating valve, and acquiring, as a second inlet pressure, a pressure value of second steam on a second inlet side as seen from a second regulating valve of a second turbine that rotates on the same rotating shaft as the first turbine using the second steam, which is supplied from the second inlet via the second regulating valve; and a control unit for regulating an opening degree of the first regulating valve and an opening degree of the second regulating valve in accordance with the first inlet pressure and the second inlet pressure.
A carbon dioxide recovery system includes an absorption tower, a regeneration tower, a rich liquid line, a lean liquid line, a heat exchange unit, and a warn fluid supply unit. The absorption tower allows a carbon dioxide containing gas containing carbon dioxide to contact an absorption liquid capable of absorbing carbon dioxide and produces a rich liquid corresponding to an absorption liquid having absorbed carbon dioxide of the carbon dioxide containing gas. The regeneration tower heats the rich liquid to discharge carbon dioxide from the rich liquid and produces a lean liquid corresponding to an absorption liquid having discharged carbon dioxide. The rich liquid line guides the rich liquid from the absorption tower to the regeneration tower. The lean liquid line guides the lean liquid from the regeneration tower to the absorption tower. The heat exchange unit exchanges the temperature of the lean liquid flowing through the lean liquid line with the absorption liquid having a temperature different from that of the lean liquid flowing through the lean liquid line. The warm fluid supply unit can supply a warm fluid for warming the heat exchange unit to the heat exchange unit.
B01D 53/14 - Separation of gases or vapoursRecovering vapours of volatile solvents from gasesChemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases or aerosols by absorption
A bearing device supports a rotary shaft that is rotatable about an axis extending in the horizontal direction, and includes: a bearing body which supports the rotary shaft; a support ring having a seating part including a support ring body that covers the bearing body from the outer circumferential side and a downwardly-oriented bottom surface that is provided integrally with the support ring body; and a bearing box which is provided separately from the support ring and which has a supporting surface abutting against the bottom surface. The bearing body has a ring part which covers the rotary shaft from the outer circumferential side; and a lower pad which is directly or indirectly supported by the inner circumferential surface of the ring part and which is slidably in contact with the outer circumferential surface of the rotary shaft.
A magnetic geared electrical machine includes: a stator including a stator coil; a first rotor which includes a plurality of pole pieces arranged with a first radial gap between the stator and the plurality of pole pieces, a first cooling passage including the first radial gap being formed between the first rotor and the stator; a second rotor which includes a plurality of rotor magnets, is arranged opposite to the stator across the first rotor in a radial direction with a second radial gap between the pole pieces and the plurality of rotor magnets, a second cooling passage including the second radial gap being formed between the first rotor and the second rotor; and an inlet cavity for cooling gas formed on one end side in an axial direction with respect to the stator, the first rotor and the second rotor.
A ducted fan device includes: a plurality of fan devices each having a fan configured to be rotated about a first axis to generate an airflow and a cylindrical smaller duct surrounding the fan about the first axis and extending in a first axis direction; and a cylindrical larger duct extending in a second axis direction parallel to the first axis. Each of the fan devices is arranged on an inner side of the larger duct when viewed in the second axis direction. At least a part of the smaller duct is arranged outside the larger duct on an upstream side in a flow direction of an airflow when viewed in a direction orthogonal to the second axis.
The present application relates to a fuel supply device for a gas turbine, which can supply a first fuel and a second fuel having a high combustion speed to a combustor of the gas turbine. In the present device, a first fuel supply line and a second fuel supply line are merged at a merging portion and are connected to the combustor via a mixing line. The second fuel supply line is provided with a first shutoff valve serving as a controlled object when the combustion state is switched from a single fuel combustion state to a mixed fuel combustion state, and a flow meter provided upstream of the first shutoff valve. The flow meter can output a detection value of a flow rate of the second fuel in order to calculate a mixing ratio of the first fuel and the second fuel for monitoring an operating state of the gas turbine.
A CO2 recovery system includes: a combustion facility; a dust collector into which exhaust gas containing CO2, discharged from the combustion facility, is introduced, and which removes solid components from the exhaust gas; an exhaust gas cooling device into which the exhaust gas is introduced, and which cools the exhaust gas through contact with cooling water; a CO2 absorption tower into which the exhaust gas cooled by the exhaust gas cooling device is introduced, and which removes the CO2 from the exhaust gas in contact with a CO2 absorbent; and a cooling water introduction line which is-connected to the exhaust gas cooling device and to a supply site on an upstream side, in the flow of exhaust gas, of the dust collector, and which guides at least a portion of the cooling water inside the exhaust gas cooling device to the supply site.
B01D 53/14 - Separation of gases or vapoursRecovering vapours of volatile solvents from gasesChemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases or aerosols by absorption
66.
POWER GENERATION SYSTEM, CONTROL DEVICE, AND CONTROL METHOD
This power generation system comprises: a gas turbine; a power generator; a first clutch that engages or disengages with the rotation shaft of the gas turbine and the rotation shaft of the power generator; a rotation drive unit that rotationally drives the gas turbine; a control unit that controls the rotation drive unit according to the exhaust temperature of the gas turbine to rotationally drive the gas turbine in a case in which the power generator is operated in synchronous phase modification while the first clutch is in a disengaged state.
F01K 23/06 - Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
F01D 15/10 - Adaptations for driving, or combinations with, electric generators
F01D 19/02 - Starting of machines or enginesRegulating, controlling, or safety means in connection therewith dependent on temperature of component parts, e.g. of turbine casing
67.
RUBBING DETERMINATION DEVICE, RUBBING DETERMINATION METHOD, AND RUBBING DETERMINATION PROGRAM FOR ROTARY MACHINE
This rubbing determination device determines rubbing of a rotary machine which comprises a fixed part and a rotary part. The present device acquires an AE signal detected by means of an AE sensor provided in the rotary machine and acquires a gap amount between the fixed part and the rotary part. A rubbing determination evaluation index is generated on the basis of the AE signal and the gap amount, and rubbing in the rotary machine is determined on the basis of the rubbing determination evaluation index.
An optical connector includes: an optical fiber arranged along an optical axis; a light guide member having a first end face and a second end face and configured to guide a laser beam from the first end face to the second end face, the laser beam emitted along the optical axis from a light source entering the first end face, and the second end face being joined to an incident end face of the optical fiber; and a window member arranged between the light source and the light guide member and configured to guide, to the first end face of the light guide member, the laser beam emitted from the light source. The window member has a first transmission face and a second transmission face, the laser beam emitted from the light source entering the first transmission face, and the second transmission face being configured to emit the laser beam.
G02B 6/12 - Light guidesStructural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
A design method for a target object includes: acquiring information about states of reflection and scattering of electromagnetic waves on a target object in a case in which the electromagnetic waves are irradiated onto the target object; identifying, based on the information, a portion at which predetermined reflection and scattering occur on the target object; changing a surface state of the portion at which the predetermined reflection and scattering occur on the target object so that the predetermined reflection and scattering at the portion at which the predetermined reflection and scattering occur on the target object are suppressed; and verifying states of the predetermined reflection and scattering of the electromagnetic waves on the target object in a case in which the electromagnetic waves are irradiated onto the target object having the changed surface state.
A cooling liquid circulation unit circulates cooling liquid in an immersion tank for immersing and cooling electronic devices in the cooling liquid and includes a flow rate adjustment part provided in a cooling liquid circulation path for circulating the cooling liquid in the immersion tank, a heat exchanger for exchanging heat between the cooling liquid and a cooling medium, the heat exchanger being provided in the cooling liquid circulation path, and a cooling liquid circulation unit controller that includes a mode selection part for selecting any one of a plurality of cooling modes, a calculation part for calculating a necessary cooling amount based on parameters related to operation states of the electronic devices, and a cooling condition setting part for setting a target value of parameters related to the flow rate of the cooling liquid based on the selected cooling mode and the necessary cooling amount.
This supply air demister comprises a duct forming a flow channel through which supply air flows upward from below, and a demister body provided above the duct. The demister body has: a plurality of gutter parts having a receiving surface depressed downward and extending obliquely, and provided side by side at intervals from each other; and a plurality of return parts provided above the gutter parts, having a return surface depressed upward, and provided side by side at intervals from each other. The return parts are configured such that a return surface overlaps with an adjacent receiving surface in the extending direction of the return surface as viewed in the vertical direction.
B01D 45/08 - Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by utilising inertia by impingement against baffle separators
A hydrogen production system and a hydrogen production method include a heat exchanger that heats steam by using a heating medium heated by thermal energy at 600° C. or higher, a high-temperature steam electrolysis device that produces hydrogen by using the steam, and a heating device that heats the high-temperature steam electrolysis device by using the steam.
A redox flow battery includes a series circuit having two or more cell stacks electrically connected in series. Each of the two or more cell stacks includes a cell stack input terminal and a cell stack output terminal. Each of the two or more cell stacks is provided with a bypass circuit that electrically bypasses the cell stack. Each of the bypass circuits includes a bypass circuit input terminal and a bypass circuit output terminal. The redox flow battery includes an input switch that, with respect to each of the two or more cell stacks, switches between the cell stack input terminal and the bypass circuit input terminal and an output switch that, with respect to each of the two or more cell stacks, switches between the cell stack output terminal and the bypass circuit output terminal.
H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
H01M 8/2495 - Grouping of fuel cells, e.g. stacking of fuel cells comprising two or more groupings of fuel cells, e.g. modular assemblies of fuel cells of different types
74.
ADDICTIVE MANUFACTURED OBJECT MANUFACTURING METHOD AND ADDITIVE MANUFACTURING SYSTEM
An addictive manufactured object manufacturing method includes: a shell portion forming step of additively forming a shell portion corresponding to an outer portion of an addictive manufactured object by a shell portion beads formed by weaving welding; and a core portion forming step of additively forming a core portion corresponding to an inner portion of the addictive manufactured object by a core portion bead formed by welding.
According to one embodiment, the present invention provides a rotating-machine casing support structure including: a casing; a built-in component that is disposed inside an interior space of the casing at a lateral side of a rotor and that is supported by the casing; a protruding part that is provided so as to protrude laterally outside of the casing from a side of the casing; and a support part that supports the protruding part laterally outside of the casing.
F01D 25/26 - Double casingsMeasures against temperature strain in casings
76.
METHOD FOR ESTIMATING FLANGE SURFACE PRESSURE DISTRIBUTION IN ROTARY MACHINE, METHOD FOR EVALUATING LEAKAGE OF FLUID FROM BETWEEN FLANGE SURFACES, AND PROGRAM AND DEVICE FOR EXECUTING THESE METHODS
A method for estimating a flange surface pressure distribution includes: a reference model receiving step of receiving a three-dimensional reference shape model of a rotary machine; a measured coordinate receiving step of receiving measured three-dimensional coordinate data at a plurality of positions on an upper flange surface and a lower flange surface when a casing is in an open state; a condition receiving step of receiving a tightening torque and an elastic coefficient of a plurality of bolts, elastic coefficients and weights of an upper-half casing and a lower-half casing, and the like; a modified model creating step of creating a three-dimensional modified shape model by modifying the three-dimensional reference shape model based on the measured three-dimensional coordinate data at the plurality of positions; and a pressure distribution estimating step of obtaining, by using the three-dimensional modified shape model and under the conditions received in the condition receiving step, a pressure distribution of a flange surface in a fastened state.
F01D 21/00 - Shutting-down of machines or engines, e.g. in emergencyRegulating, controlling, or safety means not otherwise provided for
F01D 25/24 - CasingsCasing parts, e.g. diaphragms, casing fastenings
G01M 3/26 - Investigating fluid tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
77.
WING STRUCTURE AND WING STRUCTURE MANUFACTURING METHOD
Provided is a wing structure comprising a wing body formed from fiber-reinforced plastic (FRP), and an erosion suppression layer provided so as to cover at least a portion of a front edge of the wing structure. The erosion suppression layer contains a thermal spraying layer configured so as to maintain, by having a prescribed surface roughness, a liquid film formed on the erosion suppression layer.
This component inspection method includes: a fluid supply step for supplying a fluid to a cooling flow passage of a component internally including said cooling flow passage; a heating step for heating a surface of the component; and a measurement step for measuring a temperature of the surface of the component heated by means of the heating step.
This shaft sealing device comprises: a housing that has a storage groove; a seal body stored in the storage groove; and a projected part that projects from one of the housing and the seal body toward the other in the storage groove in an axial direction. The seal body divides an annular space into a high-pressure region on a first side in the axial direction and a low-pressure region on a second side in the axial direction. The housing has a connection part that connects the low-pressure region with the inside of the storage groove. The projected part divides a portion between an opposite surface and a low-pressure-side lateral surface of the seal body into a first space on the radially outer side and a second space on the radially inner side. The connection part connects the first space with the low-pressure region.
F16J 15/3272 - Mounting of sealing rings the rings having a break or opening, e.g. to enable mounting on a shaft otherwise than from a shaft end
F16J 15/50 - Sealings between relatively-movable members, by means of a sealing without relatively-moving surfaces, e.g. fluid-tight sealings for transmitting motion through a wall
F16J 15/52 - Sealings between relatively-movable members, by means of a sealing without relatively-moving surfaces, e.g. fluid-tight sealings for transmitting motion through a wall by means of sealing bellows or diaphragms
To provide an inspection system with which it is possible to achieve the accuracy of detection suitable for the maintenance of structural soundness while reducing costs by circuit simplification and suppressing an interference with structures in the surrounding of an installed place, an increase in air resistance, and an impact on external appearance. An inspection system applied to moving vehicles, includes a circuit provided on the insulating coating material or non-conducting coating of the structural surface of a moving vehicle and closely attached to the insulating coating material or the non-conducting coating, a sensor terminal connected to the circuit, and an RF antenna terminal connected to an RF antenna, and further includes an RFID IC chip for detecting the electrical continuity state of the circuit.
A measurement method for a steam valve according to at least one embodiment of the present disclosure, includes: a step of measuring acceleration of a valve stem when a slave valve is opened by driving the valve stem with an actuator from a fully closed state of a master valve and the slave valve; a step of detecting a timing at which the slave valve is fully opened, based on the measured acceleration of the valve stem; and a step of calculating an amount of movement of the valve stem from a reference position to a position where the slave valve is fully opened.
A composite amine absorbent that absorbs at least one of CO2 and H2S in a gas includes: (a) a chain monoamine; (b) a diamine containing amino groups having the same number of substituents; (c) a chain diamine containing amino groups having different numbers of substituents; and (d) water.
B01D 53/14 - Separation of gases or vapoursRecovering vapours of volatile solvents from gasesChemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases or aerosols by absorption
In a method for estimating a flange displacement amount, effective three-dimensional coordinate data at a lower first position on a surface continuous with a lower flange surface of a first supported portion, a lower target midpoint position on the lower flange surface, an upper first position that is coincident with the lower first position in the horizontal direction on a surface continuous with an upper flange surface, and an upper target midpoint position on the upper flange surface are determined. The effective three-dimensional coordinate data at the respective positions are changed such that the effective three-dimensional coordinate data at the lower first position and the effective three-dimensional coordinate data at the upper first position are coincident with each other. A midpoint position in the vertical direction between the lower target midpoint position and the upper target midpoint position after the coordinate change is used as a target contact position.
F01D 25/24 - CasingsCasing parts, e.g. diaphragms, casing fastenings
G01B 21/04 - Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring length, width, or thickness by measuring coordinates of points
A steam turbine according to at least one embodiment of the present disclosure, includes: a first rotor blade disposed in an outer periphery of a rotor; and a stator vane adjacent to the first rotor blade on a downstream side in an axial direction of the rotor. The stator vane has a stator vane airfoil portion, a tip-side wall surface located on a tip side of the stator vane airfoil portion, and a hub-side wall surface located on a hub side of the stator vane airfoil portion. The tip-side wall surface is inclined to approach a central axis of the rotor toward the downstream side in the axial direction.
A gas turbine facility includes: a gas turbine; an ammonia supply device that supplies ammonia to a combustor of the gas turbine; a flow path forming frame forming an exhaust gas flow path through which exhaust gas from the gas turbine flows; a sprinkling device having a sprinkler that sprinkles water into the exhaust gas flow path; and a sprinkling controller that controls an operation of the sprinkling device. The sprinkling controller instructs the sprinkling device to start sprinkling the water on condition that an instruction to start supply of the ammonia to the combustor from the ammonia supply device or an instruction to stop the supply of the ammonia is received.
F02C 3/22 - Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
A hydrogen supply system includes: a hydrogen production device; a hydrogen flow line through which hydrogen produced by the hydrogen production device s circulated; a buffer tank that is provided in the hydrogen flow line on the downstream side of the hydrogen production device; a compressor that is provided in the hydrogen flow line on a downstream side of the buffer tank; a bypass line that bypasses a portion of the hydrogen flow line and has a downstream-side end portion communicating with the hydrogen flow line on the downstream side of the buffer tank; and a storage tank that is provided in the bypass line and is capable of storing the hydrogen.
Provided is a piston ring including: a low-pressure side ring; and a high-pressure side ring, the low-pressure side ring and the high-pressure side ring are arranged stacked in a direction along the axis so that the high-pressure side ring is closer to a fluid to be compressed, a low-pressure side rotation restriction part configured to restrict rotation in the circumferential direction relative to the piston is formed to the low-pressure side ring, a high-pressure side rotation restriction part configured to restrict rotation in the circumferential direction relative to the piston and a low-pressure side protrusion protruding toward the low-pressure side ring and inserted in the low-pressure side abutment are formed to the high-pressure side ring, and the low-pressure side protrusion is inserted in a low-pressure side abutment with clearances being provided in both sides in the circumferential direction between the low-pressure side ring and the low-pressure side protrusion.
The gas turbine combustor according to at least one embodiment of the present disclosure comprises a burner and fuel piping that supplies fuel to the burner. The fuel piping is connected to a member that separates at least a portion of a fuel cavity from the outside of the gas turbine combustor. The fuel piping includes a first region that is positioned upstream of the member, a second region that fits into a through hole that is formed in the member and allows the fuel cavity to communicate with the outside, and a third region that has an outer circumferential surface that is separated from an inner circumferential surface of the through hole toward the inside in the radial direction. A downstream end of the fuel piping reaches an end part of the through hole that, of either end part of the through hole, is closer to the fuel cavity.
A method for estimating a flange displacement amount includes determining effective three-dimensional coordinate data at a lower first position of a first supported portion on a surface continuous with a lower flange surface and at an upper first position coincident with the lower first position in a horizontal direction on a surface continuous with an upper flange surface. The effective three-dimensional coordinate data are changed such that the effective three-dimensional coordinate data at the lower first position and the effective three-dimensional coordinate data at the upper first position are coincident with each other. According to a difference between a position in a vertical direction indicated by the effective three-dimensional coordinate data at an upper target position and a position in the vertical direction indicated by the effective three-dimensional coordinate data at a lower target position, displacement amounts of the upper target position and the lower target position are obtained.
This threat countermeasure system comprises a calculation device and a communication device. The calculation device is configured so as to determine, on the basis of the threat level of at least one target, a countermeasure position of attack on the target. The countermeasure position represents either a first countermeasure position that is attacked in order to temporarily inhibit the function of the target or a second countermeasure position that is attacked in order to stop the function of the target. A first countermeasure period during which the attack is applied to the first countermeasure position in order to at least temporarily inhibit the function of the target may be shorter than a second countermeasure period during which the attack is applied to the second countermeasure position in order to stop the function of the target.
A high-temperature steam electrolysis device, a hydrogen production method, and a hydrogen production system include: a high-temperature steam electrolysis cell having a cylindrical shape in which a hydrogen/steam gas diffusion electrode layer is disposed on an inner side of an electrolyte layer and an oxygen gas diffusion electrode layer is disposed on an outer side thereof; a steam flow channel in which high-temperature steam flows on an inner side of the high-temperature steam electrolysis cell; and a helium flow channel in which high-temperature helium flows to heat the high-temperature steam electrolysis cell on an outer side of the high-temperature steam electrolysis cell.
C25B 9/23 - Cells comprising dimensionally-stable non-movable electrodesAssemblies of constructional parts thereof with diaphragms comprising ion-exchange membranes in or on which electrode material is embedded
A steam valve according to at least one embodiment of the present disclosure, includes: a valve body that includes a steam flow path through which steam flows, and a valve seat disposed in the middle of the steam flow path and having an opening portion; and a stop valve that includes a valve stem which extends in an axial direction, where an axis extends, and is movable back and forth in the axial direction, and a first valve disc which is fixed to a distal end part of the valve stem and is abutted against the valve seat to close the steam flow path. The valve stem is partitioned into a first valve stem to which the first valve disc is fixed and a second valve stem different from the first valve stem.
F16K 39/02 - Devices for relieving the pressure on the sealing faces for lift valves
F01K 7/16 - Steam engine plants characterised by the use of specific types of enginePlants or engines characterised by their use of special steam systems, cycles or processesControl means specially adapted for such systems, cycles or processesUse of withdrawn or exhaust steam for feed-water heating the engines being only of turbine type
An ammonia decomposition system includes: a reactor filled with a catalyst for a decomposition reaction where ammonia which is a raw material is decomposed into hydrogen and nitrogen; and a diluent gas supply line for supplying a diluent gas having a lower ammonia concentration than the raw material, such that the diluent gas is mixed with the raw material before the raw material flows into the catalyst. The reactor has an inner surface covered with a refractory material, and the catalyst is filled on a side opposite to the inner surface across the refractory material. The diluent gas supply line is provided with a temperature raising device for raising a temperature of the diluent gas.
B01J 8/02 - Chemical or physical processes in general, conducted in the presence of fluids and solid particlesApparatus for such processes with stationary particles, e.g. in fixed beds
C01B 3/04 - Production of hydrogen or of gaseous mixtures containing hydrogen by decomposition of inorganic compounds, e.g. ammonia
An ammonia decomposition system includes: a reactor filled with a catalyst for a decomposition reaction where ammonia which is a raw material is decomposed into hydrogen and nitrogen; and a diluent gas supply line for supplying a diluent gas having a lower ammonia concentration than the raw material, such that the diluent gas is mixed with the raw material before the raw material flows into the catalyst.
B01J 8/02 - Chemical or physical processes in general, conducted in the presence of fluids and solid particlesApparatus for such processes with stationary particles, e.g. in fixed beds
C01B 3/04 - Production of hydrogen or of gaseous mixtures containing hydrogen by decomposition of inorganic compounds, e.g. ammonia
A gas turbine facility includes: a fuel pipe connected to a fuel supply facility; a fuel supply pipe connected to a combustor of a gas turbine; a fuel treating pipe connected to a fuel treating apparatus that treats a fuel; and a three-way valve having an inlet port connected to the fuel pipe, a first outlet port connected to the fuel supply pipe, and a second outlet port connected to the fuel treating pipe.
F02C 3/22 - Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
F02C 3/30 - Adding water, steam or other fluids to the combustible ingredients or to the working fluid before discharge from the turbine
F02C 7/232 - Fuel valvesDraining valves or systems
A leakage gas emission system includes an enclosure surrounding at least part of a fuel supply system of a combustion device. The enclosure is provided with an outside emission unit for emitting internal gas to the outside. Fuel gas leaking from a leakage spot of the fuel supply system surrounded by the enclosure is taken in from an inlet port at one end of a first pipe and emitted from an emission port at another end toward the outside emission unit.
A blade ring assembly including: a turbine blade ring extending in a circumferential direction about an axis; a component to be cooled, disposed on an inner circumferential side of the turbine blade ring; and an outer circumferential side component disposed on an outer circumferential side of the turbine blade ring. The turbine blade ring has a cooling medium intake port leading from an outer circumferential surface to an inner circumferential surface of the turbine blade ring. The outer circumferential side component includes: a first wall portion which covers at least a portion of the cooling medium intake port from the outer circumferential side of the turbine blade ring; and a second wall portion which extends from an end portion of the first wall portion on the axially downstream thereof toward the outer circumferential side of the turbine blade ring.
A gas turbine includes a compressor for producing compressed air, a combustor for burning fuel with the compressed air, and a turbine driven by combustion gas generated by burning the fuel in the combustor, and is switchable between a normal operation mode which is an operation mode where a motor generator is driven by the turbine and a reverse power operation mode where the motor generator provides rotational power to the gas turbine. A fuel control device includes: a first valve for regulating pressure of fuel supplied to the combustor within a range of a first lower limit value and a first upper limit value; and a second valve for regulating pressure of the fuel supplied to the combustor within a flow rate range of a second lower limit value larger than the first lower limit value and a second upper limit value larger than the first upper limit value.
A hydrogen production system equipped with at least one container for housing a hydrogen compound member, a heating device for heating the inside of the at least one container by a heating medium, a cooling device for cooling the inside of the at least one container, and a water supply device for supplying water into the at least one container, the heating device being equipped with a solar collector for heating the heating medium by collecting sunlight and irradiating the heating medium.
A rotor disk includes a blade root groove into which a blade root of a turbine blade is insertable. The blade root groove includes a first bearing surface, a first disk neck outer curved surface which gradually moves toward a first circumferential side as it goes from an edge on an inner radial side of the first bearing surface toward the inner radial side, and a first disk neck inner curved surface which gradually moves toward a second circumferential side as it goes from a first disk neck position corresponding to an edge on the inner radial side of the first disk neck outer curved surface toward the inner radial side. The first disk neck outer curved surface includes a first curvature changing surface of which a curvature gradually increases from the first disk neck position toward an outer radial side.
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