145520 ⎘
Function; Heat transfer, e.g. cooling Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT
#2ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT
#3EXHAUST SYSTEM FOR A TURBINE ENGINE, COMPRISING A HEAT EXCHANGER
#4HYBRID FIXED-OPEN LOW TEMPERATURE THERMAL RESERVOIR FOR LOW-GRADE HEAT FOR A HEAT PUMP CYCLE
#5SUPERCHARGED COMBUSTOR COOLING USING TURBOMACHINERY
#6GAS TURBINE ENGINE HAVING COOLING SYSTEMS
#7AIRCRAFT HEAT MANAGEMENT
#8AIRCRAFT HEAT MANAGEMENT
#9Aircraft heat management
#10Aircraft heat management
#11METHODS, SYSTEMS, AND APPARATUS TO CONTROL A FLUID PROVIDED TO COMPONENTS IN A FLUID PUMP OF A CLOSED LOOP SYSTEM
#12ON-DEMAND HYDROGEN FOR POWER GENERATION
#13GAS TURBINE ENGINES WITH HEAT RECOVERY SYSTEMS
#14Closed-loop cooling system for a gas turbine engine
#15Blade with tip rail cooling
#16FUEL CELL POWER SYSTEM FOR A VEHICLE
#17Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
#18Gas turbine engine
#19CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT
#20COMBINATION OF A GAS TURBINE ENGINE AND A POWER ELECTRONICS
#21Components for gas turbine engines
#22CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT
#23Friction bearing, and method for lubricating and cooling a friction bearing
#24GEARBOX AND GAS TURBINE PROPULSION UNIT
#25APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE
#26Gas turbine engines with heat recovery systems
#27Air energy storage powered uninterruptible power supply
#28AIRCRAFT HAVING AN ENGINE AND A COOLING SYSTEM BASED ON DIHYDROGEN
#29High-temperature fuel thermal transport bus architecture
#30PROPULSION SYSTEM COOLING CONTROL
#31Heat transfer system
#32Cooling device for turbine nozzle guide vane by liquid metal with low melting point
#33Coolant delivery via an independent cooling circuit
#34Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
#35Coolant delivery via an independent cooling circuit
#36Regenerative thermal management system
#37Chilled working fluid generation and separation for an aircraft
#38System for cooling an aircraft turbojet engine
#39Trailing edge tip cooling of blade of a gas turbine blade
#40Supercritical carbon dioxide-cooled generator and turbine
#41Turbofan engine comprising an outlet cone cooled by its secondary flow
#42Blade with tip rail, cooling
#43OGV electroformed heat exchangers
#44Processes for removing carbon dioxide from exhaust gas using scraped and non-scraped heat exchangers
#45Gas turbine blade for re-using cooling air and turbomachine assembly and gas turbine comprising the same
#46Thermal management system
#47Compressor with thermal expansion reducing structure
#48Engine with cooling passage circuit extending through blade, seal, and ceramic vane
#49Integrated cooling sub-system
#50Turbine rotor airfoil and corresponding method for reducing pressure loss in a cavity within a blade
#51Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
#52Heat exchanger thermal shock reducer
#53Blade with tip rail cooling
#54Airfoil having internal hybrid cooling cavities
#55Apparatus for desuperheating high temperature, high velocity steam
#56Turbine blade with a coupled serpentine channel
#57Turbine scroll assembly for gas turbine engine
#58Thermal management system
#59Waste heat recovery system
#60Intercooled tangential air injector for gas turbine engines
#61Gas turbine engine and cooling air configuration for turbine section thereof
#62System with thin walled cooling plate for an electronic enclosure
#63Hybrid expander cycle with turbo-generator and cooled power electronics
#64Hybrid expander cycle with pre-compression cooling and turbo-generator
#65System with conduit arrangement for dual utilization of cooling fluid in a combustor section of a gas turbine engine
#66Airfoil having improved throughflow cooling scheme and damage resistance
#67Airfoil core inlets in a rotating vane
#68Microchannel heat exchangers for gas turbine intercooling and condensing
#69Systems and methods for cooling electronic engine control devices
#70Diversion of fan air to provide cooling air for gas turbine engine
#71Shroud for gas turbine engine
#72Shroud for gas turbine engine
#73Propulsion system cooling control
#74Chilled working fluid generation and separation for an aircraft
#75Coolant airflow assembly particulate filter with panels in series
#76Cryogenic cooling system for an aircraft
#77Telescoping bore basket for gas turbine engine
#78Blade having a tip cooling cavity and method of making same
#79Impingement cooling features for gas turbines
#80Gas turbine engine compressor
#81OIL PIPE ASSEMBLY
#82Gas turbine engine component cooling with resupply of cooling passage
#83Turbine blade comprising a cooling circuit
#84APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE ENGINE
#85Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
#86Turbine shroud cooling
#87Turbine shroud cooling
#88Air oil cooler airflow augmentation system
#89Sliding seal
#90Thermal management system
#91Liquid propellant rocket engine nozzle with passive condensate cooling
#92OGV electroformed heat exchangers
#93Fluid cooling structure for an electric machine of a gas turbine engine
#94Airfoil having internal hybrid cooling cavities
#95Airfoil having internal hybrid cooling cavities
#96Airfoil having internal hybrid cooling cavities
#97Airfoil having internal hybrid cooling cavities
#98Airfoil having fluidly connected hybrid cavities
#99Gas turbine engine active clearance control system using inlet particle separator
#100Variable orifice flow control device
#101Refrigerant gas cooling of motor and magnetic bearings
#102Variable area turbine arrangement with secondary flow modulation
#103Engine component with hollow turbulators
#104Cooling device for components of wind turbines
#105Blade with tip rail cooling
#106Airfoil with tip rail cooling
#107Gas turbine and component-temperature adjustment method therefor
#108Interdigitated turbine engine air bearing cooling structure and method of thermal management
#109Turbine engine cooling system with an open loop circuit
#110Tip clearance control for gas turbine engine
#111Leading edge hybrid cavities and cores for airfoils of gas turbine engine
#112Vane cooling system
#113Turbine engine airfoil having a cooling circuit
#114Modular gas turbine inlet cooling systems
#115ACTIVE GAP CONTROL FOR TURBINE ENGINE COMPRESSOR
#116Thermal isolation structure for rotating turbine frame
#117Injection cooled cooling air system for a gas turbine engine
#118Turbine scroll assembly for gas turbine engine
#119Turbine have a first and second rotor disc and a first and second cooling fluid conduit wherein the second cooling fluid conduit is extended through an annular axially extended bore having a radially outer extent defined by a radially innermost surface of the rotor discs
#120Cooling circuits for a multi-wall blade
#121Cooling circuits for a multi-wall blade
#122Combustor aft frame cooling
#123Chamfered stator vane rail
#124Combustion chamber structure, particularly for a rocket engine
#125Cooling circuit for a multi-wall blade
#126Ice protection system for gas turbine engines
#127GAS TURBINE ENGINE STATOR VANE BAFFLE ARRANGEMENT
#128Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct
#129RING SEGMENT SYSTEM FOR GAS TURBINE ENGINES
#130Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium
#131GAS TURBINE ENGINE
#132COpower generation system
#133Active core cooling system
#134Impingement cooling system for a gas turbine engine
#135Airfoil with cooling circuit
#136Airfoil with cooling circuit
#137System and method for cooling components of a gas turbine engine
#138Turbine engine cooling system with an open loop circuit
#139Annular ring assembly for shroud cooling
#140Turbine apparatus and method for redundant cooling of a turbine apparatus
#141Cooling device for cooling platforms of a guide vane ring of a gas turbine
#142Cooling concept for turbine blades or vanes
#143Gas turbine with two swirl supply lines for cooling the rotor
#144Method and system for controlling core cowl vent area
#145Rotor blade cooling circuit
#146System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
#147Cooling circuit for a multi-wall blade
#148Crossover hole configuration for a flowpath component in a gas turbine engine
#149Compressor core inner diameter cooling
#150Article and method of cooling an article
#151Thermal management system
#152Closed loop cooling method and system with heat pipes for a gas turbine engine
#153Multi-chamber platform cooling structures
#154Gas turbine engine with rotor centering cooling system in an exhaust diffuser
#155Article and method of cooling an article
#156Turbine engine advanced cooling system
#157METHOD FOR OPERATING A GAS TURBINE ENGINE UNIT
#158Turbine component surface cooling system with passive flow modulation
#159Gas turbine engine component cooling with resupply of cooling passage
#160Wall cooling arrangement for a gas turbine engine
#161Gas turbine engine component cooling circuit with respirating pedestal
#162Sliding seal
#163System for cooling a turbine engine
#164Diversion of fan air to provide cooling air for gas turbine engine
#165Gas turbine, gas-turbine control device, and gas turbine operation method
#166Variable area turbine arrangement with secondary flow modulation
#167Gas turbine engine component providing prioritized cooling
#168Microchannel heat exchangers for gas turbine intercooling and condensing
#169Engine component having platform with passageway
#170Heat exchanger having a coaxial or concentric tube construction
#171Supply duct for cooling air from gas turbine compressor
#172METHOD AND SYSTEM FOR SEPARATING CO2 FROM N2 AND O2 IN A TURBINE ENGINE SYSTEM
#173Sealing structure and turbine
#174Secondary flowpath system for a gas turbine engine
#175Combustor cap assembly
#176Ducting platform cover plate
#177Inner stage turbine seal for gas turbine engine
#178Gas turbine engine airfoil impingement cooling
#179Air oil cooler airflow augmentation system
#180Annular ring assembly for shroud cooling
#181Technique for cooling a root side of a platform of a turbomachine part
#182Gas turbine and operating method thereof
#183Gas turbine and operating method thereof
#184Gas turbine and operating method thereof
#185Propellant feed circuit and a cooling method
#186Turbocharger
#187Blade outer air seal with cored passages
#188System and method of distillation process and turbine engine intercooler
#189Turbine sections of gas turbine engines with dual use of cooling air
#190Turbine vane with cooled fillet
#191Heat exchanger for a turbo engine
#192Bore basket for a gas powered turbine
#193Re-use of internal cooling by medium in turbine hot gas path components
#194Method of recovering energy in a steam-cooled gas turbine
#195Axial flow machine cooling system
#196Impingement cooling of turbine blades or vanes
#197Shroud block segment for a gas turbine
#198Gas turbine engine heat exchanger system
#199Gas turbine shroud assemblies
#200Transition duct with divided upstream and downstream portions
#201Compressor air provided to combustion chamber plenum and turbine guide vane
#202Casing cooling duct
#203Electricity generation device and method employing cryogenic fluid, evaporator, superheater, and expansion turbine
#204Airfoil and method of making
#205Gas turbine and guide blade for a housing of a gas turbine
#206Turbine engine cooling system with an open loop circuit
#207Gas turbine engine airfoil cooling circuit
#208System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
#209Atomizing air heat exchange for heating attemperation feed water in a combined cycle turbine
#210Inlet air chilling system with humidity control and energy recovery
#211Cooling air configuration in a gas turbine engine
#212Turbine casing comprising ring sector attachment means
#213Blade outer air seal with cored passages
#214Gas turbine engine airfoil impingement cooling
#215Gas turbine engine airfoil cooling circuit
#216Gas turbine
#217STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES
#218Gas turbine engine having a multi-variable closed loop controller for regulating tip clearance
#219METHOD AND SYSTEM FOR SEPARATING CO2 FROM N2 AND O2 IN A TURBINE ENGINE SYSTEM
#220Hybrid vapor and film cooled turbine blade
#221Cooled turbine blade and method for cooling a turbine blade
#222Blade outer air seal with multi impingement plate assembly
#223TURBINE AIRFOIL AND METHOD OF CONTROLLING A TEMPERATURE OF A TURBINE AIRFOIL
#224Method for cooling a gas turbine plant and gas turbine plant for implementing the method
#225BLADE OUTER AIR SEAL WITH PASSAGE JOINED CAVITIES
#226Gas turbine engine
#227Turbine airfoil cooling system with high density section of endwall cooling channels
#228Rear hub cooling for high pressure compressor
#229METHOD FOR COOLING TURBINE STATORS AND COOLING SYSTEM FOR IMPLEMENTING SAID METHOD
#230GAS TURBINE ENGINE COMPONENT
#231Aircraft gas turbine
#232ARRANGEMENT AND METHOD FOR CLOSED FLOW COOLING OF A GAS TURBINE ENGINE COMPONENT
#233System for cooling and purging exhaust section of gas turbine engine
#234Platform with cooling circuit
#235Hot gas path component cooling for hybrid pulse detonation combustion systems
#236Axial flow gas turbine
#237Axial flow gas turbine
#238Axial flow gas turbine
#239Gas turbine of the axial flow type
#240Control method for cooling a turbine stage in a gas turbine
#241Gas turbine engine systems involving cooling of combustion section liners
#242Nitrogen cooled gas turbine with combustor nitrogen injection and partial nitrogen recycling
#243INTERDEPENDENT LUBRICATION SYSTEMS
#244Cooled IBR for a micro-turbine
#245COOLED COMPONENT FOR A GAS TURBINE
#246SYSTEMS, METHODS AND APPARATUS FOR PROPULSION
#247Flow device comprising a cavity cooling system
#248Hybrid cooling of a gas turbine engine
#249Adjustable loop rotor air cooler and fuel gas heater
#250Ventilation of a high-pressure turbine in a turbomachine
#251Shaft seal
#252Rear hub cooling for high pressure compressor
#253Gas turbine bucket with serpentine cooled platform and related method
#254Turbine starter lubricant cooling
#255Cooling system of ring segment and gas turbine
#256Shroud seal segments arrangement in a gas turbine
#257Gas turbine engine with cooling arrangement
#258Gas turbine and operating method thereof
#259Steam turbine having a cooling apparatus
#260APPARATUS AND METHOD FOR TURBINE ENGINE COOLING
#261Ejector controlled twin air source gas turbine pressurizing air system
#262Gas turbine engine cooling system and method
#263Steam turbine, method of cooling steam turbine, and heat insulating method for steam turbine
#264Gas turbine engine rotary injection system and method
#265Cooling structure of turbine airfoil
#266Method and apparatus for simplified thrust chamber configurations
#267Blade cooling
#268Thimble, sleeve, and method for cooling a combustor assembly
#269Thermally decoupled can-annular transition piece
#270Fuel-cooled flexible heat exchanger with thermoelectric device compression
#271Turbine airfoil cooling system with dual serpentine cooling chambers
#272Running-gap control system of an aircraft gas turbine
#273System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft
#274Cold fuel cooling of intercooler and aftercooler
#275Method and apparatus for cooling a transition piece
#276Gas turbine engine with heat insulation device
#277Cooling system for a turbomachine
#278Apparatus and method for cooling a turbine airfoil arrangement in a gas turbine engine
#279Device for regulating the flow rate of air feeding a turbine ventilation cavity of a turbomachine turbine section
#280Method and device for supplying a space propulsion engine with liquid cryogenic propellants
#281Methods and apparatus involving shroud cooling
#282Shroud hanger with diffused cooling passage
#283Steam Cooled Direct Fired Coal Gas Turbine
#284Gas turbine engine fan bleed heat exchanger system
#285Apparatus and method for drawing off and recirculating a cooling stream
#286Gas turbine engine and integrated heat exchange system
#287Simplified thrust chamber recirculating cooling system
#288Vortex cooled turbine blade outer air seal for a turbine engine
#289GAS TURBINE
#290Blade under platform pocket cooling
#291Turbine cooling flow modulation
#292Gas turbine engine systems involving cooling of combustion section liners
#293Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
#294Systems and Methods for Extending Gas Turbine Emissions Compliance
#295Turbine nozzle sector
#296Disk of a disk rotor for a gas turbine
#297Method and system for cooling fluid in a turbine engine
#298Hybrid cooling of a gas turbine engine
#299Gas turbine engine with air and fuel cooling system
#300Combined power plant