139134 ⎘
Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
Sub-classes:GAS TURBINE ENGINE
#2GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO
#3GAS TURBINE ENGINE BEARING AND GEARBOX ARRANGEMENT
#4REDUCTION GEARBOX FOR GAS TURBINE ENGINE
#5LOW NOISE TURBINE FOR GAS TURBINE ENGINE
#6GAS TURBINE ENGINE WITH CONTROLLED RETURN OF FUEL TO POWER ACCESSORIES AND RETROFITTING METHOD
#7ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
#8EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION
#9GAS TURBINE ENGINE WITH FRONT SUPPORT ARRANGEMENT
#10GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES
#11GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES
#12GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO
#13GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
#14CONSTANT SPEED ACCESSORY GEARBOX FOR TURBINE ENGINE
#15GEARED GAS TURBINE ENGINE
#16GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES
#17DUAL PURPOSE INTEGRATED GEAR FOR HYBRID TRAIN APPLICATION
#18GAS TURBINE ENGINE FRONT SECTION
#19AIRCRAFT PROPULSION SYSTEM WITH AUXILIARY TURBINE SYSTEM
#20GAS TURBINE ENGINE BEARING AND GEARBOX ARRANGEMENT
#21Recovered-cycle turboshaft engine
#22ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
#23GAS TURBINE ENGINE WITH FRONT SUPPORT ARRANGEMENT
#24METHOD OF ASSEMBLY FOR GAS TURBINE FAN DRIVE GEAR SYSTEM
#25Geared gas turbine engine
#26LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
#27GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
#28GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES
#29Transmission and method for control of boost spool
#30Boosting gas turbine engine power with fluid motor
#31GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO
#32Aircraft engine having two radially offset turbines
#33Fan module comprising improved sealing means for a lubricant chamber
#34SYSTÈME PROPULSIF AÉRONAUTIQUE
#35COMPOUNDED TURBO POWER UNIT WITH BOOST COMBUSTOR
#36POWER DEVICE CAPABLE OF GENERATING GREATER PROPELLING FORCE
#37Engine mount system for a gas turbine engine
#38Gas turbine engine compressor arrangement
#39Selective power distribution for an aircraft propulsion system
#40Geared turbine engine with relatively lightweight propulsor module
#41Gas turbine fan drive gear system
#42Gas turbine engine with power density range
#43Gas turbine engine with front support arrangement
#44PORTABLE AND WEARABLE HAND-GRASP NEURO-ORTHOSIS
#45Reduction gearbox for gas turbine engine
#46Reduction gearbox for gas turbine engine
#47Transmission and method for control of boost spool
#48Gas turbine engine with third stream
#49Low noise turbine for geared turbofan engine
#50Modular multistage turbine system for gas turbine engines
#51Planetary gearbox for gas turbine engine
#52GAS TURBINE ENGINE WITH CLUTCH SYSTEM BETWEEN LOW-PRESSURE COMPRESSOR AND LOW-PRESSURE TURBINE
#53Gas turbine engine compression system with core compressor pressure ratio
#54GEARED ARCHITECTURE FOR HIGH SPEED AND SMALL VOLUME FAN DRIVE TURBINE
#55GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES
#56Gas turbine engine bearing and gearbox arrangement
#57Aircraft hybrid propulsion fan drive gear system dc motors and generators
#58Gas turbine engine with high speed low pressure turbine section and bearing support features
#59Geared turbofan engine with targeted modular efficiency
#60Geared turbofan engine with a high ratio of thrust to turbine volume
#61Aircraft turbomachine
#62STRADDLE MOUNTED LOW PRESSURE COMPRESSOR
#63Power device capable of generating greater propelling force
#64Gas turbine engine front section
#65Assembly for retaining a gear train in a turbomachine
#66Aircraft and direct drive engine under wing installation
#67Gas turbine engine with power density range
#68Efficient gas turbine engine installation and operation
#69EFFICIENT GAS TURBINE ENGINE
#70Geared turbofan engine with targeted modular efficiency
#71Method of assembly for gas turbine fan drive gear system
#72Thrust efficient gas turbine engine
#73Planetary gearbox for gas turbine engine
#74Low noise turbine for geared gas turbine engine
#75Curvilinear coupling for aircraft turbomachinery
#76Geared turbofan engine gearbox arrangement
#77Turbine engine system utilizing an augmented combustion module
#78Planetary gear and gas turbine engine
#79Gas turbine engine having electric motor for applying power to a spool shaft and method for operating same
#80Gas turbine engine compression system with core compressor pressure ratio
#81Geared turbine engine with relatively lightweight propulsor module
#82Geared gas turbine engine arrangement with core split power ratio
#83Turbine section of gas turbine engine
#84Gas turbine engine with non-epicyclic gear reduction system
#85EXTERNAL MIXING CHAMBER FOR A GAS TURBINE ENGINE WITH COOLED TURBINE COOLING AIR
#86Aircraft turbomachine with reducer
#87Geared turbofan with integral front support and carrier
#88Double-flow turbojet engine assembly with epicycloidal or planetary gearbox
#89Low noise turbine for geared gas turbine engine
#90Fundamental gear system architecture
#91Splitter and guide vane arrangement for gas turbine engines
#92Engine mount system for a gas turbine engine
#93Geared gas turbine engine with reduced fan noise
#94Geared turbofan arrangement with core split power ratio
#95Safety apparatus
#96Geared turbofan engine with a high ratio of thrust to turbine volume
#97Aircraft hybrid propulsion fan drive gear system DC motors and generators
#98Fan drive gear system
#99Gas turbine engine with efficient thrust generation
#100Geared architecture for high speed and small volume fan drive turbine
#101GAS TURBINE ENGINE
#102GAS TURBINE ENGINE
#103Turbine section of high bypass turbofan
#104Turbine section of high bypass turbofan
#105High pressure ratio gas turbine engine
#106High pressure ratio gas turbine engine
#107Turbofan engine front section
#108Casing
#109Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbine
#110Gas turbine engine bifurcation located fan variable area nozzle
#111METHOD FOR SETTING A GEAR RATIO OF A FAN DRIVE GEAR SYSTEM OF A GAS TURBINE ENGINE
#112LUBRICATION SYSTEM FOR GAS TURBINE ENGINES
#113Efficient gas turbine engine installation and operation
#114Geared gas turbine engine
#115Shaft assembly for an aircraft turbomachine
#116Gas turbine
#117Gas turbine engine having electric motor applying power to the high pressure spool shaft and method for operating same
#118Turbine section of high bypass turbofan
#119Gas turbine engine variable area fan nozzle control
#120Gas turbine engine compressor arrangement
#121Geared turbofan engine with power density range
#122Turbine section of high bypass turbofan
#123GEAR REDUCTION FOR LOWER THRUST GEARED TURBOFAN
#124Geared turbofan engine with targeted modular efficiency
#125Low noise turbine for geared gas turbine engine
#126Geared turbofan engine gearbox arrangement
#127Joining method
#128Joining method
#129Geared turbofan with non-epicyclic gear reduction system
#130Geared gas turbine engine with reduced fan noise
#131Geared turbine engine with relatively lightweight propulsor module
#132Method of assembly for gas turbine fan drive gear system
#133Systems and methods for transferring mechanical power in a turbine engine
#134POWER TRAIN ARCHITECTURES WITH LOW-LOSS LUBRICANT BEARINGS AND LOW-DENSITY MATERIALS
#135Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
#136Low noise turbine for geared gas turbine engine
#137Efficient gas turbine engine installation and operation
#138Gas turbine engine compression system
#139LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
#140Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement
#141VARIABLE CYCLE FAN FOR MINIMIZING NOISE
#142LOW FAN NOISE GEARED GAS TURBINE ENGINE
#143Thrust efficient turbofan engine
#144Automobile engine
#145Gear assembly for a turbo machine
#146Turbofan engine bearing and gearbox arrangement
#147Planetary gear system for turbomachine
#148Geared turbofan arrangement with core split power ratio
#149HIGH THRUST GEARED GAS TURBINE ENGINE
#150Multi-directional gearbox deflection limiter for a gas turbine engine
#151Gas turbine engine and method of creating classes of same
#152SPILT COMPRESSOR SYSTEM ON MULTI-SPOOL ENGINE
#153EFFICIENT GAS TURBINE ENGINE
#154Gas turbine engine with high speed low pressure turbine section and bearing support features
#155Gas turbine engine with efficient thrust generation
#156Labyrinth sealing system and gas turbine engine with a labyrinth sealing system
#157Geared turbofan with integral front support and carrier
#158Geared turbofan arrangement with core split power ratio
#159Geared architecture gas turbine engine with oil scavenge
#160Gas turbine engine configured for modular assembly/disassembly and method for same
#161Aircraft hybrid propulsion fan drive gear system DC motors and generators
#162Magnetic torque metering system
#163GAS TURBINE
#164Gas turbine
#165Planetary gear and gas turbine engine
#166Geared turbofan engine with targeted modular efficiency
#167Casing
#168Elongated geared turbofan with high bypass ratio
#169Fluid collection gutter for a geared turbine engine
#170Fundamental gear system architecture
#171Gas turbine engine
#172Method and device for connecting fan rotor to low pressure turbine rotor
#173Fluid collection gutter for a geared turbine engine
#174Geared turbofan engine with power density range
#175GEARED TURBOFAN ENGINE WITH INTER-SHAFT DEFLECTION FEATURE
#176Gas turbine blower/pump
#177THREE SPOOL TURBOFAN ENGINE WITH LOW NOISE INTERMEDIATE TURBINE ROTOR
#178Multi-stage compressor with turbine section for fuel cell system
#179Systems and methods for a gas turbine engine with combined multi-directional gearbox deflection limiters and dampers
#180Turbofan engine bearing and gearbox arrangement
#181Gas turbine engine including a dual-speed split compressor
#182Gas turbine engine with high speed low pressure turbine section and bearing support features
#183Gas turbine engine with selective flow path
#184Geared turbine engine with relatively lightweight propulsor module
#185Geared turbofan engine with a high ratio of thrust to turbine volume
#186REVERSE-FLOW CORE GAS TURBINE ENGINE WITH A PULSE DETONATION SYSTEM
#187Method of operating an engine assembly
#188Method of providing turbine engines with different thrust ratings
#189Counter rotating turbine with reversing speed reduction assembly
#190Turbomachine with alternatingly spaced turbine rotor blades
#191Turbomachine with alternatingly spaced turbine rotor blades
#192Active system generating destructive acoustic interference for an aircraft engine with multiple fan spools
#193Gas turbine engine with optimized fan, core passage inlet, and compressor forward stage diameter ratios
#194Turbine section of high bypass turbofan
#195Spline ring for a fan drive gear flexible support
#196GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE
#197Reverse core gear turbofan
#198Geared gas turbine engine with reduced fan noise
#199Combined power generation system comprising a fuel cell and a gas turbine engine
#200Turbine section of high bypass turbofan
#201Turbine section of high bypass turbofan
#202Gas turbine engine with gearbox health features
#203Counter rotating power turbine with reduction gearbox
#204Low fan noise turbojet
#205Gas turbine engine variable area fan nozzle control
#206Gas turbine engine geared compressor with first and second input rotors
#207GEARED TURBOFAN WITH INTEGRALLY BLADED ROTOR
#208Distributed fan lubrication system
#209Aircraft and direct drive engine under wing installation
#210Counter rotating turbine with reversing reduction gear assembly
#211ANNULAR AIRFLOW ACTUATION SYSTEM FOR VARIABLE CYCLE GAS TURBINE ENGINES
#212Turbine engine with fan and reduction of speed on the shaft of the power turbine
#213Geared turbofan with non-epicyclic gear reduction system
#214Mechanical flywheel for bowed rotor mitigation
#215Aircraft propulsion assembly equipped with a main fan and with at least one offset fan
#216Aircraft with multiple fan propulsion assembly fixed under the wing
#217Gas turbine engine bifurcation located fan variable area nozzle
#218Planet-carrier for an epicyclic gearing and epicyclic gearing provided with such a planet carrier
#219Aircraft propulsion assembly equipped with a main fan and with a least one offset fan
#220Turbine housing assembly
#221Planetary gear system for turbomachine
#222GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE
#223GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
#224Planetary gearbox for gas turbine engine
#225Turbine rotor with low over-speed requirements
#226External mixing chamber for a gas turbine engine with cooled turbine cooling air
#227Counter rotating turbine with reversing reduction gearbox
#228GAS TURBINE ENGINE ARCHITECTURE WITH SPLIT COMPRESSOR SYSTEM
#229SYSTEMS AND METHODS INVOLVING MULTIPLE TORQUE PATHS FOR GAS TURBINE ENGINES
#230Assistance device for a free-turbine engine of an aircraft having at least two free-turbine engines
#231GEAR SYSTEM ARCHITECTURE FOR GAS TURBINE ENGINE
#232Cooling air for gas turbine engine with supercharged low pressure compressor
#233Lubrication system for gas turbine engines
#234Lubrication system for gas turbine engines
#235SPEED SENSOR PROBE LOCATION IN GAS TURBINE ENGINE
#236Geared turbofan with high speed generator
#237Geared low fan pressure ratio fan exit guide vane stagger angle
#238Geared architecture for high speed and small volume fan drive turbine
#239Method of assembly for gas turbine fan drive gear system
#240Geared turbofan with three turbines all counter-rotating
#241Geared turbofan gas turbine engine architecture
#242Turbofan engine bearing and gearbox arrangement
#243Gas turbine engine with a geared turbofan arrangement
#244Split compressor turbine engine
#245Reverse flow gas turbine engine with offset RGB
#246GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES
#247GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION
#248SYSTEM FOR FAULT TOLERANT PASSAGE ARRANGEMENTS FOR HEAT EXCHANGER APPLICATIONS
#249Turbine shaft power take-off
#250Multi-spool gas turbine engine architecture
#251Multi-spool gas turbine engine architecture
#252Gas turbine engine shaft architecture and associated method of disassembly
#253Gear train architecture for a multi-spool gas turbine engine
#254Geared turbofan gas turbine engine architecture
#255SYSTEM FOR A LOW SWIRL LOW PRESSURE TURBINE
#256GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE
#257System and method for an integral drive engine with a forward main gearbox
#258SYSTEM AND METHOD FOR A GAS TURBINE POWER GENERATION SYSTEM WITH A HIGH PRESSURE COMPRESSOR WITH AN ADDED FORWARD STAGE
#259Thrust efficient turbofan engine
#260Thrust efficient turbofan engine
#261Thrust efficient turbofan engine
#262Geared Architecture for High Speed and Small Volume Fan Drive Turbine
#263Gas turbine engine with distributed fans
#264Geared turbofan gas turbine engine architecture
#265TURBINE SECTION OF HIGH BYPASS TURBOFAN
#266Gas turbine engine with high speed low pressure turbine section and bearing support features
#267Electromagnetic anti-windmilling system
#268Anti-windmilling system for a gas turbine engine
#269GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE
#270Gas turbine engine gear train
#271Inlet turbine and transmission for high-mach engines
#272Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
#273Inline propeller gearbox brake
#274Gas turbine engine with high speed low pressure turbine section and bearing support features
#275Geared architecture for high speed and small volume fan drive turbine
#276System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
#277Method and system for in-line distributed propulsion
#278Electric windmill pump for gearbox durability
#279Thrust efficient turbofan engine
#280Thrust efficient turbofan engine
#281Thrust efficient turbofan engine
#282Heat exchange system for a power gear box, a power gear box and a turbo engine with a power gear box
#283Heat exchange system for power gear box, a power gear box and a turbo engine with a power gear box
#284Power gearbox pin arrangement
#285Compliant shaft with a recursive configuration for turbine engines
#286Multi-shaft gas turbine engine
#287Geared turbofan gas turbine engine architecture
#288Systems and methods for a gas turbine engine with combined multi-directional gearbox deflection limiters and dampers
#289Geared turbofan gas turbine engine architecture
#290Geared turbofan gas turbine engine architecture
#291Power transmission device
#292Method and apparatus for monitoring lubrication pump operation during windmilling
#293Turbojet engine with offset fans with a differential system
#294Shafting arrangement for a gas turbine engine
#295Multi-directional gearbox deflection limiter for a gas turbine engine
#296Geared turbofan engine gearbox arrangement
#297Gas turbine engine with low stage count low pressure turbine
#298Turbine inter-spool energy transfer system
#299Turbine section of high bypass turbofan
#300Turbine section of high bypass turbofan