139175 ⎘
Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus ; Adaptations of gas- turbine plants for special use; Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
OPEN ROTOR PROPULSION SYSTEM WITH FORWARD EXHAUST OUTLET(S)
#2REDUCTION GEARBOX FOR GAS TURBINE ENGINE
#3HYBRID GAS TURBINE ENGINE
#4BEARING CURRENT MITIGATION FOR AN ELECTRIC MACHINE EMBEDDED IN A GAS TURBINE ENGINE
#5PROPULSION SYSTEM FOR AN AIRCRAFT
#6THRUST DIVERTER FOR AN OPEN ROTOR AIRCRAFT PROPULSION SYSTEM
#7OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH BYPASS FLOWPATH
#8IMPROVED PROPULSION ASSEMBLY FOR MULTI-ENGINE HYBRID AIRCRAFT
#9METHOD AND UNIT FOR CONTROLLING A MOTOR ASSEMBLY
#10UNDUCTED PROPULSION SYSTEM
#11REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
#12UNDUCTED TURBINE ENGINE COMPRISING STATOR BLADES HAVING DIFFERENT CHORDS
#13GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY
#14PROPULSION SYSTEM AND METHOD FOR OPERATION
#15UNDUCTED THRUST PRODUCING SYSTEM ARCHITECTURE
#16Gas turbine engine
#17SYSTÈME PROPULSIF AÉRONAUTIQUE
#18EXHAUST DUCT FOR HYBRID AIRCRAFT POWERPLANT
#19ENGINE POWER EXTRACTION SYSTEM AND METHOD FOR USING SAME
#20METHOD AND AIRCRAFT PROVIDED WITH AT LEAST ONE COMBUSTION ENGINE AND A DRIVE SYSTEM WITH AT LEAST TWO ELECTRIC MACHINES
#21GAS TURBINE ENGINE AND METHOD OF OPERATION
#22PROPELLER SHAFT ASSEMBLY FOR AIRCRAFT ENGINE
#23Propulsion System for an Aircraft
#24Geared turbine engine with relatively lightweight propulsor module
#25Unducted propulsion system
#26HYBRID PROPULSION TURBOMACHINE AND AIRCRAFT COMPRISING SUCH A TURBOMACHINE
#27ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE
#28AIRCRAFT POWERPLANT WITH BOOSTED GAS TURBINE ENGINE
#29Reduction gearbox for gas turbine engine
#30Reduction gearbox for gas turbine engine
#31ACTIVE COMPRESSOR STALL RECOVERY
#32BEARING CURRENT MITIGATION FOR AN ELECTRIC MACHINE EMBEDDED IN A GAS TURBINE ENGINE
#33Gas turbine engine with third stream
#34Planetary gearbox for gas turbine engine
#35PROPULSION SYSTEM CONFIGURATIONS AND METHODS OF OPERATION
#36Reverse-flow gas turbine engine
#37Inlet for unducted propulsion system
#38Gas turbine engine shaft with lobed support structure
#39CABLE FOR ELECTRIC POWER TRANSMISSION
#40ELECTRIC COMPONENT FOR AN ELECTRIC SYSTEM
#41METHOD AND DEVICE FOR MONITORING THE OPERATION OF A PAIR OF TURBOPROP ENGINES THROUGH THE NUMERICAL PROCESSING OF AN ACOUSTIC MAGNITUDE
#42Gas turbine engine and method of operation
#43Power management methods for multi engine rotorcraft
#44Hybrid electric variable area turbine
#45Turbine over-speed brake for hybrid electric gas turbine engine
#46Operating a turboprop engine for in-flight restart
#47Hybrid gas turbine engine and torque transfer assembly therefore
#48Bearing current mitigation for an electric machine embedded in a gas turbine engine
#49Through-flow gas turbine engine with electric motor and electric generator
#50Compact low-pressure compressor
#51OPEN ROTOR TURBOMACHINERY ENGINES
#52PROPULSION SYSTEM CONFIGURATIONS AND METHODS OF OPERATION
#53ACTIVE COMPRESSOR STALL RECOVERY
#54Planetary gearbox for gas turbine engine
#55Airfoil attachment for turbine rotor
#56Gas turbine engine having a turbomachine and an electric motor coupled to a propeller
#57Gas turbine system and gas turbine power generator
#58Aircraft engine with clutch and mechanical lock
#59Hybrid electric engine speed regulation
#60GROUND OPERATIONS OF A HYBRID ELECTRIC PROPULSION SYSTEM
#61Hybrid electric aircraft engine
#62THRUST WITH THE MINIMUM EJECTION OF PROPELLANT
#63High speed rotorcraft propulsion configuration
#64Reverse-flow gas turbine engine
#65HYBRID GAS TURBINE ENGINE
#66Reverse flow engine architecture
#67Through-flow gas turbine engine with electric motor and electric generator
#68Layered fuselage shield
#69Motor controller electronics arrangements with passively cooled feeder cables
#70Turbofan engine comprising a set of rotatable blades for blocking off the bypass flow duct and redirecting the air flow
#71Propeller governor for electric synchronous thrust
#72Reverse-flow gas turbine engine
#73Gas turbine engine with clutch assembly
#74COMBINATION COMPRESSED-FLUID EJECTOR AND PROPELLER PROPULSION SYSTEM
#75AIRCRAFT TURBOPROP ENGINE INLET COMPACT PROFILE CONFIGURATION
#76Unducted single rotor engine and method for operation
#77System and method for control for unducted engine
#78Control system and method for a turbopropeller engine based on inlet temperature sensing
#79Electrical systems
#80Power management systems for multi engine rotorcraft
#81POWER SYSTEM FOR ROTARY WING AIRCRAFT
#82System and method for operating a multi-engine rotorcraft for ice accretion shedding
#83SYSTEM AND METHOD FOR OPERATING A ROTORCRAFT
#84Propulsion engine for an aircraft
#85Propulsion system for an aircraft
#86Unducted thrust producing system architecture
#87Unducted thrust producing system
#88Aircraft engine with clutch and mechanical lock
#89Multi-variable fleet optimisation method and system
#90Multi-spool gas turbine engine architecture
#91Signal processing for variable geometry mechanism control
#92Ported shroud system for turboprop inlets
#93Transmission for engine with two power inputs
#94High speed rotorcraft propulsion configuration
#95Nacelle-integrated air-driven augmentor fan for increasing propulsor bypass ratio and efficiency
#96Method and system for controlling a crossing threshold used in determining rotational speed of a propeller
#97Turboprop engine assembly with combined engine and cooling exhaust
#98Hydraulic line routing plate
#99Unducted thrust producing system
#100Pitch actuation system for a turbomachine propeller
#101Compound engine assembly with offset turbine shaft, engine shaft and inlet duct
#102Simplified pitch actuation system for a turbomachine propeller
#103Fluid cooling structure for an electric machine of a gas turbine engine
#104Turbine engine with single wall cantilevered architecture
#105System for controlling a controlled parameter
#106Aircraft power setting trims for life extension
#107Gearbox for gas turbine engine
#108Variable pitch blade pivot for a turbine engine fan hub
#109Turbomachine comprising a trap for foreign objects circulating in an air flow
#110Propulsion system for an aircraft
#111Additively manufactured heat exchanger
#112Turbojet of the unducted rotor type
#113Support assembly for a propeller shaft
#114AIRCRAFT PROPULSION ASSEMBLY COMPRISING A FAN CONJOINTLY DRIVEN BY TWO ENGINES
#115Feedback system for pitch-adjustable blades of aircraft bladed rotor
#116Propulsion system for an aircraft
#117Clutch device for gas turbine engines
#118Turbine housing assembly
#119Engine driven by Sc0cycle with independent shafts for combustion cycle elements and propulsion elements
#120Planetary gearbox for gas turbine engine
#121Turbine rotor with low over-speed requirements
#122Compound engine assembly with cantilevered compressor and turbine
#123Gearbox for gas turbine engine
#124Power plant thrust management system for turboprop engines
#125Turbine engine having horizontally offset axes
#126Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
#127Reverse flow gas turbine engine with offset RGB
#128Reverse-flow gas turbine engine
#129Propulsion engine for an aircraft
#130Hybrid aircraft
#131Hybrid aircraft with transversely oriented engine
#132Turbine shaft power take-off
#133Multi-spool gas turbine engine architecture
#134Gas turbine engine shaft architecture and associated method of disassembly
#135Gear train architecture for a multi-spool gas turbine engine
#136Propulsion unit with selective coupling means
#137Hybrid gas-electric turbine engine
#138Integral offset oil tank for inline accessory gearbox
#139Reconfigurable lubrication system for multiple powertrain orientations
#140Simplified pitch actuation system for a turbine engine propeller
#141Supply of air to an air-conditioning circuit of an aircraft cabin
#142Air inlet duct for an aircraft turbine engine
#143Air intake with scroll portion and strutted portion for gas turbine engine
#144Inline propeller gearbox brake
#145Oil system for turbine engine and related method
#146Hybrid propulsion system for a gas turbine engine including a fuel cell
#147Multi-shaft gas turbine engine
#148Nacelle-integrated air-driven augmentor fan for increasing propulsor bypass ratio and efficiency
#149Propulsion system using supercritical COpower transfer
#150Method of regulating a three-engined power plant for a rotary wing aircraft
#151System and method for propeller pitch control
#152Turboprop engine assembly with combined engine and cooling exhaust
#153Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine
#154Method of regulating a three-engined power plant for a rotary wing aircraft
#155Suspension structure for suspending a turboprop having two unducted propellers from a structural element of an aircraft with rigid fastening of the air intake structure
#156Engine driven by SC0cycle with independent shafts for combustion cycle elements and propulsion elements
#157Hydraulic line routing plate
#158Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine
#159Immersed core flow inlet between rotor blade and stator vane for an unducted fan gas turbine
#160Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine
#161Turboprop engine with compressor turbine shroud
#162Method for automatically controlling the operating speed of a helicopter turboshaft engine, corresponding control device and helicopter provided with such a device
#163Compound engine assembly with cantilevered compressor and turbine
#164Engine assembly with modular compressor and turbine
#165System and method for emergency starting of an aircraft turbomachine
#166Exhaust duct
#167Method of managing a power demand for the operation of a pilotless aircraft equipped with an internal combustion engine
#168Air intake arrangement
#169Power plant having a two-stage cooler device for cooling the admission air for a turboshaft engine
#170GAS TURBINE
#171Aircraft hybrid engine having gear ring encased fans
#172Vane assembly for an unducted thrust producing system
#173Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
#174Monitor system for monitoring the starting of a rotary wing aircraft, an aircraft, and a method using the system
#175Gas turbine engine with embedded distributed fans
#176Unducted thrust producing system architecture
#177Unducted thrust producing system
#178Hybrid drive for gas turbine engine
#179Turbine engine having a pair of propellers for an aircraft
#180Contra-rotating open fan propulsion system
#181Fixed turbine engine receiver part comprising an assembly for holding ancillary systems in position inside a fixed hollow shaft
#182Rotor noise suppression
#183Oil transfer system on rotating shaft
#184System for in-flight restarting of a multi-shaft turboprop engine
#185Turbomachine propeller blade setting device
#186Turboprop engine with compressor turbine shroud
#187Hub for radial housing of a helical ring of a turbomachine with variable-pitch blades and assembly comprising such a hub
#188Turboprop engine systems with noise reducing inlet assemblies
#189Transverse mounted gas turbine engine
#190Counterweight-based device for controlling the orientation of fan blades of a turboprop engine
#191Retention device for a rotating blade
#192Mounting system
#193Turboprop provided with a blade-positioning device
#194Cooled pusher propeller system
#195Hub for a propeller having variable pitch blades
#196Prestressing device having circumferential activity
#197Blade-retaining device for turbomachine propeller
#198Unducted propeller with variable pitch blades for a turbomachine
#199Hydraulic system for fan pitch change actuation of counter-rotating propellers
#200Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
#201Actuation mechanism for a convertible gas turbine propulsion system
#202Gas turbine engine with noise attenuating variable area fan nozzle
#203Aircraft turbine engine and use of such a turbine engine
#204Exhaust duct with bypass channel
#205Engine arrangement
#206Propulsion unit
#207Propfan engine
#208Coupling assembly
#209Method and apparatus for the operation of a turboprop aircraft engine provided with pusher propellers
#210Hybrid propulsive engine including at least one independently rotatable turbine stator
#211Hybrid propulsive engine including at least one independently rotatable propeller/fan
#212Hybrid propulsive engine including at least one independently rotatable compressor stator
#213Hybrid propulsive engine including at least one independently rotatable turbine stator
#214Turboprop including a set of adjustable-pitch blades
#215Propfan assembly
#216Rotary internal combustion engine
#217Gas discharge device for a vehicle engine
#218Cooled pusher propeller system
#219Hydrazine monopropellant decomposition air turboprop engine
#220Thermoelectric generation system
#221Actuation mechanism for a convertible gas turbine propulsion system
#222Convertible gas turbine propulsion system
#223Exhaust duct with bypass channel
#224Fan control apparatus
#225Offset drive for gas turbine engine
#226Propeller or propeller drive
#227GAS TURBINE GEARBOX
#228Gas turbine gearbox
#229Compact epicyclic gear carrier
#230Open rotor with fixed guide vane/stator
#231Heat exchanger bypass ejector
#232Thrust diverter for an open rotor aircraft propulsion system
#233Unducted propulsion system
#234Propulsion system for an aircraft