COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

COOLING ARCHITECTURE FOR LIQUID HYDROGEN SUPERCONDUCTING SYSTEM

DEVICE FOR GUIDING A MAIN AIR FLOW FOR AN AIRCRAFT TURBINE ENGINE

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Variable area nozzle assembly and method for operating same

Gas turbine engine system with mixed flow auxiliary power unit

Power and ejector cooling unit

Dual valve fluid metering system

Method of cooling a turbine blade

Turbine engine inducer assembly

Compressor with a system for removing liquid from the compressor

Gas turbine engine with fluid circuit and ejector

Ejection cone having a flexible aerodynamic attachment

EJECTOR DRIVEN SCAVENGE SYSTEM FOR PARTICLE SEPARATOR ASSOCIATED WITH GAS TURBINE ENGINE

Heat transfer system

Gas compressor with reduced energy loss

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Gas compressor with reduced energy loss

IN-SPACE PROPULSION SYSTEM

Turbine casing cooling device for a turbomachine

Fluid drain system for an aircraft propulsion system

Electric submersible pump (ESP) gas slug mitigation system

System and method for engine eductor powered by alternate managed air system

Turbine engine inducer assembly

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Vented tangential on-board injector for a gas turbine engine

Compressor arrangement for an internal combustion engine and method for operating a compressor arrangement

Aircraft propulsion unit and method for ventilating an engine enclosure

Gas compressor with reduced energy loss

Gas turbine engine buffer system

System and method for engine eductor powered by alternate managed air system

Bleed air boosted engine oil cooler

Turbo-shaft ejector with flow guide ring

Diversion of fan air to provide cooling air for gas turbine engine

Air supply system for an aircraft

FLUID EJECTOR

Ejectors and methods of manufacture

Energy recovery-recycling turbine integrated with a capillary tube gas compressor

Pyrotechnic device

Gas turbine and method of operating the same

Active tip clearance control system for gas turbine engine

Ignition device and ignition method

Lubricated enclosure for an aircraft turbine engine, limiting the retention of lubricant during pitching

Pneumatic circuit for supplying air to at least one discharge valve and to at least one device for depressurizing an oil enclosure in a turbine engine

Bleed ejector

Hydraulic and pneumatic control circuit having a fuel/air heat exchanger for a turbojet

Air oil cooler airflow augmentation system

Gas turbine and method for operating gas turbine

Jet pump for a turbomachine, comprising blading for imparting rotation to active fluid

Swirling flow eductor system and method

HEAT EXCHANGE SYSTEMS FOR TURBOMACHINES

ECOLOGY FUEL RETURN SYSTEMS

Fuel additive injection system and methods for inhibiting coke formation

Gas turbine with extraction-air conditioner

Outlet tube vent with flow energizing features

ENHANCED THERMAL MANAGEMENT FOR DIRECTED ENERGY WEAPON

Gas turbine

Turbine engine inducer assembly

Injection cooled cooling air system for a gas turbine engine

Vented tangential on-board injector for a gas turbine engine

Ejector and refrigeration cycle apparatus having ejector

System and method for purging fuel or coolant from turbomachine

Method of detecting a malfunction of a valve in a turboshaft engine

Multi-circuit buffer system for a gas turbine engine

TURBINE ENGINE EJECTOR THROAT CONTROL

Oil cooling systems for a gas turbine engine

Bleed air heat ejectors

Variable geometry thruster

System and method of compressor inlet temperature control with mixing chamber

Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine

Cooling device for a turbomachine supplied by a discharge circuit

Cooling structure for turbine, and gas turbine

Ecology fuel return systems

Staged fuel and air injection in combustion systems of gas turbines

Inlet bleed heat control system

System for generating steam and for providing cooled combustion gas to a secondary gas turbine

System for generating steam and for providing cooled combustion gas to a secondary gas turbine combustor

System and method for generating electric energy

Power transmission device

Compressor rim thermal management

Fuel system for a gas turbine engine

Power generation system having compressor creating excess air flow and turbo-expander using same

Secondary air system with venturi

Diversion of fan air to provide cooling air for gas turbine engine

Anti-icing system for an aircraft

Jet pump for turbomachine lubrication chamber depressurization circuit

Fuel supply apparatus for aircraft engine

Aircraft fuel system with fuel return from engine

Device for cooling oil for a turbine engine

Ventilation of a turbomachine nacelle

Prime mover with recovered energy driven compression of the working fluid

Gas turbine engine ejector

Cartridge Style Ejector Pump

Air oil cooler airflow augmentation system

Gas turbine engine exhaust drain

Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure

Fan device

Turbomachine fuel circuit

Self-cooling fan assembly

Gas turbine engine buffer system

Vented tangential on-board injector for a gas turbine engine

Jet pump for depressurizing lubrication chambers of a turbomachine, having independent double injectors

System and method for generating electric energy

Cooling system and method for supplying a cooling gas flow

Cooling system with compressor bleed and ambient air for gas turbine engine

Turbine flow modulation for part load performance

Jet engine with at least one oil separator

Turbocharger

Multi-circuit buffer system for a gas turbine engine

Turbine engine temperature control system with heating element for a gas turbine engine

Chamber fluid removal system

Ram air thermal management system

Gas turbine engine buffer system

System and method for reducing back pressure in a gas turbine system

Method of generating a high-speed airflow

Fuel circuit of a turbine engine

Temperature control within a cavity of a turbine engine

Device for activating a passive ejector valve for pressurising a turbojet engine chamber for an aircraft

Exhaust system for use with a turbine and method of assembling same

GAS TURBINE ANTI-ICING SYSTEM

Fuel feed network for a rotorcraft engine, the network including means for priming a pump for sucking fuel from a feed tank

Intake liner for a gas turbine engine

ACTIVE CONTROL OF COMPRESSOR EXTRACTION FLOWS USED TO COOL A TURBINE EXHAUST FRAME

Customer bleed air pressure loss reduction

BUFFER SYSTEM THAT COMMUNICATES BUFFER SUPPLY AIR TO ONE OR MORE PORTIONS OF A GAS TURBINE ENGINE

Gas turbine engine buffer system

Multi-circuit buffer system for a gas turbine engine

Gas turbine with motive fluid driven jet-compressor

Gas turbine engine bearing chamber seals

Adaptive eductor system

Method and apparatus for optimizing the operation of a turbine system under flexible loads

Gas turbine rotor with purge blades

System for ventilating a gas turbine enclosure

Method and systems for bleed air supply

Aircraft engine fuel system

Gas turbine arrangement and method for operating a gas turbine arrangement

Method, system and apparatus for providing water to a heat engine via a dammed water source

SYSTEM AND METHOD FOR GENERATING POWER IN A DAM

Gas turbine engine with ejector

Fuel feed device for aviation engine

Compressor

Gas turbine engine with cooling arrangement

Cooling system for a gas turbine and corresponding operation method

Ejector controlled twin air source gas turbine pressurizing air system

NOISE ATTENUATION DEVICE FOR REDUCING NOISE ATTENUATION IN A JET ENGINE TEST CELL

Filter assembly for fuel supply to actuators and fuel control system of aircraft engine and method

Method and systems for bleed air supply

Measurement of steam quality in steam turbine

Method for the manufacture of an ejector nozzle tube

Variable geometry ejector

GAS TURBINE ENGINE WITH EJECTOR

Gas turbine engine with ejector

Method and apparatus for using compressed air to increase the efficiency of a fuel driven turbine generator

Thermal management system

SYSTEM AND METHOD FOR MANAGING TURBINE EXHAUST GAS TEMPERATURE

Apparatus and method for cooling turbomachine exhaust gas

Turbine with fluidically-controlled valve and swirler with a bleed hole

EDUCTOR SYSTEM FOR A GAS TURBINE ENGINE

Systems and Methods for Supplying Cooling Air to a Gas Turbine

Method and device for cooling a component of a turbine

SYSTEM FOR REDUCING OIL CONSUMPTION IN GAS TURBINE ENGINES

Fluid flow machine with fluid injector assembly

Lubrication system and method, and vortex flow separator for use therewith

Pumping Ejector

Ramjet superheater

Statically-operating ejector ramjet

Hypermixing Fluid Ejector

Gas turbine oil scavenging system

Mixer for cooling and sealing air system for turbomachinery

Vent for the lubricating oil system of a jet engine

SERVO-CONTROLLED VARIABLE GEOMETRY EJECTOR PUMP

MULTI-PORT BLEED SYSTEM WITH VARIABLE GEOMETRY EJECTOR PUMP

Turbocharger for a vehicle with a coanda device

Ejector controlled twin air source gas turbine pressurizing air system

System for reducing oil consumption in gas turbine engines

Variable motive nozzle ejector for use with turbine engines

Eductor swirl buster

Method for operating a turbo engine and turbo engine

Variable jet mixer for improving the performance of a fixed displacement fuel pump

Combi-Supersonic-Adjusting-Nozzle

Turbineless jet engine

Cooling system for a gas turbine engine

Ejector for cooling air supply pressure optimization

Gas turbine apparatus

Turbomachine

Quiet chevron/tab exhaust eductor system

Thermal management for aircraft auxiliary power unit compartment

Ejector cooled nozzle

High-efficiency jet ejector and propulsive jet

Water augmented regeneration (WAR) turbine system and cycle

Ejector for cooling air supply pressure optimization

Thermal management system