BLOWER COMPRESSOR ASSEMBLY

CONNECTION STRUCTURE FOR A GENERATOR ASSEMBLY

CORE COMPARTMENT VENT DURING ENGINE SHUTDOWN TO REDUCED BOWED ROTOR START

AIRCRAFT NACELLE COMPRISING A SEALED BOX STRUCTURE AND A DOOR WHICH OPENS THE BOX STRUCTURE TO THE OUTSIDE

Ventilation structure of core chamber of turbofan engine having large bypass ratio and ventilation method therefor

MICRO GAS TURBINE DESIGNED TO LIMIT HEAT LOSSES THEREFROM

Core compartment vent during engine shutdown to reduced bowed rotor start

Means for handling gaseous fuel

METHOD FOR OPERATING A FLIGHT-PROPULSION SYSTEM

Gas Source System for Supplying Combustion Gas to a Turbine Engine by Fracturing Manifold Equipment

Cooling system of a compartment of pieces of equipment in a nacelle of an aircraft propelling assembly

Connection structure for a generator assembly

Mobile electric power generation system and transport arrangement

Seal assemblies for turbine engines and related methods

Liquid hydrogen-liquid oxygen fueled powerplant

Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions

Hydrogen fuel system

System for cooling turbine shaft coupling

Variable gap between impeller rotor and static structure

Compressor with a system for removing liquid from the compressor

Air supply device, gas turbine system and using method thereof

Means for handling gaseous fuel

Gas source system for supplying combustion gas to a turbine engine by fracturing manifold equipment

Internal structure for a turbomachine nacelle

Torque probe cooling for gas turbine engine using external air

DEGASSING TUBE AND EJECTION CONE FOR A TURBINE ENGINE, AS WELL AS TOOL FOR ASSEMBLY THEREOF

Steam turbine blade, steam turbine, and method for operating same

Connection structure for a generator assembly

Device for cooling heat-sensitive control members of a pneumatic or electropneumatic valve, and valve equipped with such a cooling device

Impact-cooling tubular insert for a turbomachine distributor

Fluid injection systems having fluid line purging

TURBINE ENGINE AND METHOD OF COOLING THEREOF

System for cooling turbine shaft coupling

Aircraft propulsion assembly having a ventilation system

Geared gas turbine engine with oil deaerator

Fluid injection systems having fluid line purging

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

Oil distribution system for an engine

Aircraft engine and air-oil separator system therefore

Turbine

Micro Gas Turbine Designed To Limit Heat Losses Therefrom

Aircraft propulsion unit and method for ventilating an engine enclosure

Gas turbine engine bypass drainage systems

Device for evacuation of a ventilated lubricated chamber of a turbomachine

LIQUID FUEL LEAK DETECTION SYSTEM AND RELATED METHOD

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

Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojet

Oil tank

Oil tank system

Centrifugal fan and air supply device having the same

Geared gas turbine engine with improved breather air venting

Thermal gradient attenuation structure to mitigate rotor bow in turbine engine

Aircraft turbomachine comprising a compartment equipped with a ventilation assembly

Sump housing for a gas turbine engine

GEARED GAS TURBINE ENGINE WITH OIL DEAERATOR

Hollow-fiber membrane for fuel degassing

Deaerator shaft with attachment surfaces

Insert assembly, airfoil, gas turbine, and airfoil manufacturing method

Gas turbine engine nacelle ventilation manifold for cooling accessories

GEARED GAS TURBINE ENGINE WITH REDUCED OIL TANK SIZE

Centrifugal compressor

Turbocharger assembly

Degassing tube and ejection cone for a turbine engine, as well as tool for assembly thereof

Turbo air blower having waterproof and damp-proof functions

Outlet tube vent with flow energizing features

GEARED GAS TURBINE ENGINE WITH OIL DEAERATOR

Ventilation panel with panel silencer for a turbine package enclosure

Turbine engine fan module including a turbine engine inlet cone de-icing system, and a de-icing method

Vibration reduction damper and jet engine

Localized engine protection from corrosion and contamination

Method and system for rotating air seal with integral flexible heat shield

Secondary flow baffle for turbomachinery

INTEGRATED AIRCRAFT ENVIRONMENTAL CONTROL AND BUFFER SYSTEM

Sump housing for a gas turbine engine

Method and system for controlling core cowl vent area

Core compartment ventilation devices for nacelles of gas turbine engines for cooling a core compartment of a gas turbine engine

STEAM TURBINE SYSTEM AND ASSOCIATED METHOD FOR PRESERVING A STEAM TURBINE SYSTEM

Hydrophobic filtration of tempering air

Exhaust-gas turbocharger for a motor vehicle

Vented gear spline lubrication

Valve device and jet engine with a valve device

Gas accumulation detection and ventilation in a gas turbine enclosure

Jet engine with multiple chambers and a bearing chamber support

Trailing edge core compartment vent for an aircraft engine

Door-type thrust reverser device for aircraft turbojet engine nacelle

Turbine ventilation structure

Motive air conditioning system for gas turbines

Drag link fitting and vent combination

Gas turbine nacelle ventilation manifold having a circumferential varying cross-sectional area

Gas turbine power generation equipment, and device and method for drying gas turbine cooling air system

Combined stability and customer bleed with dirt, water and ice rejection

Deaerator shaft with attachment surfaces

Moisture separator and air cycle system with the same

Gearbox with sealed accessory vent

Ventilation of a turbomachine nacelle

Geared gas turbine engine with oil deaerator

Gas turbine and operating method thereof

Gas turbine and operating method thereof

Gas turbine and operating method thereof

Ventilation system using thrust reverser linkages

Duct arrangement for an internal combustion engine

Cryogenic circuit conditioning system

Fairing device for aircraft propulsion assembly comprising an internal compartment fitted with a fan

Engine pylon having a drain

Axial-flow exhaust turbine

Variable geometry system turbocharger and method of manufacturing housing for variable geometry system turbocharger

Ventilation system and method for monitoring air flow in a ventilation system for a turbomachine assembly

System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine

Steam turbine

Rotor disc with fluid removal channels to enhance life of spindle bolt

Turbine engine shutdown temperature control system with an elongated ejector

Flow balancing ventilation system and method of balancing a flow

SYSTEMS AND METHODS FOR PROCESSING INLET AIR

TurbinAL™ high flow COdelivery system

Anti-icing core inlet stator assembly for a gas turbine engine

Disabling circuit in steam turbines for shutting off saturated steam

Gas turbine and gas-turbine plant having the same

Mist/moisture removal using fixed bed trickle columns

Deaerator and conduit assembly

Motor-generator connection shaft vent

System for cooling and purging exhaust section of gas turbine engine

PURGE SYSTEMS FOR ROTARY MACHINES AND METHODS OF ASSEMBLING SAME

System and method for turbine compartment ventilation

High temperature manifolds for gas turbine engines

Gas turbine and operating method thereof

Cavity ventilation

Cooling system for a turbomachine

High humidity gas turbine equipment

Oil filler tube assembly for aircraft engine

Fuel containment structure for engine fuel delivery system

Mobile electric power generation system

Torque probe cooling for gas turbine engine using internal fluid flow