GAS TURBINE ENGINE HAVING A HYDRAULIC FAN BRAKE

MULTI-SPEED TURBINE REDUCTION GEARBOX SYSTEM AND METHOD

Fluid damper for turbine engine geartrain assembly

AIRCRAFT PROPULSION SYSTEM WITH AUXILIARY TURBINE SYSTEM

AIRCRAFT PROPULSION SYSTEM GEARTRAIN

NEUTRAL TURBINE GEARBOX SYSTEM AND METHOD

Gas turbine engine having a hydraulic fan brake

UNIDIRECTIONAL FAN BRAKE FOR A GAS TURBINE ENGINE

Selective power distribution for an aircraft propulsion system

Multi-speed turbine reduction gearbox system and method

Aircraft propulsion system geartrain

Aircraft propulsion system geartrain

Multi-speed turbine reduction gearbox system and method

Aircraft thrust reverser comprising a braking mechanism for slowing a mobile cowl in the event of overtravel

Curvilinear coupling for aircraft turbomachinery

SHAFT FAILURE PROTECTION SYSTEM

System and method for rotor overspeed mitigation

Gas turbine engine

Gas turbine engine

Gas turbine engine with low pressure compressor stages

Anti-windmilling system for a gas turbine engine

COMPRESSOR SYSTEM

Gas turbine engine with gearbox health features

Anti-reverse rotation apparatuses, rotors for use therein, and related methods

Method and system for controlling the braking of an aircraft equipped with a thrust-reversal system

Gas turbine and method for protecting a gas turbine in case of a shaft break

Power plant management system for dual engine helicopter in single engine operation mode

Anti-windmilling system for a gas turbine engine

Anti-windmilling system for a gas turbine engine

Inline propeller gearbox brake

Run-up surface for the guide-vane shroud plate and the rotor-blade base plate

Gas turbine engine with gearbox health features

Emergency stop for blades of drone

System for braking a low pressure spool in a gas turbine engine

Device for driving actuators for a thrust reverser, comprising a disengageable manual drive unit

Device for driving actuators for a thrust reverser, selectively allowing motorised or manual driving

Turbine engine comprising a device for braking the fan rotor

Geared architecture to protect critical hardware during fan blade out

Device for controlling a nozzle of variable cross-section of an aircraft

Method for optimizing the speed of a twin-spool turbojet engine fan, and architecture for implementing same

Systems and methods for changing a speed of a compressor boost stage in a gas turbine

Brake mechanism for air turbine starter

System providing braking in a gas turbine engine in the event of the turbine shaft breaking

Axial flow turbine with overspeed preventing device

Hydraulic lock for axial motion output device

Synchronizing stationary clutch of compression braking with a two spool gas turbine engine