Inventor

CHARIER GILLES ALAIN MARIE

FR38 patents

⚠️ This page may combine multiple inventors who share the name “CHARIER GILLES ALAIN MARIE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

CHARIER GILLES ALAIN MARIE

SAFRAN AIRCRAFT ENGINES

Turbofan comprising a power supply device to drive the compressor

Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub

Fan module with variable pitch blades

Fan module comprising variable-pitch blades

Turbine engine comprising a rotor supporting variable-pitch blades

Radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fan

Turbomachine with fan rotor and reduction gearbox driving a low-pressure decompressor shaft

Turbojet with step-down mechanism

Assembly on a shaft of a turbomachine of a bladed rotor disc and of a rotor of a low pressure compressor having at least two mobile nozzle stages

Fan module with variable pitch blades

Fan module with variable pitch blades

Turbine engine comprising a rotor with variable-pitch blades

Aircraft turbine engine provided with an electrical machine

Aircraft turbine engine with at least two bodies and means for drawing power

Turbomachine comprising a rear integrated electrical machine

Aeronautic propulsion system with improved propulsion efficiency

Aeronautic propulsion system with improved propulsion efficiency

Fan module equipped with an electrical machine for an aircraft turbine engine

Turbomachine with electric machine comprising a rotor ring attached to the fan

Turbine engine module equipped with a propeller and stator vanes supported by retaining means and corresponding turbine engine

Aeronautical propulsion system having a low leakage flow rate and improved propulsion efficiency

Aircraft turbine engine equipped with an electrical machine

Aeronautical propulsion system with improved propulsive efficiency

Aircraft turbine engine equipped with an electrical machine

Electric module for an aircraft fan comprising blades with improved attachment

Fan module having variable-pitch blades

Aeronautic propulsion system with low leakage rate and improved propulsion efficiency

System for controlling the cyclic setting of blades

Fan module equipped with an oil transfer device

Fan module equipped with an oil-transfer device

Pitch change module for turbine engine and corresponding turbine engine

SNECMA

Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle

Compressor comprising a plurality of cells reconstituting an annular volume of separation of flows in a turbine engine

Compressor with centripetal air takeoff

Device for varying the section of the throat in a turbine nozzle

Device for ventilating turbine disks in a gas turbine engine

Assembly arrangement between a bearing inner race and a journal, race and journal suitable for such an arrangement, and turbomachine fitted therewith

Multistage turbomachine compressor