Inventor

BECOULET JULIEN FABIEN PATRICK

FR38 patents

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

BECOULET JULIEN FABIEN PATRICK

SAFRAN AIRCRAFT ENGINES

Power transmission system including a lubrication oil recovery device and turbomachine provided with such a power transmission system

Shaft assembly for an aircraft turbomachine

Dynamic sealing between two rotors of an aircraft turbomachine

Aircraft turbine engine with reduction gear

Device for centering and guiding a shaft of an aircraft turbine engine

Turbomachine with axial force recovery at the fan via pressurized gas feed

Scoop for an aircraft turbine engine

Propulsive assembly having decouplable casing portions

Aircraft turbomachine

Drive shaft comprising a fusible section and method for protecting such a drive shaft against an overtorque

Turbomachine comprising a means for decoupling a fan

Axial retention of a fan shaft in a gas turbine engine

Aircraft turbine engine with an off-axis propeller

Device for centring and rotationally guiding a turbomachine shaft comprising several optimised damping fluid films

Fused soft and hard bearing rings

Aircraft turbomachine arrangement comprising a lubrication pump driven by two oblique gears

Turbomachine comprising a means of uncoupling a fan

Turbomachine comprising a rear integrated electrical machine

Fan module comprising improved sealing means for a lubricant chamber

Planetary reducing gearset comprising a prestressed flexible support

Dynamic sealing between two rotors of an aircraft turbomachine

Turbomachine subassembly comprising a gooseneck of improved configuration, and turbomachine comprising such a subassembly

Aircraft turbomachine comprising a device for lubricating a bearing

Fan module provided with an oil transfer device

Speed reducer equipped with an electric machine

Impeller for a planet carrier of a planetary gear speed reducer of a turbomachine

Speed reducer of a turbomachine

Turbomachine comprising an alternator between two counter-rotating elements

Aircraft turbomachine comprising an electric machine

Device for centering and guiding a shaft of an aircraft turbine engine

Device for centering and guiding a shaft of an aircraft turbine engine

Flexibilities in a gas turbine engine with a speed reducer

Flexibilities in a gas turbine engine with speed reducer

Aircraft turbomachine with reduction gear

Turbomachine for an aircraft

Dual-flow turbojet engine arrangement with epicyclic or planetary reduction gear

Turbine engine module equipped with an electric machine having a rotor driven in rotation via a motion take-off mechanism

SNECMA

Turbine engine comprising a device for braking the fan rotor