Inventor

BRAULT MICHEL GILBERT ROLAND

FR44 patents

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

BRAULT MICHEL GILBERT ROLAND

SAFRAN AIRCRAFT ENGINES

Shaft assembly for an aircraft turbomachine

Dynamic sealing between two rotors of an aircraft turbomachine

Aircraft turbine engine with reduction gear

Turbomachine module comprising a rotor supporting pitchable blades

Variable-pitch fan with low pitch of a turbine engine

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

Device for deicing a separator nose of an aviation turbine engine

Turbine engine provided with a lubrication unit

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

Turbojet engine with thrust take-up means on the inter-compressors case

Turbojet engine with thrust take-up means on the inter-compressor case

Device for limiting overspeeding of a turbine shaft of a turbomachine, and associated control method

Fused soft and hard bearing rings

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

Turbojet engine comprising a simplified bearing lubrication unit

Turbomachine module equipped with an electric machine rotor

Aircraft turbomachine with reducer

Dynamic sealing between two rotors of an aircraft turbomachine

Speed reducer equipped with an electric machine

Speed reducer of a turbomachine

Low-pitch variable-setting fan of a turbine engine

Aircraft turbomachine with reduction gear

Turbofan comprising a simplified bearing lubrication assembly

Aircraft turbomachine front part

System for rotating a fan of a turbojet engine

SNECMA

Turbine module for a gas turbine engine

Turbomachine with a decoupling device common to first and second bearings of its drive shaft, compressor comprising the decoupling device and decoupling device

Intermediate casing for turbomachine and accessory gearbox drive assembly

Balancing device of a turbomachine engine

Turbine engine comprising an upstream attachment means for a de-oiling pipe

Front enclosure which is sealed during the modular dismantling of a turbojet with reduction gear

Aeroengine fitted with heat exchanger means

Rotating assembly comprising a transmission member and an oil distribution system

Impeller having a radial seal for a turbine engine turbine

BRAULT MICHEL GILBERT ROLAND

Air reinjection compressor

Rotary assembly for a turbomachine fan

Driveshaft for the gearbox of auxiliary machines of a turbojet engine

Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe

Fastener device for fastening a free turbine stator with dual centering

SNECMA MOTEURS

Bleed-off device in a bypass turbojet

Turbomachine rotor arrangement

BIL ERIC STEPHAN

Gas turbine high pressure compressor fluid return and reinjection including an annular air bleeding manifold