Inventor

BEAUJARD ANTOINE JEAN-PHILIPPE

FR26 patents

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

BEAUJARD ANTOINE JEAN-PHILIPPE

SAFRAN AIRCRAFT ENGINES

Turbomachine rotor with optimised bearing surfaces

Aircraft with a propulsion unit comprising a fan at the rear of the fuselage

Aircraft comprising a propulsion assembly including a pair of propellers at the rear of the fuselage

Shell for reducing overpressure in the vicinity of the upstream seal of a turbojet bearing housing

Turbine arrangement incorporating an oil recovery circumferential trough

Device for evacuation of a ventilated lubricated chamber of a turbomachine

Aircraft engine intake arrangement comprising a mechanical decoupler

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

Turbojet with bearing architecture optimised for the support of a low pressure shaft

Aircraft propulsion assembly comprising a thrust reverser

Turbine engine for an aircraft

Rotor for turbine engine comprising blades with added platforms

SNECMA

Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing device

Method for holding an adapter piece on a tubular housing of a turbo engine, and corresponding adapter piece and holding system

Method of fabricating a composite material casing for a gas turbine engine, and a casing obtained thereby

Impeller having a radial seal for a turbine engine turbine

BEAUJARD ANTOINE JEAN-PHILIPPE

Turbine engine comprising a metal protection for a composite part

CMC turbine nozzle adapted to support a metallic turbine internal casing by an axial contact

Assembly formed by a turbine nozzle or a compressor diffuser made of CMC for a turbine engine and by an abradable material support ring, and a turbine or a compressor incorporating such an assembly

CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contact

ROUSSILLE CLÉMENT

Turbomachine blades or vanes having complementary even/odd geometry

Turbomachine blade or vane having complementary asymmetrical geometry

COUPE DOMINIQUE

Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing same

NUNEZ ROMAIN

Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same

BELMONTE OLIVIER

Turbine engine stator wheel and a turbine or a compressor including such a stator wheel

BART JACQUES RENE

Device for locking a root of a rotor blade