Inventor

LARDELLIER ALAIN M J

25 patents

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

LARDELLIER ALAIN M J

SNECMA

Hollow blade for a turbomachine

Housing for an axial compressor

Containment structure for a turbojet engine

Turbine bearing

Removable sealing gasket for distributor segments of a jet engine

Turbine shroud sealing device

Hollow blade for a turbomachine and method of manufacturing said blade

Variable cycle propulsion engine for supersonic aircraft

Thrust reverser for a high-bypass ratio turbofan engine

Counterrotating fan engine

High by-pass ratio turbojet engine with counterrotating upstream and downstream fans

Wing mounting nacelle for a very high by-pass ratio turbojet aero-engine

Gas turbine engine

Apparatus for controlling radial clearance between a rotor and a stator of a tubrojet engine compressor

Method for the manufacture of a ceramic turbine ring integral with a metallic annular carrier

Adjustment system of centering a turbomachine wheel and mounted turbomachine by way of permitting the application of said system

Removable support for the sealing lining of the casing of jet engine blowers

Means for controlling clearance in an intershaft bearing journal of a multi-spool gas turbine

Combined turborocket and ramjet propulsion unit

Safety device for an axially rotating machine

Contra-rotating fan engine

Housing for a turbojet engine compressor

Apparatus for measuring the temperature of a gas flow traversing a grid of blades

MOTEURS D AVIAT S N E SOC NAT

Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft

MATEURS D AVIAT S N E C M A SO

Thrust vectoring nozzle assembly