P

Inventor

SOLIGNY MARCEL R

FR18 patents
⚠️ This page may combine multiple inventors who share the name “SOLIGNY MARCEL R”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SNECMA

17 patents
US4596116AJun 24, 1986

Sealing ring for a turbine rotor of a turbo machine and turbo machine installations provided with such rings

SNECMA129 citations96
US4452038AJun 5, 1984

System for attaching two rotating parts made of materials having different expansion coefficients

SNECMA78 citations96
US4411589AOct 25, 1983

Retaining device for the compressor casing of a turbine engine

SNECMA64 citations95
US5593278AJan 14, 1997

Gas turbine engine rotor blading sealing device

SNECMA102 citations94
US4415310ANov 15, 1983

System for cooling a gas turbine by bleeding air from the compressor

SNECMA75 citations94
US5700130ADec 23, 1997

Device for cooling and gas turbine rotor

SNECMA55 citations92
US4705454ANov 10, 1987

Turbomachine casing with containment structure intended to contain fractured rotating parts

SNECMA27 citations92
US4558564ADec 17, 1985

Inter-shaft journal assembly of a multi-spool turbo-machine

SNECMA33 citations92
US4409791AOct 18, 1983

Injection device for the combustion chamber of turbine engines

SNECMA47 citations92
US4527385AJul 9, 1985

Sealing device for turbine blades of a turbojet engine

SNECMA69 citations91
US4543039ASep 24, 1985

Stator assembly for an axial compressor

SNECMA23 citations81
US5520336AMay 28, 1996

Nozzle for a jet engine containing an adjustable convergent-divergent portion

SNECMA13 citations74
US4541567ASep 17, 1985

Variable area nozzle vane

SNECMA11 citations74
US4521160AJun 4, 1985

Rotors of rotating machines

SNECMA13 citations73
US4577814AMar 25, 1986

Variable section nozzle for a turbo-jet engine and an aircraft comprising such equipment

SNECMA16 citations72
US4724671AFeb 16, 1988

Device for connecting a burner ring or flame holder to an afterburner duct of a turbojet engine

SNECMA12 citations71
US4353516AOct 12, 1982

Thrust reverser and silencer assembly of turbojet engines

SNECMA14 citations66

METEUR D A SOC NAT D ETUDE CON

1 patent