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 patentsUS4596116AJun 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