Inventor · disambiguated record
Marcel R. Soligny
Also filed as: SOLIGNY MARCEL R · SOLIGNY MARCEL ROBERT
20 granted patents·813 citations·filing 1980–1986
96Inventor score
Top patents by PatentIndex Score
20 records- 0197US4596116ASealing ring for a turbine rotor of a turbo machine and turbo machine installations provided with such ringsSNECMA·Filed 1984·Granted Jun 24, 1986·129 cites·24 claims
- 0296US4452038ASystem for attaching two rotating parts made of materials having different expansion coefficientsSNECMA·Filed 1982·Granted Jun 5, 1984·78 cites·11 claims
- 0394US5593278AGas turbine engine rotor blading sealing deviceSNECMA·Filed 1983·Granted Jan 14, 1997·102 cites·34 claims
- 0494US4415310ASystem for cooling a gas turbine by bleeding air from the compressorSNECMA·Filed 1981·Granted Nov 15, 1983·75 cites·5 claims
- 0592US4409791AInjection device for the combustion chamber of turbine enginesSNECMA·Filed 1980·Granted Oct 18, 1983·47 cites·2 claims
- 0688US5700130ADevice for cooling and gas turbine rotorSNECMA·Filed 1983·Granted Dec 23, 1997·55 cites·11 claims
- 0787US4411589ARetaining device for the compressor casing of a turbine engineSNECMA·Filed 1980·Granted Oct 25, 1983·64 cites·7 claims
- 0886US4527385ASealing device for turbine blades of a turbojet engineSNECMA·Filed 1984·Granted Jul 9, 1985·69 cites·27 claims
- 0983US4558564AInter-shaft journal assembly of a multi-spool turbo-machineSNECMA·Filed 1983·Granted Dec 17, 1985·33 cites·5 claims
- 1059US4577814AVariable section nozzle for a turbo-jet engine and an aircraft comprising such equipmentSNECMA·Filed 1983·Granted Mar 25, 1986·16 cites·9 claims
- 1158US4705454ATurbomachine casing with containment structure intended to contain fractured rotating partsSNECMA·Filed 1986·Granted Nov 10, 1987·27 cites·9 claims
- 1255US5520336ANozzle for a jet engine containing an adjustable convergent-divergent portionSNECMA·Filed 1981·Granted May 28, 1996·13 cites·9 claims
- 1354US4674951ARing structure and compressor blow-off arrangement comprising said ringMETEUR D A SOC NAT D ETUDE CON·Filed 1985·Granted Jun 23, 1987·19 cites·9 claims
- 1454US4543039AStator assembly for an axial compressorSNECMA·Filed 1983·Granted Sep 24, 1985·23 cites·9 claims
- 1550US4353516AThrust reverser and silencer assembly of turbojet enginesSNECMA·Filed 1980·Granted Oct 12, 1982·14 cites·3 claims
- 1649US4724671ADevice for connecting a burner ring or flame holder to an afterburner duct of a turbojet engineSNECMA·Filed 1986·Granted Feb 16, 1988·12 cites·9 claims
- 1749US4541567AVariable area nozzle vaneSNECMA·Filed 1983·Granted Sep 17, 1985·11 cites·7 claims
- 1846US5566884ASupersonic nozzle for a turbojet engineSNECMA·Filed 1981·Granted Oct 22, 1996·9 cites·12 claims
- 1940US4521160ARotors of rotating machinesSNECMA·Filed 1983·Granted Jun 4, 1985·13 cites·13 claims
- 2035US5542607ASupersonic nozzle, in particular for a turbojet engineSNECMA·Filed 1982·Granted Aug 6, 1996·4 cites·22 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →