Inventor · disambiguated record
Georges Mazeaud
Also filed as: MAZEAUD GEORGES
23 granted patents·1 pending application·766 citations·filing 1981–2006
97Inventor score
Top patents by PatentIndex Score
24 records- 0195US5524430AGas-turbine engine with detachable combustion chamberSNECMA·Filed 1993·Granted Jun 11, 1996·100 cites·17 claims
- 0295US4805398ATurbo-machine with device for automatically controlling the rate of flow of turbine ventilation airSNECMA·Filed 1987·Granted Feb 21, 1989·107 cites·10 claims
- 0390US5052176ACombination turbojet-ramjet-rocket propulsion systemSNECMA·Filed 1989·Granted Oct 1, 1991·74 cites·98 claims
- 0487US4500143AMeans for controlling clearance in an intershaft bearing journal of a multi-spool gas turbineSNECMA·Filed 1982·Granted Feb 19, 1985·39 cites·9 claims
- 0585US5163285ACooling system for a gas turbineSNECMA·Filed 1990·Granted Nov 17, 1992·75 cites·8 claims
- 0684US6474596B1Suspension system with intrinsic safety features for aircraft powerplantsSNECMA MOTEURS·Filed 2000·Granted Nov 5, 2002·47 cites·4 claims
- 0784US4378197AInter-shaft bearing for multibody turbojet engines with damping by a film of oilSNECMA·Filed 1981·Granted Mar 29, 1983·38 cites·5 claims
- 0883US7506499B2Turbofan jet engine with ancillaries distribution supportSNECMA·Filed 2005·Granted Mar 24, 2009·22 cites·11 claims
- 0978US7543442B2Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systemsSNECMA·Filed 2005·Granted Jun 9, 2009·18 cites·7 claims
- 1069US5193980AHollow turbine blade with internal cooling systemSNECMA·Filed 1992·Granted Mar 16, 1993·51 cites·10 claims
- 1161US5347807ACombined jet engine with RAM jet and turbojetSNECMA·Filed 1993·Granted Sep 20, 1994·24 cites·2 claims
- 1260US5327719ACircuit for ventilating compressor and turbine disksCONST DE MOTEURS D AVAIATION S·Filed 1993·Granted Jul 12, 1994·36 cites·9 claims
- 1355US7007890B2Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper positionSNECMA MOTEURS·Filed 2004·Granted Mar 7, 2006·15 cites·9 claims
- 1453US7805949B2Device for supporting and housing auxiliaries in a bypass turbojetSNECMA·Filed 2006·Granted Oct 5, 2010·4 cites·14 claims
- 1553US5410870AAircraft engine layoutSNECMA·Filed 1993·Granted May 2, 1995·24 cites·3 claims
- 1650US5806793ACooling device for a turboshaft engine on an aircraftSNECMA·Filed 1996·Granted Sep 15, 1998·27 cites·10 claims
- 1750US5284014ATurbojet-ramjet hypersonic aircraft engineSNECMA·Filed 1992·Granted Feb 8, 1994·19 cites·12 claims
- 1847US7100869B2Turboprop carrier structure and an assembly including such a carrier structureSNECMA MOTEURS·Filed 2004·Granted Sep 5, 2006·6 cites·15 claims
- 1943US6129509AParticle traps for turbo-prop engineSNECMA·Filed 1999·Granted Oct 10, 2000·16 cites·4 claims
- 2040US5275532AAxial compressor and method of carrying out maintenance on the axial compressorSNECMA·Filed 1992·Granted Jan 4, 1994·10 cites·3 claims
- 2135US2005150970A1Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling systemSNECMA MOTEURS·Filed 2004·Application pending·0 cites
- 2233US5343695ACombined jet engine provided with means for switching between two operating statesSNECMA·Filed 1993·Granted Sep 6, 1994·9 cites·3 claims
- 2332US5305600APropulsion engineSNECMA·Filed 1993·Granted Apr 26, 1994·5 cites·7 claims
- 2428US7461813B2Air input device for a turboprop engineSNECMA·Filed 2003·Granted Dec 9, 2008·0 cites·7 claims
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