Inventor · disambiguated record
Georges Habarou
Also filed as: HABAROU GEORGES
15 granted patents·399 citations·filing 1986–2011
94Inventor score
Top patents by PatentIndex Score
15 records- 0197US7249462B2Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbineSNECMA·Filed 2005·Granted Jul 31, 2007·78 cites·22 claims
- 0294US8141371B1Gas turbine combustion chamber made of CMC material and subdivided into sectorsHABAROU GEORGES·Filed 2009·Granted Mar 27, 2012·56 cites·15 claims
- 0391US8257029B2Turbine ring assembly for gas turbineHABAROU GEORGES·Filed 2008·Granted Sep 4, 2012·39 cites·16 claims
- 0489US9080463B2Turbine ring assemblyDENECE FRANCK ROGER DENIS·Filed 2010·Granted Jul 14, 2015·17 cites·7 claims
- 0588US6988369B2Combustion chamber sealing ring, and a combustion chamber including such a ringSNECMA MOTEURS·Filed 2003·Granted Jan 24, 2006·43 cites·20 claims
- 0686US8496431B2Turbine ring assembly for gas turbineHABAROU GEORGES·Filed 2008·Granted Jul 30, 2013·28 cites·23 claims
- 0779US8146372B2Gas turbine combustion chamber having inner and outer walls subdivided into sectorsCARRERE BENOIT·Filed 2009·Granted Apr 3, 2012·22 cites·14 claims
- 0879US6732532B2Resilient mount for a CMC combustion chamber of a turbomachine in a metal casingSNECMA MOTEURS·Filed 2002·Granted May 11, 2004·24 cites·13 claims
- 0977US8951017B2Turbomachine blade, a rotor, a low pressure turbine, and a turbomachine fitted with such a bladeCORDIER DAMIEN·Filed 2011·Granted Feb 10, 2015·9 cites·12 claims
- 1075US8424312B2Exhaust system for gas turbineCONETE ERIC·Filed 2008·Granted Apr 23, 2013·17 cites·18 claims
- 1165US5348598AMethod of manufacturing a gun barrel provided with a liningEUROP PROPULSION·Filed 1992·Granted Sep 20, 1994·29 cites·10 claims
- 1250US6378294B1System for activating an adjustable tube by means of an elastic ring for a thrust nozzleSNECMA·Filed 2000·Granted Apr 30, 2002·10 cites·22 claims
- 1346US7168253B1Monobloc flameholder arm for an afterburner device of a bypass turbojetSNECMA MOTEURS·Filed 2004·Granted Jan 30, 2007·6 cites·19 claims
- 1444US6385965B1System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assembliesSNECMA·Filed 2000·Granted May 14, 2002·7 cites·20 claims
- 1541US4669954AAbradable turbine rings and turbines thus obtainedEUROP PROPULSION·Filed 1986·Granted Jun 2, 1987·14 cites·6 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →