Inventor · disambiguated record
Pierre Camy
Also filed as: CAMY PIERRE
8 granted patents·132 citations·filing 1999–2014
87Inventor score
Top patents by PatentIndex Score
8 records- 0194US8141371B1Gas turbine combustion chamber made of CMC material and subdivided into sectorsHABAROU GEORGES·Filed 2009·Granted Mar 27, 2012·56 cites·15 claims
- 0279US8146372B2Gas turbine combustion chamber having inner and outer walls subdivided into sectorsCARRERE BENOIT·Filed 2009·Granted Apr 3, 2012·22 cites·14 claims
- 0379US6732532B2Resilient mount for a CMC combustion chamber of a turbomachine in a metal casingSNECMA MOTEURS·Filed 2002·Granted May 11, 2004·24 cites·13 claims
- 0471US9267531B2Assembly providing a connection that is self tightening with temperatureHERAKLES·Filed 2014·Granted Feb 23, 2016·4 cites·20 claims
- 0550US6378294B1System 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
- 0646US7168253B1Monobloc flameholder arm for an afterburner device of a bypass turbojetSNECMA MOTEURS·Filed 2004·Granted Jan 30, 2007·6 cites·19 claims
- 0744US6385965B1System 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
- 0827US6170256B1Anchor device for a member for actuating a steerable nozzleSNECMA·Filed 1999·Granted Jan 9, 2001·3 cites·14 claims
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