Inventor · disambiguated record
Jackie Raymond Julien Prouteau
Also filed as: PROUTEAU JACKIE · PROUTEAU JACKIE RAYMOND JULIEN
11 granted patents·2 pending applications·80 citations·filing 2000–2016
88Inventor score
Top patents by PatentIndex Score
13 records- 0171US6276126B1Axisymmetric, directable and adjustable turbojet-engine exhaust nozzleSNECMA·Filed 2000·Granted Aug 21, 2001·22 cites·10 claims
- 0268US7784284B2Exhaust assembly forming a horizontal propulsion gas elbow in an aircraftSNECMA·Filed 2007·Granted Aug 31, 2010·9 cites·18 claims
- 0368US7310939B2Device for reducing the jet noise of a turbomachineSNECMA·Filed 2004·Granted Dec 25, 2007·20 cites·4 claims
- 0464US10167814B2Turbine engine nozzle having confluent streams and including a core cowl with overlapping flapsSNECMA·Filed 2014·Granted Jan 1, 2019·3 cites·12 claims
- 0564US8276388B2Optimizing an anti-coke film in an injector system for a gas turbine engineCAYRE ALAIN·Filed 2008·Granted Oct 2, 2012·9 cites·13 claims
- 0663US7581400B2Elbow-shaped propulsion gas exhaust assembly in an aircraftSNECMA·Filed 2007·Granted Sep 1, 2009·4 cites·20 claims
- 0757US10946975B2Turbomachine comprising a trap for foreign objects circulating in an air flowSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 16, 2021·1 cites·15 claims
- 0854US7681400B2Exhaust assembly forming a horizontal propulsion gas elbow in an aircraftSNECMA·Filed 2007·Granted Mar 23, 2010·4 cites·18 claims
- 0945US6993914B2Convergent-divergent turbojet nozzleSNECMA MOTEURS·Filed 2004·Granted Feb 7, 2006·7 cites·11 claims
- 1044US9976480B2Fluid intake systemSNECMA·Filed 2014·Granted May 22, 2018·1 cites·7 claims
- 1137US2018142562A1Turbine Engine Comprising a Lobed Mixer Having ScoopsSAFRAN AIRCRAFT ENGINES·Filed 2016·Application pending·0 cites
- 1236US2015028129A1Biconical exhaust cone for a civil aviation jet engineSNECMA·Filed 2014·Application pending·0 cites
- 1334US7631486B2Thrust orienting nozzleSNECMA·Filed 2006·Granted Dec 15, 2009·0 cites·14 claims
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