Inventor · disambiguated record
Pascal Brossier
Also filed as: BROSSIER PASCAL · BROSSIER PASCAL N · BROSSIER PASCAL NOEL · BROSSIER PASCAL NOëL
13 granted patents·1 pending application·381 citations·filing 1992–2020
92Inventor score
Top patents by PatentIndex Score
14 records- 0197US6282881B1Cooling system for a turbomachine speed reducerSNECMA·Filed 2000·Granted Sep 4, 2001·148 cites·3 claims
- 0284US6622475B2Bleed system driven in simplified manner for a turbojet or turboprop engineSNECMA MOTEURS·Filed 2002·Granted Sep 23, 2003·53 cites·5 claims
- 0382US10126228B2Peeling test deviceSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Nov 13, 2018·4 cites·7 claims
- 0482US5806792ASuspension device for a turboprop engineSNECMA·Filed 1996·Granted Sep 15, 1998·74 cites·1 claims
- 0578US10302550B2Peeling test couponSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted May 28, 2019·2 cites·6 claims
- 0661US5347807ACombined jet engine with RAM jet and turbojetSNECMA·Filed 1993·Granted Sep 20, 1994·24 cites·2 claims
- 0750US5806793ACooling device for a turboshaft engine on an aircraftSNECMA·Filed 1996·Granted Sep 15, 1998·27 cites·10 claims
- 0850US5284014ATurbojet-ramjet hypersonic aircraft engineSNECMA·Filed 1992·Granted Feb 8, 1994·19 cites·12 claims
- 0945US6050522AThrust reverser for a high bypass turbofan engineSNECMA·Filed 1998·Granted Apr 18, 2000·16 cites·6 claims
- 1041US11231265B2System for measuring a bending deformation of a surface of a materialSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 25, 2022·0 cites·11 claims
- 1141US7341380B2Installation layout for two coaxial shaft linesSNECMA MOTEURS·Filed 2005·Granted Mar 11, 2008·0 cites·5 claims
- 1237US5470020ACombination turbojet engine nozzle and thrust reverserSNECMA·Filed 1994·Granted Nov 28, 1995·9 cites·10 claims
- 1334US2005100258A1Arrangement for mounting two coaxial shaftlinesFiled 2002·Application pending·0 cites
- 1432US5305600APropulsion engineSNECMA·Filed 1993·Granted Apr 26, 1994·5 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →