Inventor · disambiguated record
Patrick Morel
Also filed as: MOREL PATRICK · MOREL PATRICK CHARLES GEORGES
12 granted patents·1 pending application·356 citations·filing 1989–2010
93Inventor score
Top patents by PatentIndex Score
13 records- 0197US7552591B2Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engineSNECMA·Filed 2006·Granted Jun 30, 2009·79 cites·11 claims
- 0292US7299621B2Three-spool by-pass turbojet with a high by-pass ratioSNECMA MOTEURS·Filed 2005·Granted Nov 27, 2007·60 cites·6 claims
- 0384US8042341B2Turbojet engine accessory gear box driveshaft; modular additional accessorySNECMA·Filed 2007·Granted Oct 25, 2011·23 cites·5 claims
- 0484US7785066B2Bleed system for a low-pressure compressor of a turbomachineSNECMA·Filed 2007·Granted Aug 31, 2010·24 cites·5 claims
- 0584US7195444B2Turbomachine with a decoupling device common to first and second bearings of its drive shaft, compressor comprising the decoupling device and decoupling deviceSNECMA·Filed 2005·Granted Mar 27, 2007·26 cites·21 claims
- 0683US5776229AOil separator rotor for lubrication enclosureSNECMA·Filed 1996·Granted Jul 7, 1998·57 cites·3 claims
- 0778US7448808B2Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangementSNECMA·Filed 2004·Granted Nov 11, 2008·27 cites·11 claims
- 0867US7661261B2Acoustic flow straightener for turbojet engine fan casingSNECMA·Filed 2008·Granted Feb 16, 2010·7 cites·11 claims
- 0965US4972357ADigital filter with integrated decimationALCATEL NV·Filed 1989·Granted Nov 20, 1990·18 cites·1 claims
- 1061US8622699B2Device adapted to be fitted with propeller bladesGALLET FRANCOIS·Filed 2010·Granted Jan 7, 2014·3 cites·17 claims
- 1154US6799416B2Device for supporting and recentering the shaft of a turbojet fan after uncouplingSNECMA MOTEURS·Filed 2003·Granted Oct 5, 2004·16 cites·3 claims
- 1252US7237959B2Breakable coupling system for a turbojet fan shaftSNECMA MOTEURS·Filed 2002·Granted Jul 3, 2007·16 cites·13 claims
- 1334US2005172610A1Turbojet having two counter-rotatable fans secured to a counter-rotatable low-pressure compressorSNECMA MOTEURS·Filed 2005·Application pending·0 cites
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