Inventor · disambiguated record
Jacques Rene Bart
Also filed as: BART JACQUES · BART JACQUES R · BART JACQUES RENE · BART JACQUES RENÉ
27 granted patents·1 pending application·556 citations·filing 1984–2013
96Inventor score
Top patents by PatentIndex Score
28 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
- 0296US5157915APod for a turbofan aero engine of the forward contrafan type having a very high bypass ratioSNECMA·Filed 1991·Granted Oct 27, 1992·168 cites·9 claims
- 0394US8794922B2Assembly between a compressor shaft trunnion and a bevel gear for driving an accessory gearbox of a turbomachineBART JACQUES RENÉ·Filed 2011·Granted Aug 5, 2014·32 cites·9 claims
- 0492US7412819B2Turbojet architecture with two fans at the frontSNECMA·Filed 2005·Granted Aug 19, 2008·33 cites·10 claims
- 0592US7299621B2Three-spool by-pass turbojet with a high by-pass ratioSNECMA MOTEURS·Filed 2005·Granted Nov 27, 2007·60 cites·6 claims
- 0688US4565492ASealing device for turbine blades of a turbojet engineSNECMA·Filed 1984·Granted Jan 21, 1986·62 cites·15 claims
- 0778US9759088B2Device for de-icing a turbomachine separatorBELMONTE OLIVIER·Filed 2012·Granted Sep 12, 2017·6 cites·12 claims
- 0878US8051952B2Deoiling device and turbomachine comprising this deviceSNECMA·Filed 2009·Granted Nov 8, 2011·16 cites·6 claims
- 0976US7661928B2Device for rotationally locking a clamping nut for a component on a shaft, clamping nut and shaft comprising it, and aircraft engine equipped therewithSNECMA·Filed 2006·Granted Feb 16, 2010·8 cites·20 claims
- 1073US8057160B2Device for limiting turbine overspeed in a turbomachineBART JACQUES RENE·Filed 2007·Granted Nov 15, 2011·6 cites·12 claims
- 1166US8919133B2Double-body gas turbine engine provided with an inter-shaft bearingBART JACQUES RENÉ·Filed 2010·Granted Dec 30, 2014·5 cites·9 claims
- 1265US10385872B2Variable pitch rectifier for a turbomachine compressor comprising two inner ringsSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Aug 20, 2019·3 cites·12 claims
- 1364US10036277B2Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing deviceSNECMA·Filed 2013·Granted Jul 31, 2018·2 cites·13 claims
- 1464US8127525B2System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engineBART JACQUES RENE·Filed 2008·Granted Mar 6, 2012·8 cites·8 claims
- 1564US7596938B2Turbomachine with a deflector systemSNECMA·Filed 2008·Granted Oct 6, 2009·8 cites·18 claims
- 1663US7828521B2Turbine module for a gas-turbine engineSNECMA·Filed 2005·Granted Nov 9, 2010·8 cites·16 claims
- 1762US9429030B2Device for locking a root of a rotor bladeBART JACQUES RENE·Filed 2011·Granted Aug 30, 2016·2 cites·12 claims
- 1862US9366183B2System for attaching a turbojet engine spinnerSNECMA·Filed 2013·Granted Jun 14, 2016·2 cites·10 claims
- 1962US8312702B2Oil recovery deviceBART JACQUES RENE·Filed 2009·Granted Nov 20, 2012·7 cites·5 claims
- 2062US8182202B2Coupling device for a turbine upstream guide vane, a turbine comprising same, and aircraft engine fitted therewithBART JACQUES RENE·Filed 2007·Granted May 22, 2012·5 cites·21 claims
- 2161US7097415B2Low-pressure turbine of a turbomachineSNECMA MOTEURS·Filed 2004·Granted Aug 29, 2006·18 cites·2 claims
- 2259US8172509B2Device for detecting breakage of a turbomachine shaftBART JACQUES RENE·Filed 2008·Granted May 8, 2012·7 cites·11 claims
- 2352US8161727B2System providing braking in a gas turbine engine in the event of the turbine shaft breakingBART JACQUES RENE·Filed 2008·Granted Apr 24, 2012·4 cites·9 claims
- 2451US8157506B2Device for supplying ventilation air to the low pressure blades of a gas turbine engineBART JACQUES RENE·Filed 2008·Granted Apr 17, 2012·3 cites·9 claims
- 2549US7743598B2Sealing system for the rear lubricating chamber of a jet engineSNECMA·Filed 2006·Granted Jun 29, 2010·2 cites·6 claims
- 2649US7507072B2Turbine module for a gas-turbine engine with rotor that includes a monoblock bodySNECMA·Filed 2005·Granted Mar 24, 2009·2 cites·14 claims
- 2734US2005172610A1Turbojet having two counter-rotatable fans secured to a counter-rotatable low-pressure compressorSNECMA MOTEURS·Filed 2005·Application pending·0 cites
- 2832US9897004B2Oil discharge device and turbomachine comprising such a deviceROCHE AMANDINE·Filed 2011·Granted Feb 20, 2018·0 cites·16 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →