Inventor · disambiguated record
Stephane Rousselin
Also filed as: ROUSSELIN STEPHANE · ROUSSELIN STÉPHANE
42 granted patents·1 pending application·343 citations·filing 2005–2019
98Inventor score
Files withSNECMA20BART JACQUES RENE6SAFRAN AIRCRAFT ENGINES3MONS CLAUDE MARCEL2PIERROT ARNAUD JEAN-MARIE2
Top patents by PatentIndex Score
43 records- 0196US7372175B2Two-spool bypass turbojet with a rear electricity generator, and an air flow connection device and systemSNECMA·Filed 2005·Granted May 13, 2008·23 cites·12 claims
- 0290US7224082B2Turbomachine including an integrated electricity generatorSNECMA·Filed 2005·Granted May 29, 2007·26 cites·20 claims
- 0388US8246255B2Device for the axial locking of a guide shaft bearing in a turbomachineRABERIN LAURENT·Filed 2009·Granted Aug 21, 2012·15 cites·14 claims
- 0488US8136999B2Turbomachine shaft guidanceMONS CLAUDE MARCEL·Filed 2009·Granted Mar 20, 2012·31 cites·9 claims
- 0587US7619331B2Turbomachine with integral generator/starterSNECMA·Filed 2007·Granted Nov 17, 2009·14 cites·10 claims
- 0684US8209834B2Centering a part inside a shaftMONS CLAUDE MARCEL·Filed 2009·Granted Jul 3, 2012·26 cites·6 claims
- 0781US10907507B2Device for measuring at least one parameter of an aerodynamic flow of a turbine engine equipped with a vibratory damping means and turbine engine duct equipped with such a deviceSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Feb 2, 2021·3 cites·13 claims
- 0881US8246310B2Turbomachine fanPIERROT ARNAUD JEAN-MARIE·Filed 2008·Granted Aug 21, 2012·16 cites·11 claims
- 0980US9200594B2Gas turbine engine having fan blades of adjustable pitch with cyclic settingBOUILLER PHILIPPE PIERRE VINCENT·Filed 2010·Granted Dec 1, 2015·9 cites·17 claims
- 1080US7685828B2Electricity generation in a turbomachineSNECMA·Filed 2008·Granted Mar 30, 2010·22 cites·13 claims
- 1178US8051952B2Deoiling device and turbomachine comprising this deviceSNECMA·Filed 2009·Granted Nov 8, 2011·16 cites·6 claims
- 1277US7390167B1Compressor with centripetal air takeoffSNECMA·Filed 2006·Granted Jun 24, 2008·15 cites·20 claims
- 1375US8529208B2Rotary assembly for a turbomachine fanBRAULT MICHEL GILBERT ROLAND·Filed 2008·Granted Sep 10, 2013·11 cites·13 claims
- 1473US10519801B2Instrumented flow passage of a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 31, 2019·2 cites·9 claims
- 1573US8057160B2Device for limiting turbine overspeed in a turbomachineBART JACQUES RENE·Filed 2007·Granted Nov 15, 2011·6 cites·12 claims
- 1672US7553126B2Device for varying the section of the throat in a turbine nozzleSNECMA·Filed 2006·Granted Jun 30, 2009·13 cites·13 claims
- 1770US8882453B2Rotor element with a fluid passage and passage-blocking member and turbine engine including the rotor elementROUSSELIN STEPHANE·Filed 2010·Granted Nov 11, 2014·5 cites·9 claims
- 1870US8587780B2Device for measuring the twist of a rotating shaftGALLET FRANCOIS·Filed 2010·Granted Nov 19, 2013·4 cites·7 claims
- 1966US8074455B2Gas turbine engine with a means of driving the accessory gear box, and method of fitting said enginePIERROT ARNAUD JEAN-MARIE·Filed 2008·Granted Dec 13, 2011·10 cites·10 claims
- 2064US8127525B2System 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
- 2164US7766607B2Device for ventilating turbine disks in a gas turbine engineSNECMA·Filed 2006·Granted Aug 3, 2010·7 cites·19 claims
- 2264US7596938B2Turbomachine with a deflector systemSNECMA·Filed 2008·Granted Oct 6, 2009·8 cites·18 claims
- 2364US7334999B2Turbomachine rotor including at least one disk reinforced by a composite ringSNECMA·Filed 2006·Granted Feb 26, 2008·9 cites·23 claims
- 2462US8182202B2Coupling 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
- 2559US8172509B2Device for detecting breakage of a turbomachine shaftBART JACQUES RENE·Filed 2008·Granted May 8, 2012·7 cites·11 claims
- 2659US7855483B2Turbomachine with integral generator/starterSNECMA·Filed 2009·Granted Dec 21, 2010·5 cites·5 claims
- 2756US7568336B2Aeroengine fitted with heat exchanger meansSNECMA·Filed 2008·Granted Aug 4, 2009·7 cites·7 claims
- 2855US9823145B2Bearing nut for measuring the rotational speed of a shaft connected to a turbomachine and associated measuring deviceSNECMA·Filed 2014·Granted Nov 21, 2017·1 cites·14 claims
- 2954US7845901B2Air bleed device on a machine stator pivoting bladeSNECMA·Filed 2006·Granted Dec 7, 2010·5 cites·3 claims
- 3052US11732759B2Flexible coupling comprising bellows and torque reacting teethSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Aug 22, 2023·0 cites·10 claims
- 3152US8161727B2System 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
- 3251US8157506B2Device 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
- 3351US7479717B2Turbomachine having a device for automatically detecting ferromagnetic particles in an oil enclosureSNECMA·Filed 2005·Granted Jan 20, 2009·3 cites·9 claims
- 3449US7743598B2Sealing system for the rear lubricating chamber of a jet engineSNECMA·Filed 2006·Granted Jun 29, 2010·2 cites·6 claims
- 3542US9909444B2Measurement installation for blade failure testing in a turbomachineSNECMA·Filed 2013·Granted Mar 6, 2018·0 cites·13 claims
- 3642US8186144B2Component ventilation and pressurization in a turbomachineBEHAGHEL LAURENT DONATIEN·Filed 2008·Granted May 29, 2012·1 cites·8 claims
- 3742US7788806B2Process for manufacturing a blisk and mold for implementing the processSNECMA·Filed 2007·Granted Sep 7, 2010·0 cites·12 claims
- 3841US10513945B2Instrumented flow passage of a turbine engineSAFRAN AIRCRAFT ENGINES PI AJI·Filed 2016·Granted Dec 24, 2019·0 cites·6 claims
- 3941US9163662B2Installation of calibration gauge for measuring constraintsSNECMA·Filed 2014·Granted Oct 20, 2015·0 cites·10 claims
- 4038US2011073717A1Aircraft with a hybrid energy supplySNECMA·Filed 2009·Application pending·0 cites
- 4136US8147184B2Air intake circuit arrangement for high pressure compressor of a turbine engineDERENES JACKY RAPHAEL MICHEL·Filed 2008·Granted Apr 3, 2012·0 cites·13 claims
- 4234US8419352B2Bypass turbojetGENTILS ROMUALD·Filed 2009·Granted Apr 16, 2013·1 cites·10 claims
- 4330US9442035B2Device for classifying strain gaugesDEPOTS EMMANUEL·Filed 2012·Granted Sep 13, 2016·0 cites·12 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →