Inventor · disambiguated record
Jean-Claude Taillant
Also filed as: TAILLANT JEAN-CLAUDE · TAILLANT JEAN-CLAUDE C · TAILLANT JEAN-CLAUDE CHRISTIAN
23 granted patents·1 pending application·748 citations·filing 1991–2022
96Inventor score
Files withSNECMA11SNECMA MOTEURS6SAFRAN AIRCRAFT ENGINES4BLANCHARD STEPHANE PIERRE GUILLAUME1TAILLANT JEAN-CLAUDE CHRISTIAN1
Top patents by PatentIndex Score
24 records- 0189US5993156ATurbine vane cooling systemSNECMA·Filed 1998·Granted Nov 30, 1999·122 cites·7 claims
- 0288US8336317B2Ventilation for a turbine wheel in a turbine engineBLANCHARD STEPHANE PIERRE GUILLAUME·Filed 2010·Granted Dec 25, 2012·13 cites·9 claims
- 0388US5222358ASystem for removably mounting a pre-vaporizing bowl to a combustion chamberSNECMA·Filed 1992·Granted Jun 29, 1993·66 cites·15 claims
- 0485US7011493B2Turbomachine with cooled ring segmentsSNECMA MOTEURS·Filed 2004·Granted Mar 14, 2006·45 cites·21 claims
- 0584US8979489B2Low pressure turbine for an aircraft turbomachine, comprising a segmented nozzle with an improved designTAILLANT JEAN-CLAUDE CHRISTIAN·Filed 2011·Granted Mar 17, 2015·12 cites·11 claims
- 0683US6334755B1Turbomachine including a device for supplying pressurized gasSNECMA MOTEURS·Filed 2000·Granted Jan 1, 2002·52 cites·8 claims
- 0782US5816776ALabyrinth disk with built-in stiffener for turbomachine rotorSNECMA·Filed 1997·Granted Oct 6, 1998·86 cites·7 claims
- 0880US5599170ASeal for gas turbine rotor bladesSNECMA·Filed 1995·Granted Feb 4, 1997·68 cites·25 claims
- 0975US5173024AFixing arrangement for mounting an annular member on a disk of a turboshaft engineSNECMA·Filed 1991·Granted Dec 22, 1992·63 cites·7 claims
- 1074US5980201ADevice for blowing gases for regulating clearances in a gas turbine engineSNECMA·Filed 1997·Granted Nov 9, 1999·61 cites·14 claims
- 1173US5772398ACooled turbine guide vaneSNECMA·Filed 1996·Granted Jun 30, 1998·59 cites·4 claims
- 1262US6787947B2Cooling the upstream end plate of a high pressure turbine by means of a system of dual injectors at the end of the combustion chamberSNECMA MOTEURS·Filed 2003·Granted Sep 7, 2004·23 cites·6 claims
- 1360US7140840B2Turboshaft engine comprising two elements connected to each other with the interposition of a sealSNECMA MOTEURS·Filed 2004·Granted Nov 28, 2006·17 cites·11 claims
- 1457US12305579B2Aircraft turbomachine comprising an electric machineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted May 20, 2025·0 cites·7 claims
- 1555US7458773B2Turbomachine with contrarotating fansSNECMA·Filed 2005·Granted Dec 2, 2008·6 cites·14 claims
- 1654US6916151B2Ventilation device for a high pressure turbine rotor of a turbomachineSNECMA MOTEURS·Filed 2004·Granted Jul 12, 2005·15 cites·4 claims
- 1748US12416248B2Sleeve mounted onto a low-pressure shaft in a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Sep 16, 2025·0 cites·25 claims
- 1847US12460550B2Fan module equipped with an oil transfer deviceSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Nov 4, 2025·0 cites·20 claims
- 1946US12331647B2System for controlling the pitch setting of a propeller vane for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 17, 2025·0 cites·19 claims
- 2040US5645398AUnsectored, one piece distributor of a turbojet turbine statorSNECMA·Filed 1995·Granted Jul 8, 1997·17 cites·4 claims
- 2139US7036320B2Gas turbine with stator shroud in the cavity beneath the chamberSNECMA MOTEURS·Filed 2003·Granted May 2, 2006·5 cites·12 claims
- 2232US5752804ASectored, one-piece nozzle of a turbine engine turbine statorSNECMA·Filed 1995·Granted May 19, 1998·11 cites·3 claims
- 2331US5915919ALayout and process for adjusting the diameter of a stator ringSNECMA·Filed 1997·Granted Jun 29, 1999·7 cites·12 claims
- 2431US2005201859A1Gas turbine ventilation circuitryFiled 2003·Application pending·0 cites
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