Inventor · disambiguated record
Christophe Thorel
Also filed as: THOREL CHRISTOPHE · THOREL CHRISTOPHE J F · THOREL CHRISTOPHE JEAN FRANÇOIS
8 granted patents·3 pending applications·150 citations·filing 1993–2023
86Inventor score
Top patents by PatentIndex Score
11 records- 0180US5615547ASystem for regulating oil and fuel temperatures of a turbojet engineSNECMA·Filed 1996·Granted Apr 1, 1997·86 cites·7 claims
- 0275US8540185B2Modular air inlet lip with electric defrosting for a turbojet podVAUCHEL GUY BERNARD·Filed 2007·Granted Sep 24, 2013·13 cites·11 claims
- 0369US8231332B2Air inlet shroud structureVAUCHEL GUY BERNARD·Filed 2007·Granted Jul 31, 2012·9 cites·11 claims
- 0465US5367874AIntegral composite gas turbine afterburner structureSNECMA·Filed 1993·Granted Nov 29, 1994·27 cites·8 claims
- 0548US9109509B2Unit for an aircraft thrusterAIRCELLE SA·Filed 2012·Granted Aug 18, 2015·1 cites·8 claims
- 0647US11719192B2Acoustic attenuation panel for an aircraft jet engine nacelleSAFRAN NACELLES·Filed 2020·Granted Aug 8, 2023·0 cites·11 claims
- 0747US5359849AAfterburner assembly for a gas turbine engineSNECMA·Filed 1993·Granted Nov 1, 1994·14 cites·36 claims
- 0845US12065985B2Sealing assembly for a turbine ejection coneSAFRAN CERAM·Filed 2021·Granted Aug 20, 2024·0 cites·12 claims
- 0939US2025188887A1Ejection cone for an aircraft turbine engineSAFRAN NACELLES·Filed 2023·Application pending·0 cites
- 1039US2009107108A1Nacell for bypass engine with high bypass ratioVAUCHEL GUY BERNARD·Filed 2007·Application pending·0 cites
- 1137US2014086678A1Assembly for an aircraft nacelleAIRCELLE SA·Filed 2013·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →