Inventor · disambiguated record
Jean Bertucchi
Also filed as: BERTUCCHI JEAN
7 granted patents·1 pending application·4 citations·filing 2011–2016
71Inventor score
Files withSNECMA4BENSILUM STEPHANE EMMANUEL DANIEL1BENSILUM STÉPHANE EMMANUEL DANIEL1GAILLOT MATHIEU1SAFRAN AIRCRAFT ENGINES1
Top patents by PatentIndex Score
8 records- 0152US9488106B2Assembly formed by a turbine engine and a system for attaching it to an aircraft structureGAILLOT MATHIEU·Filed 2012·Granted Nov 8, 2016·2 cites·5 claims
- 0247US9682783B2Pylon for fixing an aircraft engine having unducted pusher propellersBENSILUM STÉPHANE EMMANUEL DANIEL·Filed 2011·Granted Jun 20, 2017·2 cites·13 claims
- 0341US9683516B2Convergent-divergent nozzle for a turbine engineSNECMA·Filed 2012·Granted Jun 20, 2017·0 cites·5 claims
- 0439US9540109B2Turbomachine comprising a device for the cooling of a pylonSNECMA·Filed 2014·Granted Jan 10, 2017·0 cites·10 claims
- 0537US11221020B2Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 11, 2022·0 cites·10 claims
- 0635US9915227B2Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design methodSNECMA·Filed 2013·Granted Mar 13, 2018·0 cites·10 claims
- 0733US2013032642A1Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverserSNECMA·Filed 2011·Application pending·0 cites
- 0828US9341082B2Pipe having an upstream core having a sharp curvatureBENSILUM STEPHANE EMMANUEL DANIEL·Filed 2012·Granted May 17, 2016·0 cites·9 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →