Inventor · disambiguated record
Alexandre Alfred Gaston Vuillemin
Also filed as: VUILLEMIN ALEXANDRE ALFRED GAS · VUILLEMIN ALEXANDRE ALFRED GASTON
12 granted patents·3 pending applications·42 citations·filing 2007–2014
87Inventor score
Files withSNECMA9AEBERLI SEBASTIEN JEAN-PAUL2VUILLEMIN ALEXANDRE ALFRED GASTON2BODARD GUILLAUME1MOREL CEDRIC1
Top patents by PatentIndex Score
15 records- 0182US9611865B2Bypass turbojetMOREL CEDRIC·Filed 2012·Granted Apr 4, 2017·10 cites·8 claims
- 0271US8701380B2Turbine engine with nonstreamlined impellersVUILLEMIN ALEXANDRE ALFRED GASTON·Filed 2011·Granted Apr 22, 2014·7 cites·8 claims
- 0369US9617954B2Primary cowl of a turbofan comprising a rotating ring having micro-jetsSNECMA·Filed 2012·Granted Apr 11, 2017·4 cites·8 claims
- 0466US8827199B2Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assemblyAEBERLI SEBASTIEN JEAN-PAUL·Filed 2011·Granted Sep 9, 2014·7 cites·11 claims
- 0562US9885315B2Tail cone for a microjet rotary turbine engineSNECMA·Filed 2014·Granted Feb 6, 2018·2 cites·11 claims
- 0659US7810335B2Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraftSNECMA·Filed 2007·Granted Oct 12, 2010·6 cites·8 claims
- 0758US9938901B2Attachment pylon for a turbine engineSNECMA·Filed 2012·Granted Apr 10, 2018·3 cites·11 claims
- 0847US9361876B2Method of processing acoustic waves emitted at the outlet of a turbo engine of an aircraft with a dielectric-barrier discharge device and aircraft comprising such a deviceVUILLEMIN ALEXANDRE ALFRED GASTON·Filed 2011·Granted Jun 7, 2016·1 cites·8 claims
- 0941US7827802B2Variable-section flow mixer for a double-flow turbojet for a supersonic airplaneSNECMA·Filed 2008·Granted Nov 9, 2010·2 cites·6 claims
- 1039US8037687B2Bypass turbomachine with reduction of jet noiseSNECMA·Filed 2008·Granted Oct 18, 2011·0 cites·5 claims
- 1137US2008105487A1Curved lobe mixer for a converging-stream nozzle for a turbomachineSNECMA·Filed 2007·Application pending·0 cites
- 1236US7784270B2Rotary motion mixer for a converging-stream nozzle of a turbomachineSNECMA·Filed 2007·Granted Aug 31, 2010·0 cites·5 claims
- 1335US2009084111A1Turbomachine nozzle cowl having jet noise reduction patternsSNECMA·Filed 2008·Application pending·0 cites
- 1431US9422887B2Device for reducing the noise emitted by the jet of an aircraft propulsion engineBODARD GUILLAUME·Filed 2011·Granted Aug 23, 2016·0 cites·6 claims
- 1531US2012192543A1Exhaust nozzle for a bypass airplane turbojet having a deployable secondary cover and a retractable central bodyAEBERLI SEBASTIEN JEAN-PAUL·Filed 2012·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Alexandre Alfred Gaston Vuillemin files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →