Inventor · disambiguated record
Guillaume Sevi
Also filed as: SEVI GUILLAUME
17 granted patents·1 pending application·76 citations·filing 2002–2020
92Inventor score
Top patents by PatentIndex Score
18 records- 0182US9091445B2Guiding a sparkplug in a turbine engine combustion chamberBUNEL JACQUES MARCEL ARTHUR·Filed 2010·Granted Jul 28, 2015·4 cites·12 claims
- 0274US11060418B2Turbomachine exhaust casing and method for manufacturing sameSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jul 13, 2021·1 cites·17 claims
- 0374US6966189B2System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamberSNECMA MOTEURS·Filed 2004·Granted Nov 22, 2005·16 cites·10 claims
- 0473US9310083B2Combustion chamber for an aircraft engine, and method for attaching an injection system in a combustion chamber of an aircraft engineBUNEL JACQUES MARCEL ARTHUR·Filed 2011·Granted Apr 12, 2016·5 cites·14 claims
- 0573US9080771B2Combustion chamber having a ventilated spark plugBUNEL JACQUES MARCEL ARTHUR·Filed 2010·Granted Jul 14, 2015·4 cites·6 claims
- 0673US7673460B2System of attaching an injection system to a turbojet combustion chamber baseSNECMA·Filed 2006·Granted Mar 9, 2010·14 cites·13 claims
- 0762US9188064B2Fuel injection system for turbojet engine and method of assembling such an injection systemBUNEL JACQUES MARCEL ARTHUR·Filed 2011·Granted Nov 17, 2015·2 cites·15 claims
- 0861US10746056B2Reinforced exhaust casing and manufacturing methodSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 18, 2020·1 cites·9 claims
- 0961US8425184B2Turbine shroud ring with rotation proofing recessDRUEZ BRUNO·Filed 2010·Granted Apr 23, 2013·4 cites·14 claims
- 1058US7568350B2Combustion chamber for a turbomachineSNECMA·Filed 2006·Granted Aug 4, 2009·5 cites·16 claims
- 1155US7117682B1Turbojet axisymmetric nozzle controlled hot flap shutterSNECMA MOTEURS·Filed 2004·Granted Oct 10, 2006·10 cites·6 claims
- 1253US10677100B2Handling fitting with movable jaws for a turbomachine casingSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 9, 2020·0 cites·12 claims
- 1351US11261756B2Method for manufacturing a turbomachine exhaust casing from segments welded togetherSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Mar 1, 2022·0 cites·7 claims
- 1451US8261556B2Device for guiding an element in an orifice in a wall of a turbomachine combustion chamberAUDIN PATRICK·Filed 2008·Granted Sep 11, 2012·7 cites·10 claims
- 1549US7004189B2Lubrication cutoff deviceSNECMA MOTEURS·Filed 2002·Granted Feb 28, 2006·3 cites·17 claims
- 1640US7520135B2Variable-section turbomachine nozzleSNECMA·Filed 2005·Granted Apr 21, 2009·0 cites·11 claims
- 1735US2006086093A1Variable-section turbomachine nozzle with a one-piece control lever supportSNECMA·Filed 2005·Application pending·0 cites
- 1834US11859508B2Aircraft turboshaft engine compressor comprising a device for immobilising a retaining annulusSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 2, 2024·0 cites·19 claims
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