Inventor · disambiguated record
Laurent Gilles Dezouche
Also filed as: DEZOUCHE LAURENT GILLES
9 granted patents·1 pending application·48 citations·filing 2005–2020
83Inventor score
Top patents by PatentIndex Score
10 records- 0189US7887286B2Sector of a compressor guide vanes assembly or a sector of a turbomachine nozzle assemblySNECMA·Filed 2007·Granted Feb 15, 2011·25 cites·18 claims
- 0279US8794908B2Stator stage for turbomachine compressorDEZOUCHE LAURENT GILLES·Filed 2011·Granted Aug 5, 2014·9 cites·13 claims
- 0365US7753651B2Balancing flyweight, rotor disk equipped therewith, rotor and aircraft engine comprising themSNECMA·Filed 2007·Granted Jul 13, 2010·7 cites·19 claims
- 0453US7419360B2Rotor disk for a turbomachineSNECMA·Filed 2005·Granted Sep 2, 2008·5 cites·12 claims
- 0549US10337527B2Turbomachine blade, comprising intersecting partitions for circulation of air in the direction of the trailing edgeSNECMA·Filed 2015·Granted Jul 2, 2019·0 cites·14 claims
- 0648US9709072B2Angular diffuser sector for a turbine engine compressor, with a vibration damper wedgeSNECMA·Filed 2013·Granted Jul 18, 2017·0 cites·12 claims
- 0745US7540714B1Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising themSNECMA·Filed 2006·Granted Jun 2, 2009·2 cites·8 claims
- 0843US9879549B2Aircraft engine annular shroud comprising an opening for the insertion of bladesDEZOUCHE LAURENT GILLES·Filed 2012·Granted Jan 30, 2018·0 cites·12 claims
- 0937US2012128482A1Outer shell sector for a bladed ring for an aircraft turbomachine stator, including vibration damping shimsDEZOUCHE LAURENT GILLES·Filed 2010·Application pending·0 cites
- 1036US11767767B2Turbomachine stator sector having flexible regions subjected to high stressSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 26, 2023·0 cites·10 claims
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