Inventor · disambiguated record
Matthieu Leyko
Also filed as: LEYKO MATTHIEU
16 granted patents·2 pending applications·8 citations·filing 2012–2018
86Inventor score
Top patents by PatentIndex Score
18 records- 0167US11060732B2Constant volume combustion chamber with counter rotating shutter valveSAFRAN·Filed 2018·Granted Jul 13, 2021·1 cites·5 claims
- 0267US10550715B2Gyratory-effect flow deflector of a discharge valve system, discharge valve system and turbine engine comprising such a discharge valve systemSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Feb 4, 2020·1 cites·12 claims
- 0365US11047254B2Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve systemSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 29, 2021·1 cites·12 claims
- 0463US10082080B2Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gearSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 25, 2018·1 cites·8 claims
- 0560US11296377B2Cover for an electrochemical cell with enhanced heat conductionACCUMULATEURS FIXES·Filed 2018·Granted Apr 5, 2022·0 cites·18 claims
- 0659US9249755B2Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzleSNECMA·Filed 2013·Granted Feb 2, 2016·2 cites·15 claims
- 0755US11619380B2Constant volume combustion systemSAFRAN·Filed 2018·Granted Apr 4, 2023·0 cites·3 claims
- 0852US9488106B2Assembly 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
- 0945US11168610B2Constant-volume combustion system comprising a rotating closure element with segmented aperturesSAFRAN·Filed 2018·Granted Nov 9, 2021·0 cites·13 claims
- 1044US10794246B2Heat-exchange and noise-reduction panel for a propulsion assemblySAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 6, 2020·0 cites·25 claims
- 1142US10036318B2Air circulation device for turbomachineSNECMA·Filed 2015·Granted Jul 31, 2018·0 cites·19 claims
- 1241US9683516B2Convergent-divergent nozzle for a turbine engineSNECMA·Filed 2012·Granted Jun 20, 2017·0 cites·5 claims
- 1341US2020063967A1Annular combustion chamber with continuous detonation waveSAFRAN·Filed 2017·Application pending·0 cites
- 1440US10662874B2Constant-volume combustion module for a turbine engineSAFRAN·Filed 2016·Granted May 26, 2020·0 cites·7 claims
- 1539US9540109B2Turbomachine comprising a device for the cooling of a pylonSNECMA·Filed 2014·Granted Jan 10, 2017·0 cites·10 claims
- 1638US11066990B2Constant-volume combustion module for a turbine engine, comprising communication-based ignitionSAFRAN·Filed 2016·Granted Jul 20, 2021·0 cites·7 claims
- 1737US2012247083A1Porous core cowling for a turbojet engineLEYKO MATTHIEU·Filed 2012·Application pending·0 cites
- 1835US9915227B2Discharge 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
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