ML

Matthieu Leyko

SN Snecma: 6 patents #141 of 1,717Top 9%
SA Safran: 5 patents #32 of 487Top 7%
SE Safran Aircraft Engines: 4 patents #317 of 1,821Top 20%
SA Saft: 1 patents #70 of 205Top 35%
Overall (All Time): #291,042 of 4,157,543Top 8%
16
Patents All Time

Issued Patents All Time

Patent #TitleCo-InventorsDate
11619380 Constant volume combustion system Pierre Jean-Baptiste METGE, Eric Conete, Gautier Mecuson 2023-04-04
11296377 Cover for an electrochemical cell with enhanced heat conduction Alexandre NARBONNE, Gerard Rigobert, Thierry Berlureau 2022-04-05
11168610 Constant-volume combustion system comprising a rotating closure element with segmented apertures Pierre Jean-Baptiste METGE, Eric Conete, Gautier Mecuson 2021-11-09
11066990 Constant-volume combustion module for a turbine engine, comprising communication-based ignition 2021-07-20
11060732 Constant volume combustion chamber with counter rotating shutter valve Pierre Jean-Baptiste METGE 2021-07-13
11047254 Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve system Julien Szydlowski 2021-06-29
10794246 Heat-exchange and noise-reduction panel for a propulsion assembly Imane Ghazlane 2020-10-06
10662874 Constant-volume combustion module for a turbine engine 2020-05-26
10550715 Gyratory-effect flow deflector of a discharge valve system, discharge valve system and turbine engine comprising such a discharge valve system Julien Szydlowski 2020-02-04
10082080 Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear Christian Sylvain Vessot 2018-09-25
10036318 Air circulation device for turbomachine Christian Sylvain Vessot 2018-07-31
9915227 Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method Jean Bertucchi, Arthur Droit 2018-03-13
9683516 Convergent-divergent nozzle for a turbine engine Jean Bertucchi, Mathieu Gaillot 2017-06-20
9540109 Turbomachine comprising a device for the cooling of a pylon Jean Bertucchi, Julien Szydlowski 2017-01-10
9488106 Assembly formed by a turbine engine and a system for attaching it to an aircraft structure Mathieu Gaillot, Jean Bertucchi 2016-11-08
9249755 Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle Julien Szydlowski, Guillaume Bodard, Jonathan Langridge 2016-02-02