Matthieu Leyko
17Patents
1h-index
14Co-inventors
43Inventor score
Filing activity: Aug 24, 2012 → Dec 21, 2018
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9249755B2 | Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle | Emerging Cross-Sectional Technologies | 2 | Active |
| US10550715B2 | Gyratory-effect flow deflector of a discharge valve system, discharge valve system and turbine engine comprising such a discharge valve system | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11060732B2 | Constant volume combustion chamber with counter rotating shutter valve | Emerging Cross-Sectional Technologies | 1 | Active |
| US9488106B2 | Assembly formed by a turbine engine and a system for attaching it to an aircraft structure | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11047254B2 | Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve system | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10082080B2 | Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear | Emerging Cross-Sectional Technologies | 1 | Active |
| US11066990B2 | Constant-volume combustion module for a turbine engine, comprising communication-based ignition | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9683516B2 | Convergent-divergent nozzle for a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9726111B2 | Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method | General | 0 | Revoked |
| US10794246B2 | Heat-exchange and noise-reduction panel for a propulsion assembly | Emerging Cross-Sectional Technologies | 0 | Active |
| US9915227B2 | Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method | Emerging Cross-Sectional Technologies | 0 | Active |
| US10662874B2 | Constant-volume combustion module for a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9540109B2 | Turbomachine comprising a device for the cooling of a pylon | Emerging Cross-Sectional Technologies | 0 | Active |
| US11296377B2 | Cover for an electrochemical cell with enhanced heat conduction | Emerging Cross-Sectional Technologies | 0 | Active |
| US11619380B2 | Constant volume combustion system | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10036318B2 | Air circulation device for turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| US11168610B2 | Constant-volume combustion system comprising a rotating closure element with segmented apertures | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.