Jérôme Corfa
6Patents
1h-index
17Co-inventors
40Inventor score
Filing activity: May 27, 2014 → Dec 21, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10634059B2 | Acoustic attenuation panel for a turbojet engine nacelle | Emerging Cross-Sectional Technologies | 7 | Active |
| US11293378B2 | Thrust reverser for an aircraft engine nacelle, comprising a panel for avoiding a movable slat of the wing, and nacelle associated therewith | Emerging Cross-Sectional Technologies | 1 | Active |
| US11891965B2 | Turbojet engine nacelle with a cascade thrust reverser comprising a flap control sector | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10753315B2 | Rear assembly of a turbojet engine nacelle including a fireproof sealing device | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12158122B2 | Nacelle for an aircraft propulsion assembly comprising a flap for closing a recess for the passage of an actuator | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10047634B2 | Actuator for aircraft turbine engine nacelle with notably one-piece annular rear part | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.