Laurent Georges Valleroy
22Patents
8h-index
32Co-inventors
75Inventor score
Filing activity: Jun 22, 1994 → Dec 14, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5725182A | Turbo fan engine thrust reverser | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US5970704A | Pivoting door thrust reverser with sliding panel | Emerging Cross-Sectional Technologies | 21 | Expired |
| US5615549A | Thrust reverser for a fan-type turbojet engine | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US5775097A | Turbojet engine thrust reverser with biased baffles | Emerging Cross-Sectional Technologies | 16 | Expired |
| US8245815B2 | Cellular-core structure for an acoustic panel | Emerging Cross-Sectional Technologies | 16 | Active |
| US8047326B2 | Method for making an acoustic absorption panel in particular for the nacelle of an aircraft engine | Emerging Cross-Sectional Technologies | 16 | Active |
| US5473886A | Thrust reverser with aerodynamically cooled baffle | Emerging Cross-Sectional Technologies | 13 | Expired |
| US9027884B2 | Method for making a nacelle de-icing element | Emerging Cross-Sectional Technologies | 8 | Active |
| US8985506B2 | Air intake for aircraft nacelle, and propulsion assembly including such air intake | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US8745966B2 | Mobile thrust reverser cowl and thrust reverser provided with such a cowl | Emerging Cross-Sectional Technologies | 2 | Active |
| US11624339B2 | Aircraft turbojet engine nacelle, propulsion unit and aircraft including such a nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US10875659B2 | Acoustic attenuation structure with a plurality of attenuation degrees for a propulsion assembly of an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US12264625B2 | Acoustic attenuation panel and its manufacturing methods | Emerging Cross-Sectional Technologies | 0 | Active |
| US11692480B2 | Air intake scoop for an aircraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9341083B2 | Turbojet engine nacelle with downstream section | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11866178B2 | Air intake of an aircraft turbine engine nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US11913403B2 | Door thrust reverser comprising a deflector for redirecting an air flow in the upstream direction | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9617955B2 | Cascade thrust reverser for an aircraft turbojet engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12258925B2 | Thrust reverser comprising pivoting half-assemblies and a connecting beam for the half-assemblies at the six o'clock position | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11390394B2 | Nacelle for an aircraft turbojet engine provided with a device for detecting deformation of its movable structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12258924B2 | Thrust reverser with door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior | Emerging Cross-Sectional Technologies | 0 | Active |
| US12085042B2 | Position sensor for aircraft nacelle thrust reverser door | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.