Vincent Peyron
20Patents
3h-index
23Co-inventors
59Inventor score
Filing activity: Nov 19, 2012 → Mar 22, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9127623B2 | Thrust reverser device | Emerging Cross-Sectional Technologies | 11 | Active |
| US8939713B2 | Aerodynamic element for an aircraft nacelle | Performing Operations; Transporting | 4 | Active |
| US9382814B2 | Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device | Emerging Cross-Sectional Technologies | 3 | Active |
| US11772810B2 | Aircraft nacelle comprising at least one heat exchanger | Emerging Cross-Sectional Technologies | 1 | Active |
| US10745140B2 | Locking device for pivoting cowls of a thrust reverser | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11891185B2 | Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure | Emerging Cross-Sectional Technologies | 1 | Active |
| US11698004B2 | Aircraft propulsion assembly comprising air-liquid heat exchangers | Emerging Cross-Sectional Technologies | 0 | Active |
| US11987372B2 | System with locking indicator for a nacelle element, comprising a removable key for locking and controlling the indicator | Performing Operations; Transporting | 0 | Active |
| US12331699B2 | Actuating system for a cascade thrust reverser | Emerging Cross-Sectional Technologies | 0 | Active |
| US12049853B2 | Thrust reverser for an aircraft bypass turbojet engine nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US12152552B2 | Front frame and deflection grid of a thrust reverser of an aircraft nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US10633103B2 | Propulsion unit for an aircraft and method for opening a movable cowl of said propulsion unit | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11883874B2 | Method for manufacturing a structural surface heat exchanger for a nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US11230973B2 | Heat-transfer fluid for a cooling system of an aircraft turbojet engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US9341083B2 | Turbojet engine nacelle with downstream section | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9617955B2 | Cascade thrust reverser for an aircraft turbojet engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11199158B2 | Thrust reverser with movable cascades for an aircraft propulsion unit and related mounting and dismounting methods | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11268443B2 | Turbine engine nacelle comprising a cooling device | Emerging Cross-Sectional Technologies | 0 | Active |
| US11512638B2 | Surface heat-exchanger for a cooling system of an aircraft turbojet engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US11959439B2 | Thrust reverser provided with cable kinematics for scoop flaps | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.