Patrick Gonidec
66Patents
18h-index
77Co-inventors
87Inventor score
Filing activity: Sep 4, 1996 → Sep 8, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5960626A | Electric control system for a turbojet engine thrust reverser including an electromechanical drive device and a locking device which are controlled by an electronic control unit | Emerging Cross-Sectional Technologies | 58 | Expired |
| US6274216A | Honeycomb structure, particularly for absorbing sound and its production process | Emerging Cross-Sectional Technologies | 47 | Expired |
| US6122892A | Ventilated honeycomb cell sandwich panel and ventilation process for such a panel | Emerging Cross-Sectional Technologies | 44 | Expired |
| US6094908A | Synchronizing control system for aircraft jet engine thrust reversers | Emerging Cross-Sectional Technologies | 43 | Expired |
| US5996937A | Variable cross-section turbofan exhaust duct with door type thrust reverser for aircraft | Emerging Cross-Sectional Technologies | 39 | Expired |
| US5974783A | Turbojet engine thrust reverser having movable rear baffle pivattally connected by forward and rear linkrods which are totally enclosed in the forward thrust mode | Mechanical Engineering; Lighting; Heating | 35 | Expired |
| US6085865A | Soundproofing panel and method of producing said panel | Emerging Cross-Sectional Technologies | 33 | Expired |
| US6148607A | Thrust reverser with lock-status display | Mechanical Engineering; Lighting; Heating | 28 | Expired |
| US6045091A | Thrust reverser with improved impact strength | Performing Operations; Transporting | 28 | Expired |
| US6151884A | Turbojet engine thrust reverser door spoilers with motion controlling drive system | Mechanical Engineering; Lighting; Heating | 27 | Expired |
| US6170255A | Turbojet thrust reverser with downstream obstacles | Mechanical Engineering; Lighting; Heating | 26 | Expired |
| US5997054A | Device for closing and locking the shutters of a thrust reverser | Emerging Cross-Sectional Technologies | 25 | Expired |
| US6216980A | System for closing a pivoting thrust reverser door | Emerging Cross-Sectional Technologies | 23 | Expired |
| US5983625A | Pivoting door thrust reverser with deflecting passage within the door | Emerging Cross-Sectional Technologies | 22 | Expired |
| US5913476A | Turbojet engine thrust reverser having hinged doors | Emerging Cross-Sectional Technologies | 22 | Expired |
| US6145786A | Latching mechanism for a jet engine thrust reverser door | Mechanical Engineering; Lighting; Heating | 22 | Expired |
| US6065285A | Thrust reverser for turbojet engine having scoop-forming doors cooperating with movable flow deflecting baffles | Mechanical Engineering; Lighting; Heating | 22 | Expired |
| US5893265A | Pivoting door thrust reverser with deflecting vane | Emerging Cross-Sectional Technologies | 18 | Expired |
| US5937636A | Pivoting door thrust reverser with controlled bypass through the rear portion of the thrust reverser door | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US6044641A | Locking system for an aircraft jet engine thrust reverser door including a plurality of locking devices arranged to prevent deformation of the thrust reverser door | Emerging Cross-Sectional Technologies | 18 | Expired |
| US6101807A | Gas flow guide for an aircraft thrust reverser | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US5765362A | Pivoting door thrust reverser with cowling mounted auxiliary panel | Mechanical Engineering; Lighting; Heating | 16 | Expired |
| US6029439A | Gas flow guide for an aircraft thrust reverser | Mechanical Engineering; Lighting; Heating | 16 | Expired |
| US6158211A | Turbojet-engine thrust reverser with scoop-doors of adjustable exhaust cross-section | Mechanical Engineering; Lighting; Heating | 16 | Expired |
| US6145301A | Thrust reverser for fan type turbojet engines using independently actuated pivoted thrust deflectors | Emerging Cross-Sectional Technologies | 15 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.