Frédéric Piard
14Patents
3h-index
23Co-inventors
52Inventor score
Filing activity: Nov 27, 2017 → Oct 24, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10830089B2 | Turbofan comprising a series of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 6 | Active |
| US10690088B2 | Jet engine comprising a nacelle equipped with reverser flaps | Emerging Cross-Sectional Technologies | 4 | Active |
| US10995700B2 | Jet engine comprising a nacelle equipped with reverser flaps | Emerging Cross-Sectional Technologies | 3 | Active |
| US11255293B2 | Turbofan comprising a nacelle equipped with a reverser system and a mobile cascade grill | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10655563B2 | Turbofan nacelle including a reverser flap | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10836503B2 | Air intake structure for an aircraft nacelle | Emerging Cross-Sectional Technologies | 1 | Active |
| US11161619B2 | Turbojet engine comprising a nacelle equipped with a fan case and with a fixed structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11168644B2 | Jet engine comprising a nacelle equipped with a reverser system comprising inner doors and outer flaps | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11187188B2 | Turbojet including a nacelle equipped with a thrust reverser system including a hinged structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12139267B2 | Assembly for an aircraft nacelle and comprising a support panel, a thermal protection element and a fastening system | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11072433B2 | Aircraft cowl locking system | Fixed Constructions | 0 | Active |
| US11975858B2 | Aircraft nacelle comprising a connection between ducts comprising flanges which are oriented towards the interior, and aircraft comprising at least one nacelle of this type | Performing Operations; Transporting | 0 | Active |
| US10550796B2 | Turbojet engine comprising a nacelle equipped with reverser flaps | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11143141B2 | Nacelle equipped with a thrust-reversing system comprising doors and anti-vibration systems for the doors in stowed position | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.