Frédéric Ridray
18Patents
3h-index
24Co-inventors
56Inventor score
Filing activity: Aug 22, 2008 → Mar 8, 2023
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 |
| US8464541B2 | Closing system for an aircraft fan shroud | Performing Operations; Transporting | 3 | Active |
| US11255293B2 | Turbofan comprising a nacelle equipped with a reverser system and a mobile cascade grill | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US8382031B2 | Fan cowl support cradle mounted on the attachment pylon and on the air inlet of the nacelle | Performing Operations; Transporting | 2 | Active |
| US11105297B2 | Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 1 | Active |
| US12420937B2 | Propulsion assembly for an aircraft, comprising a load bearer | Performing Operations; Transporting | 0 | Active |
| US11161619B2 | Turbojet engine comprising a nacelle equipped with a fan case and with a fixed structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11136938B2 | Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports | Emerging Cross-Sectional Technologies | 0 | Active |
| US11187188B2 | Turbojet including a nacelle equipped with a thrust reverser system including a hinged structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11434849B2 | Turbofan engine comprising a series of rotary blades for blocking the stream of the bypass air | 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 |
| US12344388B2 | Propulsion assembly for an aircraft, comprising a load bearer | Performing Operations; Transporting | 0 | Active |
| US10550796B2 | Turbojet engine comprising a nacelle equipped with reverser flaps | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11215141B2 | Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means | 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 |
| US11565822B2 | Propulsion assembly for an aircraft, comprising a load support | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.