Inventor · Épouville, FR

Sébastien Laurent Marie Pascal

15Patents
2h-index
25Co-inventors
50Inventor score

Filing activity: Apr 13, 2012 → Jun 17, 2022

Most-cited inventions

PatentTitleAreaCited byStatus
US9593582B2 Propulsion device having unducted counter-rotating and coaxial rotors Emerging Cross-Sectional Technologies 10 Active
US10018152B2 Turbojet engine nacelle including a thrust reversing device with doors, including inner flanks on the sides of an opening Mechanical Engineering; Lighting; Heating 2 Active
US10036349B2 Afterbody for a turbojet engine comprising a nozzle provided with a thrust reverser system that incorporates a crown of noise-reducing chevrons Mechanical Engineering; Lighting; Heating 0 Active
US11913403B2 Door thrust reverser comprising a deflector for redirecting an air flow in the upstream direction Mechanical Engineering; Lighting; Heating 0 Active
US11952963B2 Thrust reverser with anti-buckling actuating system Emerging Cross-Sectional Technologies 0 Active
US11591960B2 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air 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
US11655760B2 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Emerging Cross-Sectional Technologies 0 Active
US12044193B2 Thrust reverser comprising doors and at least one retractable deflector for closing a lateral opening 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
US12140107B2 Thrust reverser for the nacelle of an aircraft turbofan engine Mechanical Engineering; Lighting; Heating 0 Active
US12006892B2 Thrust reverser comprising doors forming an upward air deflection opening in the open position Emerging Cross-Sectional Technologies 0 Active
US9481449B2 Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine Emerging Cross-Sectional Technologies 0 Active
US11608781B2 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Emerging Cross-Sectional Technologies 0 Active
US12049853B2 Thrust reverser for an aircraft bypass turbojet engine nacelle Emerging Cross-Sectional Technologies 0 Active

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.