SP

Sébastien Laurent Marie Pascal

SN Safran Nacelles: 11 patents #8 of 253Top 4%
SN Snecma: 3 patents #318 of 1,717Top 20%
AI Aircelle: 2 patents #60 of 206Top 30%
SE Sentera: 1 patents #66 of 178Top 40%
📍 Épouville, FR: #1 of 4 inventorsTop 25%
Overall (All Time): #311,333 of 4,157,543Top 8%
15
Patents All Time

Issued Patents All Time

Showing 1–15 of 15 patents

Patent #TitleCo-InventorsDate
12152552 Front frame and deflection grid of a thrust reverser of an aircraft nacelle Xavier Cazuc, Vincent Peyron, Jean-Philippe Joret 2024-11-26
12140107 Thrust reverser for the nacelle of an aircraft turbofan engine Luigi Bisanti 2024-11-12
12049853 Thrust reverser for an aircraft bypass turbojet engine nacelle Xavier Cazuc, Jean-Philippe Joret, Vincent Peyron 2024-07-30
12044193 Thrust reverser comprising doors and at least one retractable deflector for closing a lateral opening Patrick Gonidec, Alexandre Phi, Paul Ferrey 2024-07-23
12006892 Thrust reverser comprising doors forming an upward air deflection opening in the open position 2024-06-11
11987372 System with locking indicator for a nacelle element, comprising a removable key for locking and controlling the indicator Alexandre Phi, Vincent Peyron 2024-05-21
11952963 Thrust reverser with anti-buckling actuating system Xavier Cazuc, Vincent Dutot, Stephane Riquier, Patrick Boileau, Fabien Jourdan 2024-04-09
11913403 Door thrust reverser comprising a deflector for redirecting an air flow in the upstream direction Laurent Georges Valleroy, Paul Ferrey 2024-02-27
11655760 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Jean-Michel Paul Ernest Nogues, Marc Versaevel, François Chauveau 2023-05-23
11608781 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Jean-Michel Paul Ernest Nogues, Marc Versaevel, François Chauveau 2023-03-21
11591960 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Jean-Michel Paul Ernest Nogues, Marc Versaevel, François Chauveau 2023-02-28
10036349 Afterbody for a turbojet engine comprising a nozzle provided with a thrust reverser system that incorporates a crown of noise-reducing chevrons Irwin Pierre Robert Kernemp, Jonathan Langridge, Denis Guillois, Gerard Clere, Loïc Chapelain 2018-07-31
10018152 Turbojet engine nacelle including a thrust reversing device with doors, including inner flanks on the sides of an opening Alexandre Breton 2018-07-10
9593582 Propulsion device having unducted counter-rotating and coaxial rotors Clement Marcel Maurice Dejeu, Jerome Talbotec, Michael Leborgne, Ingrid Lepot 2017-03-14
9481449 Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine 2016-11-01