MV

Marc Versaevel

SN Safran Nacelles: 20 patents #4 of 253Top 2%
SE Safran Aircraft Engines: 2 patents #588 of 1,821Top 35%
SA Safran: 1 patents #203 of 487Top 45%
📍 Moissy-Cramayel, FR: #59 of 1,676 inventorsTop 4%
Overall (All Time): #201,143 of 4,157,543Top 5%
21
Patents All Time

Issued Patents All Time

Showing 1–21 of 21 patents

Patent #TitleCo-InventorsDate
12429015 Assembly for an ejection cone of an aircraft turbomachine Tony MIOSSEC, Fabien Bravin, Vincent Devanlay, Valentin SIMEON 2025-09-30
12315486 Method for creating alveolar cores having open inner conical shapes Bertrand Desjoyeaux, Mathieu PREAU, Laurent Moreau 2025-05-27
12305592 Method for manufacturing a structure with cellular cores for a turbojet nacelle Bertrand Desjoyeaux, Mathieu PREAU, Laurent Moreau 2025-05-20
12264625 Acoustic attenuation panel and its manufacturing methods Pierre Caruel, Bertrand Desjoyeaux, Bertrand Pierre Martin Leroyer, Laurent Georges Valleroy 2025-04-01
12180891 Acoustic panel for a turbine engine Bertrand Desjoyeaux, Pierre-Yves GINI 2024-12-31
12170077 Acoustic attenuation panel for low-frequency waves Bertrand Desjoyeaux, Mathieu PREAU 2024-12-17
12129042 Acoustic sealing element Denis Guillois, Loïc Chapelain 2024-10-29
12092026 Nacelle air intake and nacelle comprising such an air intake Virginie Emmanuelle Anne-Marie Digeos, Paul Oldham, Patrick Boileau 2024-09-17
11686247 Acoustic panel for a nacelle of an aircraft propulsion unit, and related manufacturing methods Bertrand Desjoyeaux 2023-06-27
11655760 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Sébastien Laurent Marie Pascal, Jean-Michel Paul Ernest Nogues, François Chauveau 2023-05-23
11629644 Acoustic attenuation panel comprising a front skin and a central structure Jean-Philippe Ginefri, Fabrice Provost, Jeremy Quesnel, Wouter Balk, Sébastien LOUCHARD +1 more 2023-04-18
11608781 Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Sébastien Laurent Marie Pascal, Jean-Michel Paul Ernest Nogues, 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 Sébastien Laurent Marie Pascal, Jean-Michel Paul Ernest Nogues, François Chauveau 2023-02-28
11542865 Air inflow lip for turbojet nacelle Patrick Boileau, Caroline COAT-LENZOTTI, Virginie Emmanuelle Anne-Marie Digeos, Pierre-François Behaghel 2023-01-03
11401866 Active device for attenuating acoustic emissions for a turbojet engine including controlled turbines Jean-Paul Rami, Herve Hurlin, Jean-Baptiste GOULARD, Philippe Micheau, Julien Drant +3 more 2022-08-02
11220346 Acoustic attenuation panel for an aircraft propulsion unit and propulsion unit including such a panel Denis Ramage, Baptiste Cordier, Georges Jean Xavier Riou, Jacky Novi Mardjono 2022-01-11
10995038 Method for manufacturing an acoustic attenuation panel made of an oxide ceramic-matrix composite material Arnaud DELEHOUZE, Sylvain Sentis, Bertrand Desjoyeaux, Frédéric Fosse 2021-05-04
10875659 Acoustic attenuation structure with a plurality of attenuation degrees for a propulsion assembly of an aircraft Laurent Georges Valleroy, Bertrand Desjoyeaux, Patrick Gonidec 2020-12-29
10634059 Acoustic attenuation panel for a turbojet engine nacelle Jean-Paul Rami, Jérôme Corfa, François Brefort, Remko Moeys 2020-04-28
10487738 Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels Arnaud DELEHOUZE, Laurence Lemains, Pierre-François Behaghel 2019-11-26
10408165 Device with gratings for ejecting microjets in order to reduce the jet noise of a turbine engine Jacky Novi Mardjono, Philippe Gerard Chanez, Jeremy Paul Francisco Gonzalez, Maxime KOENIG, Franck Zaganelli +1 more 2019-09-10