Issued Patents 2024
Showing 1–10 of 10 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 12158122 | Nacelle for an aircraft propulsion assembly comprising a flap for closing a recess for the passage of an actuator | Romain Gardel, Pierre-Alain Reboul, Jérôme Corfa, Thomas Marlay, Matthieu Menielle | 2024-12-03 |
| 12152552 | Front frame and deflection grid of a thrust reverser of an aircraft nacelle | Xavier Cazuc, Vincent Peyron, Sébastien Laurent Marie Pascal | 2024-11-26 |
| 12116954 | Fastening of an exhaust cone in a turbomachine nozzle | Vincent Devanlay, Fabien Bravin, Boualem Merabet | 2024-10-15 |
| 12049853 | Thrust reverser for an aircraft bypass turbojet engine nacelle | Xavier Cazuc, Vincent Peyron, Sébastien Laurent Marie Pascal | 2024-07-30 |
| 12044168 | Air inlet of a turbomachine nacelle including a circulation conduit of a hot air flow between a movable upstream part and a fixed downstream part | Hazem Kioua, Pierre Caruel, Charles-Antoine Lampaert | 2024-07-23 |
| 12037941 | Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing method | Damien Lemoine, Charles-Antoine Lampaert, Hazem Kioua | 2024-07-16 |
| 12037940 | Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing method | Hazem Kioua, Emmanuel Lesteven | 2024-07-16 |
| 12000300 | Exhaust cone for a turbomachine | Vincent Devanlay, Marine Ollivier, Guillaume Levieux | 2024-06-04 |
| 11959437 | Fastening of an exhaust cone in a turbomachine nozzle | Vincent Devanlay, Fabien Bravin, Thomas Vandellos | 2024-04-16 |
| 11891185 | Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure | Patrick Boileau, Vincent Peyron, Gina Ferrier | 2024-02-06 |