Issued Patents All Time
Showing 1–13 of 13 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 11964779 | Device and method for filling an oil reservoir of an aircraft engine | Mathieu Jean Jacques SANTIN, Clément Dupays | 2024-04-23 |
| 11401836 | Portion of a fluid drainage conduit for a turbomachine | Jeremy Edmond Fert | 2022-08-02 |
| 11143462 | Panel for heat exchange and improved noise reduction for a turbomachine | Sebastien Christophe Chalaud, Lancelot Guillou, Jacky Novi Mardjono, Guillaume Mathon-Margueritte, Georges Jean Xavier Riou +1 more | 2021-10-12 |
| 11035294 | Turbomachine with double flow and its lubricant reservoir | Frédéric Paul Eichstadt, Nicolas Maurice Hervé Aussedat | 2021-06-15 |
| 10946317 | Fuel filter having high resistance to icing | Thomas Chauveau, Philippe Vertenoeuil, José Rodrigues | 2021-03-16 |
| 10808628 | Hydromechanical cutoff device with hysteresis for a turbomachine lubrification system | — | 2020-10-20 |
| 10641183 | Butterfly valve for bleeding a compressor for an aircraft turbine engine | Arnaud Bernard Clément Thomas Joudareff, Pierre C. Mouton | 2020-05-05 |
| 10526973 | System for supplying a turbine engine with fluid having a low pressure pumping assembly comprising two pumps in parallel | Philippe Vertenoeuil | 2020-01-07 |
| 10458422 | Turbine engine provided with a lubrication unit | Benoit Jean Henri Gomanne, Michel Gilbert Roland Brault, Thomas Chauveau | 2019-10-29 |
| 10094291 | Gear pump intended, in particular, as a high pressure fuel pump | Philippe Vertenoeuil | 2018-10-09 |
| 10072581 | Gas turbine engine comprising a starter engaged with a low-pressure body | Sebastien Christophe Chalaud, Alain Pierre Garassino | 2018-09-11 |
| 9803556 | Drive gearbox on a turbomachine, consisting of a drive train with gear lines extending into non-parallel planes | Jordane Peltier, Frantz Armange, Lambert Olivier Marie Demoulin, Alain Pierre Garassino, Nuria Llamas Castro +1 more | 2017-10-31 |
| 9347335 | Tank having an inclined partition provided at its ends with through-holes for continuous supply of a supply liquid to a turbine engine | Antoine Laigle, Gilles Le Gouellec | 2016-05-24 |