Issued Patents All Time
Showing 1–15 of 15 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 9518467 | Blade with 3D platform comprising an inter-blade bulb | Olivier Kueny, Ludovic Pintat | 2016-12-13 |
| 9022744 | Turbine engine blade | Renaud Gabriel Constant Royan, Renaud Martet | 2015-05-05 |
| 9004865 | Blade with non-axisymmetric platform | Olivier Kueny, Ludovic Pintat | 2015-04-14 |
| 8757968 | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine | Jean Bleuzen, Ludovic Pintat, Pascal Pierre Routier | 2014-06-24 |
| 8734096 | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine | Pierre Hervé Fernand Marche, Renaud Martet, Renaud Gabriel Constant Royan | 2014-05-27 |
| 8734115 | Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbine | Jean Bleuzen, Pierre Hervé Fernand Marche, Renaud Martet | 2014-05-27 |
| 8647066 | Blade with non-axisymmetric platform: recess and boss on the extrados | Olivier Kueny, Ludovic Pintat | 2014-02-11 |
| 8162593 | Inter-turbine casing with cooling circuit, and turbofan comprising it | Philippe Pabion, Sebastien Jean Laurent Prestel, Jean-Luc Soupizon | 2012-04-24 |
| 8162594 | Cooled blade for a turbomachine | Philippe Pabion, Jean-Luc Soupizon | 2012-04-24 |
| 8083476 | Method of designing a multistage turbine for a turbomachine | Olivier Kueny, Eric Schwartz | 2011-12-27 |
| 8011879 | Transition channel between two turbine stages | Philippe Pabion, Eric Schwartz, Jean-Luc Soupizon | 2011-09-06 |
| 7658591 | Cooling layout for a turbine blade, turbine blade included therein, turbine and aircraft engine equipped therewith | Alexandre Dervaux, Damien Redon, Pascal Bertrand Yves Claude Papot | 2010-02-09 |
| 7527470 | Stator turbine vane with improved cooling | Philippe Pabion, Eric Schwartz | 2009-05-05 |
| 7137783 | Cooled gas turbine blades | Philippe Pabion, Jean-Luc Soupizon | 2006-11-21 |
| 7004721 | Annular platform for a nozzle of a low-pressure turbine of a turbomachine | Sebastien Imbourg, Jean-Luc Soupizon, Philippe Pabion | 2006-02-28 |