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Damien Prat, Colomiers FR
Damien Prat, Colomiers FR
| Patent application number | Description | Published |
|---|---|---|
| 20080217101 | Method of Reducing Noise Emissions at the Rear of a Turboshaft Engine and Turboshaft Engine thus Improved - The invention relates to a method of reducing noise emissions at the rear of a turboshaft engine and to a turboshaft engine thus improved. According to the invention, the thickness of the rear part ( | 09-11-2008 |
| 20080217476 | AIRCRAFT INCLUDING AN AIR CONDITIONING SYSTEM - According to the invention, means ( | 09-11-2008 |
| 20090000305 | Dual Flow Turbine Engine Equipped with a Precooler - The invention concerns a precooler ( | 01-01-2009 |
| 20090007567 | Dual Flow Turbine Engine Equipped with a Precooler - The invention concerns a precooler ( | 01-08-2009 |
| 20090090095 | AIRCRAFT TURBOFAN ENGINE - According to the invention, there is arranged on the inner fan cowl ( | 04-09-2009 |
| 20090111370 | VENTILATING AIR INTAKE ARRANGEMENT WITH MOBILE CLOSING DEVICE - The invention concerns a ventilating air intake arrangement with mobile sealing device. The arrangement comprises at least one air passage channel ( | 04-30-2009 |
| 20090253361 | VENTILATING AIR INTAKE ARRANGEMENT - The invention concerns an arrangement comprising at least one air passage channel ( | 10-08-2009 |
| 20100087132 | Air Intake Arrangement for a Vehicle, in Particular an Aircraft - The arrangement of the invention includes mobile means for blocking an air passage channel (10) which are controlled by an aerodynamic surface (20) provided in said air passage channel (10) and capable of generating a lift force (P) under the action of the external air flow (F) flowing through said air passage channel (10). | 04-08-2010 |
| 20100107597 | Method for Reducing Sound Output at the Back of a Turbo Engine and Turbo Engine Improved By This Method - The invention relates to a method for reducing the noise missions from the rear of a turbo engine, and a turbo engine improved by said method. According to the invention, the nozzle for the cold flow ( | 05-06-2010 |
| 20100186369 | DUAL FLOW TURBOSHAFT ENGINE AND IMPROVED HOT FLOW NOZZLE - According to the invention, the hot flow nozzle includes a single skin ( | 07-29-2010 |
| 20100242433 | METHOD FOR IMPROVING THE PERFORMANCE OF A BYPASS TURBOJET ENGINE - Method for improving the performance of a bypass turbojet engine. According to the invention, the area of the annular outlet orifice ( | 09-30-2010 |