| Patent application number | Description | Published |
|---|
| 20090255589 | TURBINE ENGINE FOR AIRCRAFT - According to the invention, the internal wall of the air intake ( | 10-15-2009 |
| 20090277181 | AIRCRAFT PROPULSION UNIT THAT COMPRISES AN EXHAUST PIPE WITH A SCALLOPED TRAILING EDGE - A propulsion unit includes at least one exhaust pipe ( | 11-12-2009 |
| 20100000227 | AIR INTAKE FOR AN AIRCRAFT TURBINE ENGINE - According to the invention, the air intake ( | 01-07-2010 |
| 20100038476 | DEVICE THAT MAKES IT POSSIBLE TO IMPROVE THE EFFECTIVENESS OF THE ACOUSTIC TREATMENTS IN A PIPE OF AN AIRCRAFT POWER PLANT - A device for improving the effectiveness of the acoustic treatment(s) in an aircraft propulsion unit that includes a pipe ( | 02-18-2010 |
| 20100089690 | METHOD FOR MAKING AN ACOUSTIC TREATMENT COATING AND COATING THUS OBTAINED - A process for the producing a coating for acoustic treatment relative to a leading edge such as an air intake of an aircraft nacelle, the coating including a reflective layer, an alveolar structure, and an acoustically resistive layer, includes: | 04-15-2010 |
| 20100096213 | COATING FOR ACOUSTIC TREATMENT HAVING A HOT AIR ICING PROCESSING FUNCTION OF FROST TREATMENT WITH HOT AIR - A coating for acoustic treatment relative to an aircraft's surface, in particular a leading edge such as an air intake of an aircraft nacelle, includes an acoustically resistive layer, at least one alveolar structure ( | 04-22-2010 |
| 20100116587 | ACOUSTIC PANEL - The invention relates to a panel for an acoustic treatment at the surface of an aircraft, that comprises from the outside to the inside an acoustically resistive porous layer, at least one cellular structure and a reflective or non-permissive layer, wherein the acoustically resistive porous layer includes, at the outer surface that may contact the aerodynamic flows of a sheet or foil, open areas ( | 05-13-2010 |
| 20100276548 | ACOUSTIC PROCESSING STRUCTURE PARTICULARLY ADAPTED TO THE AIR INLET OF AN AIRCRAFT NACELLE - An acoustic treatment structure related to a leading edge onto which an aerodynamic stream flows, in particular at an air intake of an aircraft nacelle, includes—from the outside to the inside—at least one acoustically resistive substructure ( | 11-04-2010 |
| 20100294882 | AIRCRAFT LEADING EDGE - An aircraft leading edge, such as, for example, an air intake ( | 11-25-2010 |
| 20100301161 | ACOUSTIC COATING FOR AN AIRCRAFT INCORPORATING A FROST TREATMENT SYSTEM BY JOULE EFFECT - The invention relates to acoustic lining for an aircraft, which can cover a leading edge, such as an air inlet in the nacelle of a propulsion unit, said lining comprising: (i) from the inside outwards, a reflective layer ( | 12-02-2010 |
