| 摘要 |
The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material that is adjacent to the first alveolar structure, where the second alveolar structure is flattened against the inside surface of the wall, with the defrosting system and inserted between the second alveolar structure and the wall. The alveolar structures are made of aluminum alloy. An independent claim is also included for an aircraft nacelle. |
