| 摘要 |
The surface (10) has a hollow and elongated molded structure (11) extending from a connecting section (11') for fixing a structure of a body of aircraft (1) towards a free section (11''), where the structure is formed from composite materials. An openwork support unit is arranged in a reception section distinct from the connecting section. An interchangeable fixing plate (12) is fixed reversibly to the support unit. The fixing plate includes a positioning equipment (20) e.g. global positioning system antenna, for positioning the aircraft. |
