| 摘要 |
- The invention relates to a helicopter fuselage of the type including a central structure to which are attached a front structure, a rear structure and a landing gear, and which supports a transmission gearbox, a main rotor and at least one engine (50), and of the type in which the central structure includes a framework (16) fitted with cladding elements which define the external shape of the fuselage. - According to the invention, the framework (16) of the central structure has substantially the shape of a regular hexahedron consisting of framework panels (28, 30, 32, 34, 36, 38) assembled together. - The invention finds an application especially in producing light helicopters. <IMAGE> |
