| 摘要 |
The invention is related to a compound helicopter (1) with a fuselage (2) and at least one main rotor (3), said fuselage comprising a lower side (4) and an upper side (5) that is opposed to said lower side, said at least one main rotor being arranged at said upper side (5), wherein at least one propeller (10) is provided and mounted to a fixed wing arrangement (11, 12) that is laterally attached to said fuselage, said fixed wing arrangement comprising at least one upper wing (11) that is arranged at an upper wing root joint area (14) provided at said upper side of said fuselage and at least one lower wing (12) that is arranged at a lower wing root joint area (13) provided at said lower side of said fuselage, said upper and lower wings being at least interconnected at an associated interconnection region (15). |
