| 摘要 |
The rotorcraft (1) has a wing (10) extending from an end (11) carrying a propulsive propeller (21) to another end (12) carrying another propulsive propeller (22). A landing gear (30) and a tail (40) are arranged in the rotorcraft. Two fuselages (51, 52) are secured to the wing between the former propulsive propeller and the latter propulsive propeller so as to present an inter-fuselage space (60) having no propeller between the fuselages. Each fuselage is arranged with an undercarriage (31) of the landing gear. |
