Amphibious vertical take-off and landing aircraft structure
The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of rotor wing mechanisms are mounted on the mounting frame; the rotor wing mechanism comprises a rotor wing and a driving motor; and the rotor wings are obliquely mounted on the mounting frame in the advancing direction of the aircraft. The aircraft not only can take off and land on the water surface, but also can take off and land so as to adapt to multi-scene application. In the whole flight process of the aircraft, the multiple rotor mechanisms on the aircraft are always in a running state and are both vertical take-off and landing lift power and cruise flight thrust power, and compared with a traditional aircraft with a lift and thrust layout, the aircraft is simpler and safer to operate and control flight, and t |
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