The invention relates to the field of aircraft devices, in particular to a tilting composite wing unmanned manned aircraft. Comprising a fuselage, the side streamline of the fuselage is fusiform, and the fuselage comprises an outer cover, a rotating head, a rudder, wings, a first motor, a first lifting arm, a second lifting arm, an undercarriage and a shell. Projections of the front face and the side faces are streamlines, the overall appearance streamlines meet the requirement for low resistance during high-speed flight, the tilting rotors are adopted, the front face projection area of the fuselage is increased while the rotors are increased, the front face projection area is reduced, the endurance is prolonged, energy consumption is reduced, and the use requirements are better met; according to the invention, the rudder is designed into a plurality of small control surfaces, but a driving point is also ensured to be driven by one motor, the maneuverability of the rudder cannot be reduced by the cooperative work of the plurality of control surfaces, and the design of the plurality of control surfaces enables the size of the aircraft to be smaller and the occupied area to be smaller, so that the storage convenience of the aircraft in practical use in the future is facilitated.
本发明涉及飞行器装置领域,具体涉及一种倾转复合翼无人驾驶载人飞行器。包括机身,机身侧面流线为梭形,所述机身包括外盖、旋转头、方向舵、机翼、第一电机、第一升降臂、第二升降臂、起落架、外壳。本发明正面和侧面均投影均为流线,整体外形流线满足高速飞行时低阻力的需要,本发明采用倾转旋翼,这样的设计没有在增加旋翼的同时增加机身的正面投影面积,降低正面投影面积确保了延长续航和降低能耗,更加的符合使用需求,本发明将方向舵设计成了多个小舵面,但是驱动点还是保证了由一台电机驱动,多舵面协同工作可以保证它的机动性不会降低,多舵面设计可以让飞行器的体积变得更小占地更少,有利于飞行器日后在实用中存放的便利性。
Tilting composite wing unmanned manned aircraft
一种倾转复合翼无人驾驶载人飞行器
2025-03-04
Patent
Electronic Resource
Chinese
IPC: | B64U |
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