The invention relates to a short-distance/vertical take-off and landing aircraft adopting a variant undercarriage, and belongs to the technical field of aviation. Wings of the short-distance/vertical take-off and landing aircraft adopting the variant undercarriage are fixed to a fuselage, and power systems are installed on the wings. Ailerons are arranged on the wings; a wheel type nose undercarriage is arranged on the fuselage; tail boom systems for vertical take-off and landing or short-distance take-off and landing of the aircraft are arranged on the wing top surface and the wing bottom surface of the wing respectively; wheel type front and back falling frames are arranged in the tail boom system on the bottom surface of the wing; the tail boom system is in an outward opening and closing posture or an inward closing posture; according to the short-distance/vertical take-off and landing aircraft adopting the variant undercarriage, the attitude mode can be adjusted according to task and environment requirements by adopting the variant undercarriage, and the adaptability to task work in a future complex environment is enhanced.
本发明涉及一种采用变体起落架的短距/垂直起降飞行器,属于航空技术领域。采用变体起落架的短距/垂直起降飞行器的机翼固定在机身上,机翼上安装动力系统;机翼上设置副翼;机身上设有轮式前起落架;所述机翼的翼顶面、翼底面分别设有用于飞行器垂直起降或短距起降的尾撑系统;位于翼底面的尾撑系统内设有轮式前后落架;尾撑系统为向外开合姿态或向内收拢闭合姿态;本发明提供的采用变体起落架的短距/垂直起降飞行器,采用的变体起落架,可根据任务及环境需要调整姿态模式,增强了对未来复杂环境下的任务工作的适应性。
Short-distance/vertical take-off and landing aircraft adopting variant undercarriage
一种采用变体起落架的短距/垂直起降飞行器
2021-08-24
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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