A short-distance take-off and landing aircraft is divided into an A type and a B type A type, a hydraulic lifting main body is arranged in a nose landing gear, and a fuselage is converted by 0-40 degrees to realize short-distance take-off and landing of the aircraft. A brake wheel for paying off and a hook are arranged at the tail of an aircraft B, and a hook A is arranged in front of an aircraft front wheel. According to the scheme B, various aircrafts can take off and land on highways, open fields, large and medium ships and airports in a short distance. The development of the method in the theoretical and technical field and the specific implementation scheme specification are comprehensively discussed.

    短距起降飞机分A.B型A在前起落架中设液压升降主体,机身0‑40度转换,实现飞机短距起降。B飞机机尾设制动轮放线与挂钩,机前轮前设挂钩A、B方案可使各型飞机在高速路、空旷地、大中航船、机场短距起降本发明在理论与技术领域的发展,具体实施方案说明书有全面论述。


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    Title :

    Short-distance take-off and landing aircraft


    Additional title:

    短距起降飞机


    Publication date :

    2024-09-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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