The invention discloses an undercarriage assembly of an aircraft and a flight vehicle, and relates to the technical field of transportation, the aircraft comprises a flight body, and the undercarriage assembly comprises an undercarriage body and a buffer assembly; the undercarriage body is used for being hinged to a flight body, and the undercarriage body is used for rotating relative to the flight body in the first rotating direction in the landing process; the buffer assembly is provided with a first connecting part and a second connecting part which are oppositely arranged; the first connecting part is connected to the undercarriage body, and the second connecting part is used for connecting a flight body; the buffer assembly is used for generating elastic deformation and/or plastic deformation along with rotation of the undercarriage body so as to prevent the undercarriage body from rotating relative to the flight body in the first rotation direction. The undercarriage assembly of the aircraft can solve the technical problems that an existing undercarriage is complex and heavy in structure, low in energy absorption efficiency, large in occupied space and inconvenient to store and integrate.
本申请公开了一种飞行器的起落架组件及飞行交通工具,涉及交通运输技术领域,飞行器包括飞行本体,起落架组件包括起落架本体和缓冲组件;起落架本体用于铰接在飞行本体上,起落架本体用于在着陆过程中沿第一转动方向相对飞行本体转动;缓冲组件具有相对设置的第一连接部和第二连接部;第一连接部连接于起落架本体上,第二连接部用于连接飞行本体;缓冲组件用于随起落架本体的转动而发生弹性形变和/或塑性形变,以阻止起落架本体沿第一转动方向相对飞行本体转动。该飞行器的起落架组件可解决现有的起落架结构复杂笨重、吸能效率较低,且占用空间较多,不便于进行收纳整合的技术问题。
Undercarriage assembly of aircraft and flight vehicle
飞行器的起落架组件及飞行交通工具
2024-05-24
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
British Library Conference Proceedings | 1997
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