The invention provides an aircraft vertical recovery landing device. The device comprises a body, supporting legs, a buffer, a first end frame, a second end frame and reinforcing beams; the supportinglegs comprise the first supporting leg and the second supporting leg; the first end frame and the second end frame are respectively arranged on the body; the buffer is arranged on the first supporting leg; one end of the first supporting leg is movably connected with one end of the second supporting leg; and the other end of the first supporting leg and the other end of the second supporting legare movably connected to the first end frame and the second end frame respectively; the reinforcing beams are arranged in the first end frame and the second end frame and transmit concentrated force loads; and the second supporting leg is of a truss structure. The vertical recovery landing device is of a modular assembly structure, so that the vertical recovery landing device is convenient to disassemble and assemble and low in cost.

    本公开提供了一种飞行器垂直回收着陆装置,包括:本体、支腿、缓冲器、第一端框、第二端框和加强梁,支腿包括第一支腿和第二支腿;第一端框和第二端框分别设置在本体上;缓冲器设置在第一支腿上;第一支腿与第二支腿的一端活动连接,第一支腿与第二支腿的另一端分别活动连接于第一端框和第二端框上;第一端框和第二端框内设置加强梁,加强梁传递集中力载荷;以及第二支腿为桁架结构。本公开垂直回收着陆装置模块化装配结构,拆装方便,成本低。


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    Titel :

    Aircraft vertical recovery landing device


    Weitere Titelangaben:

    飞行器垂直回收着陆装置


    Erscheinungsdatum :

    2020-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16F SPRINGS , Federn