The invention specifically discloses a simple sleeve strut type undercarriage. The simple sleeve strut type undercarriage comprises a shock absorber and a retractable system, wherein the shock absorber comprises a shock absorber outer cylinder, a shock absorber inner cylinder, a torque arm and an airplane wheel; the folding and unfolding system comprises a folding and unfolding actuating cylinder, a walking beam, a trunnion connecting rod, a reaction connecting rod, a side supporting rod and a resistance rod; and wherein the upper end of the shock absorber outer cylinder is hinged to one end of the retractable actuating cylinder, one end of the walking beam, one end of the reaction connecting rod and one end of the resistance rod through the upper end of the trunnion connecting rod, and the lower end of the shock absorber outer cylinder is hinged to the lower end of the side supporting rod; one end of the shock absorber inner cylinder is slidably connected in the shock absorber outer cylinder, the other end of the shock absorber inner cylinder is fixedly installed at the upper end of an airplane wheel, and the shock absorber inner cylinder and the shock absorber outer cylinder are hinged through a torsion arm. According to the invention, folding and unfolding functions of the undercarriage can be realized, wherein the folding and unfolding functions of the undercarriage can be achieved by folding and unfolding the actuating cylinder, the lower locking mechanism, the upper locking mechanism, the side supporting rod and other mechanisms.

    本发明具体揭示了一种简易型套筒支柱式起落架,包括:减震器、收放系统;减震器包括减震器外筒、减震器内筒、扭力臂和机轮;收放系统包括收放作动筒、游动梁、耳轴连杆、反作用连杆、侧撑杆、阻力杆;其中,所述减震器外筒上端通过耳轴连杆上端分别与收放作动筒一端、游动梁一端、反作用连杆一端以及阻力杆一端铰接连接,所述减震器外筒下端与侧撑杆的下端铰接连接;所述减震器内筒一端在减震器外筒内部滑动连接,所述减震器内筒另一端固定安装在机轮上端,所述减震器内筒、减震器外筒之间通过扭力臂铰接。可实现起落架的收放功能。通过收放作动筒、下锁机构、上锁机构、侧撑杆等机构可实现起落架合起和展开功能。


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    Titel :

    Simple sleeve strut type undercarriage


    Weitere Titelangaben:

    一种简易型套筒支柱式起落架


    Beteiligte:
    LI BO (Autor:in) / LEI XINGCHI (Autor:in) / YANG KANG (Autor:in)

    Erscheinungsdatum :

    28.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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