The invention belongs to the field of loads, and discloses an aircraft load release device. The device comprises a cylinder body, a piston rod and a sliding rod, wherein the right end of the cylinderbody is provided with a cylinder groove, the left end of the piston rod is inserted into the cylinder groove, a sliding hole is formed in the right end of the piston rod, and the sliding rod is inserted into the sliding hole leftwards; a limiting hole is formed in the left end of the piston rod, and an elastic limiting device is arranged on the inner wall of the right end of the cylinder groove and matched with the limiting hole; a first buffer device is arranged on the right end face of the cylinder body, a step is arranged at the right end of the piston rod, a second buffer device is arranged on the left end face of the step of the piston rod, and the first buffer device is matched with the second buffer device. By arranging three-stage load release, the release speed is increased, repeated use is facilitated through the limiting hole and the limiting block, and the stability of the limiting block is improved through the sliding block and the sliding groove.

    本发明属于载荷领域,公开了一种飞行器载荷释放装置,包括缸体、活塞杆和滑杆,缸体右端设有缸槽,活塞杆左端插设在缸槽内,活塞杆右端设有滑孔,滑杆左插设在滑孔内;活塞杆左端设有限位孔,缸槽右端的内壁上设有弹性限位装置,弹性限位装置与限位孔配合;缸体右端的端面上设有第一缓冲装置,活塞杆右端设有台阶,活塞杆的台阶左端面上设有第二缓冲装置,第一缓冲装置与第二缓冲装置的位置匹配。本发明通过设有三级载荷释放,从提高释放速度,通过限位孔和限位块便于进行重复使用,通过滑块与滑槽提高限位块的稳定性。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft load release device


    Weitere Titelangaben:

    一种飞行器载荷释放装置


    Beteiligte:
    ZHANG XIAOQIN (Autor:in) / JI YAOHUA (Autor:in) / REN XIANGJUN (Autor:in)

    Erscheinungsdatum :

    2020-10-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft load release mechanism

    ZHANG ZE / LIN FAPENG / SUO GUILAN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft load release window obtaining method

    WANG HUI / WANG BEI'ER / YANG HAORUI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft wing load alleviation device and aircraft wing load alleviation method

    HIRABAYASHI DAISUKE / AKIBA KOUSABUROU | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT WING LOAD ALLEVIATION DEVICE AND AIRCRAFT WING LOAD ALLEVIATION METHOD

    HIRABAYASHI DAISUKE / AKIBA KOUSABUROU | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT WING LOAD REDUCTION DEVICE AND AIRCRAFT WING LOAD REDUCTION METHOD

    HIRABAYASHI DAISUKE / AKIBA KOSABURO | Europäisches Patentamt | 2019

    Freier Zugriff