The invention relates to a sliding device for guiding the movement of a trailing edge flap of an aircraft, which is laid in the longitudinal direction of the fuselage of the aircraft and comprises: aslide rail having a pi-shaped cross-sectional shape and a pulley yoke assembly, the slide rail comprising: an elongated roof panel extending in the longitudinal direction of the slide rail; two side plates spaced apart from each other and extending vertically downward from a bottom surface of the top plate; two bottom plates which extend in the opposite directions from the bottom ends of the two side plates and the top plate in parallel, and the top plate, the corresponding bottom plates and the corresponding side plates form grooves which are opened towards the outer sides of the sliding rails in the transverse direction of the sliding rails; the pulley yoke assembly can move on the sliding rail in the longitudinal direction of the sliding rail and comprises a first roller set and a second roller set which are installed on the sliding rail, rollers in the first roller set can roll in the groove along at least one surface of the groove, and rollers in the second roller set can roll along the two side edges, extending in the longitudinal direction, of the top plate, and rollers of the first roller set and the second roller set are at least partially exposed.

    本发明涉及一种用于引导飞机后缘襟翼运动的滑动装置,其沿飞机机身的纵向铺设并包括:具有π形横截面形状的滑轨和滑轮架组件,滑轨包括:沿滑轨的纵向方向延伸的长条形顶板;彼此间隔开并且从顶板的底面向下垂直延伸的两个侧板;和分别从两个侧板的底端与顶板平行地朝彼此相反的方向延伸的两个底板,顶板分别与对应的底板和侧板形成沿滑轨的横向方向朝滑轨的外侧敞开的沟槽,滑轮架组件能够沿滑轨的纵向方向在其上运动并包括安装在其上的第一滚轮组和第二滚轮组,第一滚轮组中的滚轮能够分别沿沟槽的至少一个表面在沟槽中滚动,第二滚轮组中的滚轮能够分别沿顶板的纵向延伸的两个侧缘滚动,并使得第一滚轮组和第二滚轮组的滚轮至少部分地露出。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Sliding device for guiding movement of trailing edge flap of aircraft


    Weitere Titelangaben:

    一种用于引导飞机后缘襟翼运动的滑动装置


    Beteiligte:
    YUAN JIANFENG (Autor:in) / DONG MENG (Autor:in) / CHEN YAN (Autor:in) / LIU YANG (Autor:in) / LIU SONG (Autor:in) / FAN JINGJIE (Autor:in)

    Erscheinungsdatum :

    2021-01-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft trailing edge flap

    WANG WENHU / LI QIANG / NIE XIN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Embedded trailing edge flap movement mechanism

    WANG ZHIGANG / FU SHUO / ZHU XIAOJUN | Europäisches Patentamt | 2024

    Freier Zugriff

    TRAILING EDGE FLAP ASSEMBLY

    EVERAERT BOB ARMAND HENRI | Europäisches Patentamt | 2023

    Freier Zugriff