The invention relates to an aircraft flap/slat handle device. The device comprises a handle, a rod part, a force application mechanism and a clamping part, and the clamping part is provided with a plurality of clamping positions corresponding to the rotating angles of the flap and the slat, wherein each clamping position forms a clamping groove, a corresponding protruding lower clamping piece is arranged between every two adjacent clamping grooves, a sliding rail face is formed between the bottoms of the clamping grooves and the tops of the lower clamping pieces, the sliding rail face comprises a first sliding rail face section and a second sliding rail face section, and the slope or curvature of the first sliding rail face section is different from that of the second sliding rail face section. The aircraft flap/slat handle device meets the man-machine power optimization requirement, and misoperation can be effectively avoided.

    本发明涉及飞机襟/缝翼手柄装置,包括:把手、杆部、施力机构、卡档部,所述卡档部具有与襟翼和缝翼旋转角度相对应的多个卡位,其中,每个卡位形成为一个卡槽,相邻两个卡槽之间设置相应的突出的下卡档件,从卡槽的底部到下卡档件的顶部之间形成滑轨面,所述滑轨面包括第一滑轨面部段和第二滑轨面部段,所述第一滑轨面部段具有的斜率或曲率不同于第二滑轨面部段具有的斜率或曲率。本发明的飞机襟/缝翼手柄装置符合人机功率优化要求,可有效地避免误操作。


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    Titel :

    Aircraft flap/slat handle device


    Weitere Titelangaben:

    飞机的襟/缝翼手柄装置


    Beteiligte:
    ZHANG FANG (Autor:in) / XUE YING (Autor:in) / LI JIAN (Autor:in)

    Erscheinungsdatum :

    2020-04-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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