The invention discloses an aircraft interior pull rod which comprises a rod body, a left fork-shaped connector and a left locking mechanism, the left fork-shaped connector is arranged at the left end of the rod body and is in threaded connection with the rod body, the left end of the left locking mechanism is in butt joint with the left fork-shaped connector, the right end of the left locking mechanism is in butt joint with the rod body, the length of the pull rod is adjusted by rotating the left fork-shaped connector, and the length of the pull rod is adjusted by rotating the right fork-shaped connector. After adjustment is completed, the left locking mechanism and the rod body are locked and fixed through the left locking mechanism, the rod body, the left fork-shaped connector and the left locking mechanism are arranged so that the pull rod can have the adjusting function, after adjustment is completed, the pull rod is fixed to meet the requirement of the pull rod, the installation convenience of the pull rod is improved, and the tensile capacity and the anti-pressure capacity are improved; the guide plate is arranged on the fixed semi-ring so that the fixed semi-ring can be more easily pressed into the locking gear, the hoop is arranged to prevent transition adjustment of the left fork type connector, the safety of the pull rod is improved, the auxiliary nut is arranged to enable the adjusting rod to be more easily tightened, the installation convenience is improved, and the sealing ring is arranged to prolong the service life of the pull rod.

    本发明公开了一种飞机内饰拉杆,包括杆体、左叉型接头、左锁紧机构,所述左叉型接头设于所述杆体左端和其螺纹连接,所述左锁紧机构左端和所述左叉型接头对接,所述左锁紧机构右端和所述杆体对接,转动所述左叉型接头调节拉杆长度,调节完成后利用所述左锁紧机构将所述左锁紧机构和所述杆体锁止固定,设置杆体、左叉型接头和左锁紧机构使拉杆具有调节功能且调节好之后对拉杆进行固定使拉杆满足,提升了拉杆的安装便利性,且提升了抗拉、抗压能力,在固定半环上设置引导板使固定半环更加容易按入锁紧齿轮上,设置卡箍防止左叉型接头过渡调节,提升了拉杆的安全性,设置辅助螺母使调节杆更加容易拧紧,提升安装便捷性,设置密封圈提升了拉杆的使用寿命。


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    Titel :

    Airplane interior trim pull rod


    Weitere Titelangaben:

    一种飞机内饰拉杆


    Beteiligte:
    MIAO PENG (Autor:in) / WANG LEI (Autor:in) / CHEN ZHE (Autor:in) / WANG HAIXIANG (Autor:in) / YIN YANJIAO (Autor:in)

    Erscheinungsdatum :

    2023-10-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16C SHAFTS , Wellen



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