The invention provides an aircraft throttle lever synchronizing device, which comprises a throttle lever head, a first mounting hole, a second mounting hole, a first connecting rod, a second connecting rod and a second connecting rod, wherein the throttle lever head comprises a clamping groove and a first mounting hole; the first mounting hole is formed in the upper part of the clamping groove; the locking device is connected with the clamping groove; the locking device can lock the throttle lever small ball in the clamping groove. The lateral extension rod is arranged in the first mounting hole; wherein a driver can hold the lateral extension rod to synchronously operate the aircraft throttle lever; according to the aircraft throttle lever synchronizing device, all engine throttles are synchronized as much as possible, the state difference, caused by human factors, of all engines is reduced, and the control precision of the throttles in the aerial oil receiving process is improved.

    本申请提供了一种飞机油门杆同步装置,所述同步装置包括:油门杆头,包括卡槽以及设置在所述卡槽上部的第一安装孔;锁紧装置,与所述卡槽连接;其中,所述锁紧装置能够将油门杆小球锁紧在所述卡槽内;侧向延伸杆,设置在所述第一安装孔内;其中,驾驶员能够握住所述侧向延伸杆,进行同步操作飞机油门杆;本申请提供的一种飞机油门杆同步装置,使各发动机油门尽可能同步,减少因人为因素造成的各发动机状态差异,提高了空中受油过程中油门的操纵精度。


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    Titel :

    Aircraft throttle lever synchronizing device


    Weitere Titelangaben:

    一种飞机油门杆同步装置


    Beteiligte:
    WANG JUNDONG (Autor:in) / KONG DELIANG (Autor:in) / LI XINJUN (Autor:in) / WANG QUAN (Autor:in) / WANG MING (Autor:in) / LIU WENPING (Autor:in) / LI JIANXUN (Autor:in) / SHEN YUAN (Autor:in) / ZHAO HANCHAO (Autor:in) / LIU SHUAI (Autor:in)

    Erscheinungsdatum :

    2023-04-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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