The invention discloses a four-way parallel throttle lever operating force adjusting mechanism with a linkage locking device, which comprises a locking rod (1), a push rod A (2), a push rod B (3), a push rod C (4), a push rod D (5), a friction locking force adjusting mechanism (6), a support shaft a (7) and a support shaft b (8), and is characterized in that the support shaft b (8) is respectively connected with the locking rod (1), the push rod A (2), the push rod B (3), the push rod C (4), the push rod D (5) and the upper end of the friction locking force adjusting mechanism (6); the lower end of the friction locking force adjusting mechanism (6) is installed on the supporting shaft a (7). The invention has the advantages of small volume, compact structure, no attenuation of basic operating force, easiness in adjusting the operating force, simplicity in repair and maintenance, reduction of maintenance and low maintenance labor cost.

    本发明公开了一种带有联动锁紧装置的四路并联式油门杆操作力调节机构,包括锁紧杆(1)、推杆A(2)、推杆B(3)、推杆C(4)、推杆D(5)、摩擦锁紧调力机构(6)、支撑轴a(7)、支撑轴b(8),其特征在于:支撑轴b(8)上分别连接有锁紧杆(1)、推杆A(2)、推杆B(3)、推杆C(4)、推杆D(5)、摩擦锁紧调力机构(6)上端,摩擦锁紧调力机构(6)下端安装在支撑轴a(7)上。本发明体积小、结构紧凑、基础操作力不会衰减,操作力调节易、维修维护简单,减少维护、维修人工成本低。


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    Title :

    Four-way parallel throttle lever operating force adjusting mechanism with linkage locking device


    Additional title:

    带有联动锁紧装置的四路并联式油门杆操作力调节机构


    Contributors:
    LIU JIAN (author) / ZHANG MINGJUN (author) / CHEN XUANREN (author) / XU KAIJIA (author)

    Publication date :

    2025-02-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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