Adjustable-length connecting rod for an aircraft turbomachine, connecting rod having a generally elongate shape and having first and second longitudinal opposite ends for attachment to elements to be connected. The first longitudinal end is connected to a first threaded shaft screwed into a first tubular portion of an adjustment sleeve. The second longitudinal end is connected to a second threaded shaft screwed into a second tubular portion of the adjustment sleeve. The connecting rod further includes a housing in which at least a portion of the first shaft is configured to slide.


    Access

    Download


    Export, share and cite



    Title :

    Adjustable-length connecting rod for turbomachine


    Contributors:

    Publication date :

    2020-01-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    ADJUSTABLE-LENGTH CONNECTING ROD FOR TURBOMACHINE

    CLADIERE MATHIEU / VERGEZ STÉPHANE | European Patent Office | 2019

    Free access

    ADJUSTABLE-LENGTH CONNECTING ROD FOR TURBOMACHINE

    CLADIERE MATHIEU / VERGEZ STEPHANE | European Patent Office | 2017

    Free access

    Length-adjustable toe-in connecting rod

    WEI GUOZHEN | European Patent Office | 2020

    Free access

    Flexible connecting piece with adjustable length

    YI DAN / ZHANG XIONGFEI / YANG HAOQIANG et al. | European Patent Office | 2022

    Free access