A hydraulic actuator is adapted to drive a spoiler of a wing having a flap. When the hydraulic actuator drives the spoiler in an overlapping region where a driving range of the flap and a driving range of the spoiler overlap, an output suppressing structure suppress a drive output of the hydraulic actuator in the overlapping region to be less than that in a non-overlapping region other than the overlapping region.


    Access

    Download


    Export, share and cite



    Title :

    HYDRAULIC ACTUATOR


    Contributors:
    ITO KOJI (author)

    Publication date :

    2016-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



    Hydraulic actuator

    MA SHAOMING / YUAN ZHAO / YANG ZHIJIE et al. | European Patent Office | 2021

    Free access

    Hydraulic actuator

    MARGER THIBAUT / POULY FRANÇOIS / LABASCOULE JEAN-CHRISTOPHE | European Patent Office | 2020

    Free access

    HYDRAULIC ACTUATOR

    PARK SANG JOON / KIM KIL YEONG / JOO CHOON SHIK et al. | European Patent Office | 2019

    Free access

    HYDRAULIC ACTUATOR

    NIINIKANGAS SAKU / SUNDSTEN MAGNUS | European Patent Office | 2016

    Free access

    HYDRAULIC ACTUATOR

    FOSTER JOHN GERARD | European Patent Office | 2015

    Free access