In the research of variant aircraft and small UAV, the actuator is considered to be smaller in size and compacter in structure. In this background, this paper designs a new type of compact smart actuator, the actuator integrates simple hydraulic pump, hydraulic pump plunger adopts two simple structure, Oil flow distribution is realized by suction and discharge of one-way valve. In order to reduce the volume of the actuator, the housing of the hydraulic pump is connected to the actuator housing. The control circuit of the actuator is designed, and the simulation model is built on the AMEsim simulation platform to verify the correctness of the design.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Design of compact smart actuator


    Contributors:
    Mingjun, Zhu (author) / Liqun, Xia (author) / Yixue, Hu (author) / Jingyue, Chen (author) / Xin, Song (author)


    Publication date :

    2017-08-01


    Size :

    355215 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Compact electromechanical actuator

    GIERAS JACEK F / ROZMAN GREGORY I | European Patent Office | 2016

    Free access

    Compact linear hydraulic actuator

    FENNY CARLOS A / ELVING CARL T / CAHOON RODNEY M et al. | European Patent Office | 2019

    Free access

    COMPACT AIRCRAFT ACTUATOR SYSTEM

    ALLEN JASON BRADLEY | European Patent Office | 2023

    Free access

    Compact aircraft actuator system

    ALLEN JASON BRADLEY | European Patent Office | 2024

    Free access

    COMPACT SPRING BRAKE ACTUATOR

    LESKO PIOTR / SZCZUPLAK LUKASZ / SZOZDA ANDRZEJ et al. | European Patent Office | 2016

    Free access