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  • a new servo mechanism named eccentuator

    Paper number

    IAC-13,C2,P,1.p1,x17363

    Author

    Mrs. Zhou Bei, China Academy of Launch Vehicle Technology, China

    Coauthor

    Mr. Lou Yizhi, China

    Coauthor

    Mr. Shi Rui, China

    Coauthor

    Mr. Zhong Jiehua, China

    Year

    2013

    Abstract
    Aiming at the problems that the torque is large and the installation is narrow and long,the paper puts forward a new light-gauge mechanism named eccentuator .Eccentuator dosen't drive the rudder axle like the traditional servo mechanism,but drives the control surface directly.Prototype model is designed,which passed the preliminary test.The results indicate that the design is reasonable.
    Abstract document

    IAC-13,C2,P,1.p1,x17363.brief.pdf

    Manuscript document

    IAC-13,C2,P,1.p1,x17363.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.