The invention provides a control method for a rotor mechanism of a coaxial rigid dual-rotor test bed, which comprises total pitch control, pitching control and rolling control, is flexible in control, and can be used on the coaxial rigid dual-rotor test bed to meet the installation of measuring equipment so as to carry out a dynamic test related to a coaxial rigid dual-rotor helicopter; besides, the upper rotor wing system and the lower rotor wing system can be separated and independently changed in pitch.

    本发明提供了一种用于共轴刚性双旋翼试验台的旋翼机构的操纵方法,包括总距操纵、俯仰操纵和滚转操纵,操纵灵活,能够用在共轴刚性双旋翼试验台上满足测量设备的安装以进行共轴刚性双旋翼直升机相关的动力学试验,并且可以实现上、下旋翼系统分开独立变距。


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    Titel :

    Control method for rotor mechanism of coaxial rigid dual-rotor test bed


    Weitere Titelangaben:

    用于共轴刚性双旋翼试验台的旋翼机构的操纵方法


    Beteiligte:
    GAO YADONG (Autor:in) / GAO YAZHOU (Autor:in)

    Erscheinungsdatum :

    2021-12-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



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