The flap rudder layout for enhancing the rolling-control capability of a hypersonic aircraft is a layout form applied to a spherical-conical-cylindrical axisymmetric hypersonic aircraft, and the aircraft obtains a control moment through flap rudder deflection so as to control the flight attitude. The flap rudder is designed into a flat plate structure and is mounted at the bottom of the aircraft through a rudder shaft. The designed installation angle of the flap type rudder remarkably improves the rolling-control capacity of the aircraft, and effective distribution of pitching, yawing and rolling control efficiency of the aircraft is achieved.

    一种增强高超声速飞行器滚控能力的襟翼舵布局,是应用在球‑锥‑柱型轴对称高超声速飞行器上的布局形式,飞行器通过襟翼舵偏转获得控制力矩,从而控制飞行姿态。襟翼舵设计为平板构型,通过舵轴安装于飞行器底部。襟翼舵设计安装角显著提升了飞行器的滚转控制能力,且实现了对飞行器俯仰、偏航和滚转控制效率的有效分配。


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    Titel :

    Flap rudder layout for enhancing rolling-control capability of hypersonic aircraft


    Weitere Titelangaben:

    一种增强高超声速飞行器滚控能力的襟翼舵布局


    Beteiligte:
    LIU QIANG (Autor:in) / LIANG JIANJUN (Autor:in) / ZHAO XINQIANG (Autor:in) / SUN YONGFENG (Autor:in) / XIE XUEMING (Autor:in) / CHEN JINGPENG (Autor:in)

    Erscheinungsdatum :

    25.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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 / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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