The invention belongs to the technical field of propeller aircraft rolling moment calculation, and particularly relates to a propeller aircraft rolling moment characteristic calculation method considering dynamic influence. The influence of an attack angle, a sideslip angle, a speed, engine tension, the number of engines, the size and position of an engine nacelle, the diameter and rotating speed of a propeller, a flap deflection angle and a flap chord length on the rolling moment is fully considered, the influence of propeller slip flow and a propeller disc lateral force on the rolling moment is accurately represented, and a propeller aircraft rolling moment coefficient considering the dynamic influence is obtained. The method is used for calculating the rolling torque of the propeller-driven aircraft and can provide effective support for design, improvement and control of the propeller-driven aircraft.

    本申请属于螺旋桨飞机滚转力矩计算技术领域,具体涉及一种考虑动力影响的螺旋桨飞机滚转力矩特性计算方法,充分考虑迎角、侧滑角、速度、发动机拉力、发动机数量、发动机短舱尺寸与位置、螺旋桨直径与转速、襟翼偏转角、襟翼弦长对滚转力矩的影响,准确表征螺旋桨滑流与桨盘侧向力对滚转力矩的影响,得到考虑动力影响的螺旋桨飞机滚转力矩系数,用以对螺旋桨飞机滚转力矩进行计算,可为螺旋桨飞机的设计、改进及其操控提供有效支撑。


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    Title :

    Propeller aircraft rolling moment characteristic calculation method considering dynamic influence


    Additional title:

    一种考虑动力影响的螺旋桨飞机滚转力矩特性计算方法


    Contributors:

    Publication date :

    2025-05-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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 / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung







    JET AIRCRAFT MANEUVERING CHARACTERISTIC SIMULATION SYSTEM FOR SINGLE PROPELLER AIRCRAFT AND SINGLE PROPELLER AIRCRAFT

    HARA SHUNICHIRO / FUKUROSE TAKESHI / IKEDA KOJI | European Patent Office | 2022

    Free access