The invention discloses a wind tunnel test platform for helicopter maneuvering flight state simulation, which comprises a connecting part, a lifting mechanism, an advancing and retreating mechanism, a rolling mechanism, a pitching mechanism and a yawing mechanism, and is characterized in that the connecting part is used for connecting a to-be-tested rotor mechanism; the yawing mechanism comprises a front yawing piece and a rear yawing piece, the front yawing piece is in shaft hinge with the rear yawing piece through a first shaft, the rear yawing piece is in shaft hinge with the lifting mechanism or the advancing and retreating mechanism through a second shaft, the second shaft and the first shaft are both parallel to the Z axis, and the front yawing mechanism is connected with the connecting part through a rolling mechanism and/or a pitching mechanism; the front yawing piece is provided with a first power assembly used for enabling the front yawing piece to rotate with the first shaft as the axis, and the rear yawing piece is provided with a second power assembly used for enabling the rear yawing piece to rotate with the second shaft as the axis. Multi-degree-of-freedom motion simulation can be carried out, and when yaw motion simulation is carried out, the technical problems that an existing test platform is poor in continuity and the orientation of a to-be-tested rotor mechanism cannot be changed in real time can be solved.

    本发明公开了一种用于直升机机动飞行状态模拟的风洞试验平台,包括连接部、升降机构、进退机构、滚转机构、俯仰机构及偏航机构,连接部用于连接待试验旋翼机构;偏航机构包括前偏航件和后偏航件,前偏航件通过第一轴与后偏航件轴铰,后偏航件通过第二轴与升降机构或进退机构轴铰,第二轴及第一轴均与Z轴平行,前偏航机构通过滚转机构和/或俯仰机构与连接部连接;前偏航件设有第一动力组件,用于使前偏航件以第一轴为轴转动,后偏航件设有第二动力组件,用于使后偏航件以第二轴为轴转动。其能够进行多自由度的运动模拟,且其在进行偏航运动模拟时,能够解决现有试验平台连贯性较差且无法实时改变待试验旋翼机构朝向的技术问题。


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    Titel :

    Wind tunnel test platform for helicopter maneuvering flight state simulation


    Weitere Titelangaben:

    一种用于直升机机动飞行状态模拟的风洞试验平台


    Beteiligte:
    TANG MIN (Autor:in) / WU JIE (Autor:in) / PENG XIANMIN (Autor:in) / LUO HUAN (Autor:in) / ZHANG GUICHUAN (Autor:in) / WEI YIBO (Autor:in) / SONG XIN (Autor:in) / TANG BO (Autor:in) / DUAN ZHANGCHENG (Autor:in)

    Erscheinungsdatum :

    2023-03-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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



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