The invention discloses a pneumatic hole test platform for simulating a full maneuvering state of an aircraft, which relates to the technical field of wind tunnel tests and comprises a base, a roll angle adjusting mechanism, a pitch angle adjusting mechanism, a yaw angle and Z-direction adjusting mechanism, a Y-direction adjusting mechanism and an X-direction adjusting mechanism. The roll angle adjusting mechanism is used for driving the test machine body to rotate around a first axis relative to the roll angle adjusting mechanism so as to adjust the roll angle; the pitch angle adjusting mechanism can drive the test machine body yaw angle and Z-direction adjusting mechanism to rotate up and down around a second axis in a pitching manner; the yaw angle and Z-direction adjusting mechanism can be used for vertically moving the test machine body along the Z direction and rotating along a third axis which is vertically arranged; the Y-direction adjusting mechanism can enable the test machine body to linearly move along the horizontal Y direction; the X-direction adjusting mechanism can drive the test machine body to linearly move along the horizontal X direction; the six-degree-of-freedom maneuvering state simulation of the aircraft can be met, the coupling situation between the degrees of freedom is reduced, and motion control is facilitated.

    本发明公开了一种模拟飞行器全机动状态风动洞试验平台,涉及风洞试验技术领域,包括基座、滚转角调节机构、俯仰角调节机构、偏航角及Z向调节机构、Y向调节机构和X向调节机构;滚转角调节机构用于驱动试验机体相对于滚转角调节机构绕第一轴线旋转以调节滚转角;俯仰角调节机构能够驱动试验机体偏航角及Z向调节机构绕第二轴线上下俯仰转动;偏航角及Z向调节机构能够试验机体沿Z向竖直移动以及沿竖向设置的第三轴线旋转;Y向调节机构能够试验机体沿水平Y向直线移动;X向调节机构能够驱动试验机体沿水平X向直线移动;能够满足飞行器六个自由度的机动状态模拟,且减少自由度之间的耦合情形,便于运动控制。


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    Titel :

    Wind tunnel test platform for simulating full maneuvering state of aircraft


    Weitere Titelangaben:

    一种模拟飞行器全机动状态的风洞试验平台


    Beteiligte:
    ZHANG XIAYANG (Autor:in) / HE YONGTAO (Autor:in) / ZHAO QIJUN (Autor:in) / CHEN XI (Autor:in) / WANG BO (Autor:in) / LI WEI (Autor:in)

    Erscheinungsdatum :

    2024-05-10


    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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