The invention relates to the technical field of aircraft testing, and discloses a flapping-wing aircraft testing device which comprises a supporting frame and a rotating arm, the upper end of the supporting frame is connected with a rotating shaft through a rotating mechanism, the upper end of the rotating shaft is connected with a rocker arm, and one end of the rotating arm is rotationally connected with the rocker arm. One end of the rotating arm is provided with a limiting mechanism, the angle of the rotating arm is adjusted through the limiting mechanism, the other end of the rotating arm is provided with a fixing frame, the fixing frame is provided with an angle adjusting device used for installing the flapping wing air vehicle, and the angle adjusting device is provided with a sensor. According to the flapping-wing air vehicle testing device, the flight attack angle of the flapping-wing air vehicle can be adjusted, the initial angle between the wings of the flapping-wing air vehicle and the horizontal plane is guaranteed, the flight test of the flapping-wing air vehicle around the shaft can be carried out, and research and development personnel can visually observe the flight condition conveniently.
本发明涉及飞行器测试技术领域,公开了一种扑翼飞行器测试装置,包括支撑架和旋转臂,所述支撑架的上端通过转动机构连接转轴,所述转轴的上端连接有摇臂,所述旋转臂的一端与所述摇臂转动连接,并通过限位机构调整所述旋转臂的角度,所述旋转臂的另一端设有固定架,所述固定架上设有用于安装扑翼飞行器的角度调整装置,其所述角度调整装置上设有传感器。本发明提供的扑翼飞行器测试装置,能调整扑翼飞行器的飞行攻角,保证扑翼飞行器翅翼与水平面之间的初始角度,能进行扑翼飞行器的绕轴扑翼飞行测试,方便研发人员直观观察飞行情况。
Flapping wing air vehicle testing device
一种扑翼飞行器测试装置
2022-12-13
Patent
Electronic Resource
Chinese
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 |
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