The invention relates to an aircraft rotor test device. The aircraft rotor test equipment comprises a test bench, an upper rotor test device and a lower rotor test device, wherein the upper rotor test device and the lower rotor test device are respectively arranged on the test bench; the upper rotor testing device comprises an upper rotor driving part, a first force sensor and a first torque sensor, the upper rotor driving part is used for driving an upper testing rotor to rotate, the first force sensor is used for testing the tensile force borne by the upper testing rotor, and the first torque sensor is used for testing the torque borne by the upper testing rotor during rotation; the lower rotor testing device comprises a lower rotor driving part, a second force sensor and a second torque sensor, the lower rotor driving part is used for driving the lower testing rotor to rotate, the second force sensor is used for testing the tensile force borne by the lower testing rotor, and the second torque sensor is used for testing the torque borne by the lower testing rotor during rotation. According to the scheme provided by the invention, the double rotors which are arranged up and down can be tested at the same time.
本申请涉及一种飞行器旋翼测试设备。该飞行器旋翼测试设备包括:测试台架及分别设于所述测试台架上的上旋翼测试装置和下旋翼测试装置;所述上旋翼测试装置包括上旋翼驱动件、第一力传感器和第一扭矩传感器,所述上旋翼驱动件用于驱动上测试旋翼旋转,所述第一力传感器用于测试上测试旋翼所受的拉力,所述第一扭矩传感器用于测试上测试旋翼旋转时所受的扭矩;所述下旋翼测试装置包括下旋翼驱动件、第二力传感器和第二扭矩传感器,所述下旋翼驱动件用于驱动下测试旋翼旋转,所述第二力传感器用于测试下测试旋翼所受的拉力,所述第二扭矩传感器用于测试下测试旋翼旋转时所受的扭矩。本申请提供的方案,能够同时对上下布置的双旋翼进行测试。
Aircraft rotor test equipment
飞行器旋翼测试设备
2023-07-18
Patent
Elektronische Ressource
Chinesisch
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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