The invention relates to the technical field of magnetic suspension rotors, in particular to a performance test platform and system for a magnetic suspension rotor power system. The supporting parts comprise clamping parts, the clamping parts are installed on the supporting parts in a sliding mode, the number of the supporting parts is at least three, and the at least three supporting parts are perpendicularly installed on the installation part respectively; therefore, the technical effect that the actual operation state of the magnetic suspension rotor power system meets the operation requirement of being loaded on the aircraft in the performance test process of the magnetic suspension rotor power system is achieved.
本申请涉及磁悬浮旋翼技术领域,尤其涉及一种磁悬浮旋翼动力系统的性能测试试验平台及系统,包括安装部;支撑部,所述支撑部包括夹持部,所述夹持部可滑动的安装于所述支撑部,所述支撑部为至少三个,至少三个所述支撑部分别垂直的安装于所述安装部,从而达到在磁悬浮旋翼动力系统性能测试过程中使磁悬浮旋翼动力系统的实际运行状态满足装载在飞行器上的运行要求技术效果。
Performance test platform and system for magnetic suspension rotor power system
一种磁悬浮旋翼动力系统的性能测试试验平台及系统
2025-04-04
Patent
Electronic Resource
Chinese
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 |
Performance test system and method for magnetic suspension rotor power system
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