旋翼刹车综合试验台惯量设计技术  

Inertia Design Technology of Rotor Brake Integrated Test Bench

作　　者：王靖[1] Wang Jing(Aircraft Strength Research Institute of China,Xi′an 710065,Shaanxi,China)

机构地区：[1]中国飞机强度研究所,陕西西安710065

出　　处：《工程与试验》2022年第1期57-58,共2页Engineering and Test

摘　　要：旋翼刹车综合试验台主要针对直升机旋翼刹车装置以及超轻型飞机、无人机机轮刹车装置两种试验产品。试验台在设计中,应充分考虑不同类型试验产品的试验条件,特别是在机械惯量与电惯量相结合时,机械惯量及电模拟惯量的配置设计应能覆盖试验台技术要求中的试验包络曲线,故在此提出惯量设计技术。The rotor brake integrated test bench is mainly used for the performance test of the helicopter rotor brake device,and the ultralight aircraft and UAV wheel brake device.In the design of the test bench,the test conditions of different types of test products should be fully considered,especially when the mechanical inertia and electrical inertia are combined,the configuration design of mechanical inertia and electrical simulation inertia should cover the test envelope curve in the technical requirements of the test bench.Therefore,the inertia design technology is proposed here.

关 键 词：机械惯量 电模拟惯量 惯量设计技术 

分 类 号：V216.8[航空宇航科学与技术—航空宇航推进理论与工程]