摘要
液压助力器的稳定性是保证其正常工作的必要条件,直接关系到直升机的飞行安全。本文根据直—9直升机主液压助力器的结构及工作特点,应用自动控制原理及系统稳定判据,对影响助力器稳定性的诸因素进行分析探讨,以指导助力器的使用与维修。
The stability of the hydraulic booster is an essential prerequisite for its normal operation which is associated with the flying safety of the helicopter. In this paper the factors influencing the primary hydraulic booster stability of Z-9 was analysised according to its structure and working characteristics by using automatic control theory and system stability determinant. so that the use and mainlanance of the booster are instructed.
出处
《直升机技术》
2000年第1期32-39,共8页
Helicopter Technique
