摘要
设计了某型飞机进气道伺服装置测试系统,包括液压源系统、测试台系统和控制系统。通过集成模块化设计、无泄漏切换设计、动态缸的改进设计,测试系统满足了所有测试项目要求,并取得了一定的经济效益。
An aircraft inlet servo device testing system, includes the hydraulic source system, the test bench system and the control system, is designed. Through the integrated modular design, the switch without leakage design, and dynamic cylinder improvement, the test system meets all test project requirements and has achieved certain economic benefits.
出处
《液压与气动》
北大核心
2015年第10期124-127,130,共5页
Chinese Hydraulics & Pneumatics
