液压气动与密封
液壓氣動與密封
액압기동여밀봉
Hydraulics Pneumatics & Seals
2015年
10期
34-36
,共3页
发动机%电磁阀%测试系统%设计
髮動機%電磁閥%測試繫統%設計
발동궤%전자벌%측시계통%설계
aircraft engine%solenoid valve%test-system%design
根据飞机发动机喷口电磁阀的测试需求,设计了电磁阀的测试系统.该系统由液压测控单元,电子测量单元,软件控制单元组成.可以对喷口电磁阀密封性能、溢流性能、工作性能参数测量.试验结果表明:测试系统满足航修厂对喷口电磁阀的测试需求,在应用中取得良好效果.
根據飛機髮動機噴口電磁閥的測試需求,設計瞭電磁閥的測試繫統.該繫統由液壓測控單元,電子測量單元,軟件控製單元組成.可以對噴口電磁閥密封性能、溢流性能、工作性能參數測量.試驗結果錶明:測試繫統滿足航脩廠對噴口電磁閥的測試需求,在應用中取得良好效果.
근거비궤발동궤분구전자벌적측시수구,설계료전자벌적측시계통.해계통유액압측공단원,전자측량단원,연건공제단원조성.가이대분구전자벌밀봉성능、일류성능、공작성능삼수측량.시험결과표명:측시계통만족항수엄대분구전자벌적측시수구,재응용중취득량호효과.
Based on the test requirement of hydraulic solenoid valve of exhaust nozzle exit of a certain aero-engine, the test-system of the hy-draulic solenoid valve is designed. The test-system consists of hydraulic measurement and control unit, a electronic measurement unit and a software control unit. It can be used to perform the performance parameter test of the hydraulic solenoid valve.The test-system is fulfilled the needs of fighter repair factories and worked in good condition.
