摘要
防止共振和自激振动是转子动力学设计的基本要求，一般通过理论计算与实物试验相结合来解决，因此氢涡轮泵试验是氢涡轮泵研制工作的重要环节。振动特性是氢涡轮泵的重要参数，通过分析正常的和有故障的氢涡轮泵的试验数据，可以确定振动特性参数和发现可能存在的隐患，以便及早提出修改设计措施，保证研制工作的顺利进行。
Prevention from resonant vibration and selfexcited vibration is elemental requirement of rotordynamic design.It is solved by ways of theoretical calc ulation and full scale test,so LH_2turbopump test is an important part of developmental program.Vibration characteristic is one of important parameters of LH_2turbopump.The vibration characteristic parameter is determined by vibration data analysis of normal and failure LH_2turbopump tests,and also design defect is found,so that design can be modified as early as possible,and developmental program proceeds well.
出处
《导弹与航天运载技术》
1995年第5期40-46,共7页
Missiles and Space Vehicles
关键词
液氢泵
转子
故障分析
氢涡轮泵
Liquid hydrogen pump:Dynamics
Rotor
Failure analysis.
