1·Turbopump is an important part in liquid rocket engine.
涡轮泵是液体火箭发动机的重要组成部份。
2·The engine-feed system interface is at the turbopump inlet flanges.
发动机与供应系统的交界是在涡轮泵的进口法兰盘处。
3·The engine-feed system interface is at the turbopump inlet flanges .
发动机与供应系统的交界是在涡轮泵的进口法兰盘处。
4·This has brought a lot of difficulties for the design of the turbopump.
这给涡轮泵的设计带来了很大的困难。
5·The drive for the turbopump units was actuated using hydrogen peroxide.
涡轮泵由过氧化氢分解产生的气体驱动。
6·Rotor dynamic is one of the most complicated problems in development of LOX turbopump of liquid rocket engine.
转子动力学问题是液体火箭发动机研制中最复杂的问题之一。
7·To drive the turbopump unit, gas pressure was derived from a generator that used the main propellant components.
驱动涡轮泵系统的气压来自使用主推进剂的燃气发生器。
8·The problem of the rotor dynamics is one of the most complex problems in research of LOX/LH 2 engine LH 2 turbopump.
转子动力学问题是液体火箭发动机氢涡轮泵研制中最复杂的问题之一。
9·At the end of this paper, some key technologies about oxygen hybrid bearing application in the engine turbopump are proposed.
并针对液氧涡轮泵动静压轴承提出了研究需要解决的关键技术。
10·Comes to the conclusion that the hybrid bearing can be used to the liquid rocket engine turbopump, and then puts forward the key technique to be solved.
得出了液体动静压滑动轴承可用于液体火箭发动机涡轮泵转子支撑的结论，同时提出了待解决的关键技术。