讨论了某型燃起涡轮起动机试车台测试系统的开发；
The development of testing system of a subminiature starter of gas turbine is discussed.
涡轮起动机是航空发动机的重要组成部分，其工作性能直接影响发动机的起动可靠性。
Turbine starter is a very important composing part for aero-engine, its work capability directly affects the reliability of aero-engine in start.
为了提高燃气涡轮起动机的功率，了解燃气涡轮设计点的气动参数以及内部流场结构。
It is important to understand aerodynamic parameters of design-point of gas turbine in order to improve the power of gas-starter.
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