Turbine starter is a very important composing part for aero-engine, its work capability directly affects the reliability of aero-engine in start.
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。
In order to validate auxiliary airstart performance of a gas turbine starter designed only for the ground engine, the test of auxiliary airstart was conducted on the flight test rig.
为验证原本只为在地面起动发动机而设计的某型燃气涡轮起动机的空中辅助起动性能，在飞行试验台上，对其进行了空中辅助起动试验。
The development of testing system of a subminiature starter of gas turbine is discussed.
讨论了某型燃起涡轮起动机试车台测试系统的开发；
It is important to understand aerodynamic parameters of design-point of gas turbine in order to improve the power of gas-starter.
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.
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。
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