以采用强迫起动方式的补燃发动机涡轮泵联试系统为研究对象，建立了系统的动态模型。
The dynamic model is established for a turbo-pump test system of a staged combustion cycle engine which employs forced start.
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。
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.
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.
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.
然后，利用建立的数学模型分析起动电机特性对燃气涡轮轴发动机起动性能的影响。
Then, we can use the model to analyze starter characteristic effect on start performance of turboshaft engine.
针对可重复使用液体火箭发动机起动过程，研究了系统控制输入序列的变化对以涡轮叶片为代表的关键部件累积损伤的影响。
This paper studies the problem of tradeoff optimization between damage of reusable liquid propellant rocket engine's turbine blade and control input sequences during the start-up process.
然后，利用建立的数学模型分析部件材料温升对燃气涡轮轴发动机起动性能的影响。
Then, the model was used to analyze component material warm-up effect on the turboshaft engine starting characteristics.
简单介绍了某燃气涡轮轴发动机起动电机数学模型。
A starter mathematic model on a turboshaft engine is described briefly in the paper.
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.
系统研究了燃气涡轮起动机与加载系统匹配的方法，以及加载系统附加振动信号的识别与分离。
We study the matching method of the starter and loading system, identify and separate additional vibration signal from the loading system.
系统研究了燃气涡轮起动机与加载系统匹配的方法，以及加载系统附加振动信号的识别与分离。
We study the matching method of the starter and loading system, identify and separate additional vibration signal from the loading system.
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