【摘要】 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。与在地面起动发动机时的参数进行比较,得到了有意义的结论,掌握了其在空中工作时参数的变化规律,为提高该型燃气涡轮起动机空中辅助起动性能提供了依据。更多还原

【Abstract】 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. The change law of the starter engine parameter in the air was obtained by comparison with the parameters of ground starter engine. The foundation was provided for improving the performance of auxiliary airstart of the gas turbine starter.更多还原