XF-2发动机空气起动试验

J. Miyano
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引用次数: 0

摘要

发动机空气启动测试项目是作为日本下一代支援战斗机XF-2的飞行测试之一进行的。该项目的目的是演示飞机在飞行中发动机关闭后的恢复能力。XF-2是单引擎飞机,这是对飞机的主要要求之一。介绍了试验的计划和结果。测试计划的重点是安全执行,因为在飞行测试期间发动机是关闭的。在所有测试的空气启动条件下,空气启动成功,没有超过标准;点火时间,推力恢复时间和最大排气温度,并证实飞机能够从飞行中发动机关闭中恢复。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The engine air-start test of XF-2
The engine air-start test program was carried out as one of the flight tests for the XF-2, Japanese next generation support fighter. The objective of the program was to demonstrate the aircraft's capability to recover from in-flight engine shutdown. The XF-2 being a single engine aircraft, this is one of major requirements to the aircraft. The planning and results of the tests are described. Tests were planned with emphasis on the safe execution because the engine is shut down during the flight tests. In all air-start conditions tested the air-start succeeded without exceeding the criteria; the time to ignition, the time to thrust recovery and the maximum exhaust gas temperature, and it was confirmed that the aircraft is capable to recover from in-flight engine shutdown.
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