首页> 外文会议>IEEE Aerospace Conference >The engine air-start test of XF-2
【24h】

The engine air-start test of XF-2

机译:XF-2的发动机空气开始试验

获取原文

摘要

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.
机译:发动机空气启动测试程序是作为XF-2,日本下一代支持战斗机的飞行测试之一。该计划的目的是展示飞机能力从飞行中的发动机关闭。 XF-2是单一发动机飞机,这是飞机的主要要求之一。描述了测试的规划和结果。计划重点是安全执行,因为发动机在飞行测试期间关闭。在所有空气启动条件下,测试空气开始成功而不超过标准;点燃的时间,推力恢复的时间和最大的排气温度,并且证实了飞机能够从飞行中的发动机关闭。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号