航空发动机吸雹试验用多颗同步抛射装置设计
DOI:
CSTR:
作者:
作者单位:

中国飞行试验研究院发动机所 西安 710089

作者简介:

通讯作者:

中图分类号:

V263.3;TN06

基金项目:


Design of multiple synchronous ejection equipment for aero-engine hail absorption test
Author:
Affiliation:

Engine Institute, Chinese Flight Test Establishment, Xi′an 710089, China

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    为满足航空发动机吸雹试验的适航审定需求,针对国内多颗同步抛雹装置研究缺乏的现状,设计了单气室多炮管抛雹装置。通过仿真分析装置结构参数对冰雹抛射过程的影响,并开展试验验证。结果表明:装置实现了多颗冰雹同步抛射,速度误差≤±1.5%,位置散布≤±5 mm,同步时间≤35 ms,各项指标均满足CCAR33.78等适航条款要求,且性能稳定、重复性好。该研究为航空发动机吸雹试验提供了关键装备支撑,验证了单气室多炮管设计在同步性与精准度控制上的有效性。

    Abstract:

    To meet the airworthiness certification requirements for hail ingestion tests of aircraft engines and address the scarcity of research on multi-hail simultaneous ejection devices in China, a single-chamber multi-barrel hail ejection device was designed. The influence of the device′s structural parameters on the hail ejection process was analyzed through simulation, and experimental verification was carried out. The results show that the device enables simultaneous ejection of multiple hailstones with a speed error ≤±1.5%, position dispersion ≤±5 mm, and synchronization time ≤35 ms, all of which comply with airworthiness regulations such as CCAR33.78, and the device also features stable performance and good repeatability. This study provides key equipment support for aircraft engine hail ingestion tests and validates the effectiveness of the single-chamber multi-barrel design in ensuring synchronization and accuracy control.

    参考文献
    相似文献
    引证文献
引用本文

许思琦,薛文鹏,金利强.航空发动机吸雹试验用多颗同步抛射装置设计[J].电子测量技术,2025,48(24):27-33

复制
分享
相关视频

文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2026-02-04
  • 出版日期:
文章二维码

重要通知公告

①《电子测量技术》期刊收款账户变更公告
×
《电子测量技术》
关于防范虚假编辑部邮件的郑重公告