基于电容层析成像的航空发动机油气两相流测试设计及研究
CSTR:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:


Design and research of aeroengine oil-gas two-phase flow testing based on electrical capacitance tomography
Author:
Affiliation:

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:

    针对航空发动机润滑系统回油管路内油气两相参数测量难题,研发基于电容层析成像的航空发动机油气两相流测试系统。采用电容层析成像技术实现截面相含率测量,通过整流器实现流型规整,提高测量精度,利用文丘里技术进行总流量测量,最终实现气液两相流量测量。基于现场试验台架搭建油气两相流标定校准装置,对基于电容层析成像的航空发动机油气两相流测试系统进行性能验证,结果表明:6种实验工况下,液相流量最大测量误差为7.26 %FS,气相流量最大测量误差为6.56 %FS。该系统能够有效满足现场测试要求,为航空发动机润滑系统设计优化提供重要技术支撑。

    Abstract:

    To address the challenging measurement of oil-gas two-phase parameters in the return oil pipeline of an aeroengine lubrication system, a testing system for oil-gas two-phase flow of aeroengines based on electrical capacitance tomography has been developed. The cross-sectional phase fraction measurement is achieved using electrical capacitance tomography technology, and the flow pattern is regularized through a rectifier to enhance measurement accuracy, at the same time, the Venturi technology is utilized to achieve total flow measurement, ultimately leading to the measurement of gas-liquid two-phase flow. A calibration device for oil-gas two-phase measurement has been set up based on the field test bench for comparative testing of the measurement system. The results indicate that the maximum measurement error for liquid phase flow rate is 7.26 %FS, and the maximum measurement error for gas phase flow rate is 6.56 %FS under six experimental conditions. The research presented in this paper plays a crucial supporting role in the design of lubrication systems in the aeroengine field.

    参考文献
    相似文献
    引证文献
引用本文

张龙赐, 曹西征, 雷敦财, 龚轩, 何宇.基于电容层析成像的航空发动机油气两相流测试设计及研究[J].计测技术,2026,46(4):138~147:
10.11823/j. issn.1674-5795.2026.04.10.

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: 2026-09-09
  • 出版日期:
文章二维码