北京航空航天大学学报 ›› 2009, Vol. 35 ›› Issue (12): 1413-1416.

• 论文 •    下一篇

基于稳态方法的对流换热系数传感器研制

全永凯, 徐国强, 罗 翔, 丁水汀   

  1. 北京航空航天大学 航空发动机气动热力重点实验室, 北京 100191
  • 收稿日期:2008-11-07 出版日期:2009-12-31 发布日期:2010-09-14
  • 作者简介:全永凯(1983-),男,黑龙江哈尔滨人,博士生,quanyongkai@126.com.

Development of kind of heat transfer coefficient sensor based on steady method

Quan Yongkai, Xu Guoqiang, Luo Xiang, Ding Shuiting   

  1. National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
  • Received:2008-11-07 Online:2009-12-31 Published:2010-09-14

摘要: 基于稳态方法研制出一种对流换热系数传感器.在研究中引入一个标定端,并分析其精度,与经典的经验公式进行了对比.通过标定实验验证了此传感器的可行性,得到修正系数值 K ,修正后传感器测量值与标准值的相对误差范围为0.4%~1.7%,不同传感器的K值不同.

Abstract: A kind of heat transfer coefficient sensor based on steady state method was developed. A calibration terminal was pulled. The precision was analyzed and the results were compared with the values calculated from the classics empirical equation. The heat transfer coefficient obtained from the calibration terminal and the empirical equation is in a good agreement. The results shows that the calibration method is reasonable. The feasibility of the sensor is proved by the calibration experiment and the modified coefficient K is obtained. The relative error range is from 0.4% to 1.7% between the measured values and standard values. The values of K of separate sensors are different.

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