[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
导弹与制导技术

弹用热流传感器敏感元件的热传导模型研究

  • 赵亮 ,
  • 彭舒钰 ,
  • 侯文 ,
  • 邓勇 ,
  • 王刚
展开
  • 1 中北大学仪器科学与动态测试教育部重点实验室,太原 030051
    2 中国兵器工业第203研究所,西安 710065
    3 驻061 基地军事代表室,贵阳 550000

赵亮(1987-),男,山西长治人,硕士研究生,研究方向:测试计量技术及仪器方面的研究。

收稿日期: 2012-10-18

  网络出版日期: 2025-05-24

Heat Transfer Model of Sensitive Element of Heat Flux Sensor for Missiles

  • ZHAO Liang ,
  • PENG Shuyu ,
  • HOU Wen ,
  • DENG Yong ,
  • WANG Gang
Expand
  • 1 Key Laboratory of Instrumentation Science and Dynamic Measurement (North University of China), Ministry of Education, Taiyuan 030051, China
    2 No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China
    3 Military Representative Office in 061 Base, Guiyang 550000, China

Received date: 2012-10-18

  Online published: 2025-05-24

摘要

为研究导弹燃气发出热流对弹体的影响,采用热流传感器测量其热流的变化。基于热传导原理热流传感器敏感元件——康铜箔上接收热流并形成温度差,利用镍铬-康铜热电偶将温度差转换为输出热流信号。考虑了热传导系数为温度的非线性函数这一特点的基础上,对敏感元件进行导热过程分析,建立了热传导模型,编写热传导程序,得到热流输出信号与被测热流的关系,通过校准试验测得数据进行对比,验证模型的正确性。

本文引用格式

赵亮 , 彭舒钰 , 侯文 , 邓勇 , 王刚 . 弹用热流传感器敏感元件的热传导模型研究[J]. 弹箭与制导学报, 2013 , 33(1) : 25 -27,33 . DOI: 10.15892/j.cnki.djzdxb.2013.01.030

Abstract

In order to study the impact of heat flux on missile body discharging by missile gas, the change of heat flux was measured by heat flux sensor. Using NiCr-Constantan foil thermocouple for temperature difference that formed by receiving the heat flux from sensitive element-Constantan foil based on the theory of heat conduction into heat flux signal. The relationship between heat flux density and output signal of heat flux was worked out with analysis on conduction process and a heat transfer model was daveloped based on nonlinearity of thermal conductivity relative to temperature that had been considered, program of heat transfer was compiled. Through comparing calculated value with measured value, the accuracy of the model was proved.

[an error occurred while processing this directive]

参考文献

[1]
高政民,张克军,董敬文.导弹燃气流瞬态温度测量系统设计[J]. 海军航空工程学院学报, 2007, 22(5): 559 -561.
[2]
陈道龙.热电偶测温的现状和发展趋势[J]. 国外计量, 1976(3): 12 - 17.
[3]
廖亚非,张青文,何容盛.热流计的发展、国际领先技术与改进方向研究[J]. 重庆建筑大学学报, 2005, 27(2): 84 - 87.
[4]
任玲,黄凤良.薄膜热电偶动态特性标定技术研究现状 [J]. 传感器与微系统, 2006, 25(10): 4 - 6.
[5]
张伟,张正平,李海波,等.高超声速飞行器结构热试验技术进展[J]. 强度与环境学报, 2011, 38(1): 1 - 8.
[6]
陶文栓.传热学[M]. 西安: 西北工业大学出版社, 2006.
[7]
Oh SH, Lee SH. Bulk-micromachined circular foil type mi-cro hear-flux sensor[J]. Sensors and Actuators: Physical, 2006,132(2): 581- 586.
[8]
HOWARD F G. Single-thermocouple method for determi-ning heat flux to a thermally thick wall, NASA-TND-4737 R. 1977.
文章导航

/

[an error occurred while processing this directive]