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镍铬-镍硅热电偶特性分析与应用研究
引用本文:李建军.镍铬-镍硅热电偶特性分析与应用研究[J].火箭推进,2010,36(5):63-66.
作者姓名:李建军
作者单位:西安航天动力试验技术研究所,陕西西安,710100
摘    要:以镍铬-镍硅热电偶在火箭发动机试验中的应用为研究对象。对其特性和影响测量的主要因素进行了论述。对镍铬-镍硅热电偶在使用中的劣化问题进行了研究和探讨,结果表明重复使用后的镍铬-镍硅热电偶的劣化是不可避免的,其劣化程度随封装形式、使用温度、直径及使用时间的不同而异,并根据多次试验数据的积累,总结出了相应的处理方法。

关 键 词:火箭发动机试验  镍铬-镍硅  k状态  择优氧化  劣化

Application and characteristic analysis of nickel-chromium and nickel-silicon thermocouple
LI Jian-jun.Application and characteristic analysis of nickel-chromium and nickel-silicon thermocouple[J].Journal of Rocket Propulsion,2010,36(5):63-66.
Authors:LI Jian-jun
Institution:LI Jian-jun (Xi'an Aerospace Propulsion Test Technique Institute, Xi'an 710100, China)
Abstract:Taking the application of nickel-chromium and nickel-silicon thermocouple in the rocket engine test as a research object, its characteristic and the main factors of affecting measurement are elaborated, and the degradation existing in the application of the nickel-chromium and nickel-silicon thermocouple is analyzed and discussed. The result shows that the degradation of the nickel-chromium and nickel-silicon thermocouple is unavoidable, and the degradation can be different with its packaging, temperature, diameter and working duration. The K state and preferred oxidation of nickel-chromium and nickel-silicon thermocouple, as well as its effects on measurement are described in this paper. The method of thermocouple treatment is concluded according to the data obtained in the past tests.
Keywords:rocket engine test  nickel-chromium and nickel-silicon  K state  preferred oxidation  degradation
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