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Probe design for measuring total temperature of combustor outlet based on water cooling 被引量:1

Probe design for measuring total temperature of combustor outlet based on water cooling
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摘要 To obtain the outlet temperature of combustor,a kind of high-temperature and water cooling thermocouple was designed.The main factors affecting the results of thermocouple measurement were analyzed after numerical simulation.Results showed that the high-temperature water cooling thermocouple can achieve high temperature measurement under the condition of 2 400 K.With the increase of the distance between the water cooling structure and the stagnation cover,the temperature measurement result was more accurate,and the increase in the area ratio of the inlet and outlet of the stagnation cover within a reasonable range can make the measurement results more accurate.The surface emissivity of the measuring point had a great influence on the radiation error.The pressure and flow rate of cooling water can be effectively reduced after adding zirconia coating onto the surface of the rake body. To obtain the outlet temperature of combustor,a kind of high-temperature and water cooling thermocouple was designed.The main factors affecting the results of thermocouple measurement were analyzed after numerical simulation.Results showed that the high-temperature water cooling thermocouple can achieve high temperature measurement under the condition of 2 400 K.With the increase of the distance between the water cooling structure and the stagnation cover,the temperature measurement result was more accurate,and the increase in the area ratio of the inlet and outlet of the stagnation cover within a reasonable range can make the measurement results more accurate.The surface emissivity of the measuring point had a great influence on the radiation error.The pressure and flow rate of cooling water can be effectively reduced after adding zirconia coating onto the surface of the rake body.
作者 ZHAO Kai LI Feng LU Fuguo ZHOU Tao YANG Hongyu ZHAO Kai;LI Feng;L Fuguo;ZHOU Tao;YANG Hongyu(School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautic;School of Aviation Operations and Services,Aviation University of Air Forc)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2018年第9期2084-2092,共9页 Journal of Aerospace Power
基金 National Natural Science Foundation(9174110013) Aviation Power Fund(614B090310)
关键词 PROBE total temperature combustion chamber water cooling THERMOCOUPLE probe total temperature combustion chamber water cooling thermocouple
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