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某型发动机涡轮前后温度分布的研究
张洪滨1,2, 李光中1,2
1.空军第一研究所!北京;2.100076
摘要:
阐述了在某型涡喷发动机上测量涡轮前、后温度分布的方法,并对测量结果进行了分析,得出"涡轮后温度分布不能代替燃烧室出口(涡轮前)温度分布"的结论。
关键词:  燃烧室  涡轮进口总温  涡轮排气总温  温度分布
DOI:
分类号:V235.1
基金项目:
AN INVESTIGATION OF TEMPERATURE PROFILE BEFORE AND AFTER TURBINE IN A TYPE OF ENGINE
Zhang Hongbin,Li Guangzhong
The First Inst., Air Force, Beijing, 100076
Abstract:
The temperature profile quality at engine combustor exit (before turbine) is aimportant technical index, which concern operational reliability and life of engine’s thermalcomponent, thus measuring temperature profile at the combustor exit (before turbine) in a engine isvery important. The method of measuring temperature profile before and after turbine in a typeturbojet is presented and the measured results is analysed. It can be concluded that the aftertemperature profile turbine differs from the one before turbine.
Key words:  Combustion chamber  Turbine inlet total temperature  Turbine discharge total temperature  Temperature distribution