With the increase of the turbine inlet temperature of high performance aero-engine day by day, the turbine coating blade coating technology has been widely used.
随着高性能航空发动机涡轮进口温度日益提高，涂层技术在涡轮叶片上得以广泛应用。
This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.
本文研究利用不同飞行状态下测量的发动机变量估计涡轮进口温度和压气机出口压力。
The performance of a gas turbine is related to environmental temperatures and its output decreases with the increase of gas inlet temperature, which can be solved by cooling the inlet gas.
燃气轮机的性能与环境温度有关，其出力随燃气进气温度升高而降低的问题可通过冷却燃气进气来解决。
This paper calculates the temperature of inlet air, and analyzes precedence of gas turbine inlet air-cooling by water spray evaporative cooling in Xinjiang area.
对进气空气的温度进行分析计算，并通过计算的结果分析在我国新疆地区燃气轮机采用喷雾蒸发冷却方式冷却进气空气的优越性。
With the elevation of inlet working temperature of gas turbine engine, thermal barrier coatings (TBCs)are receiving a great deal of attention.
前言：随着燃气涡轮发动机进口工作温度的提高，热障涂层技术受到了广泛的关注。
Several calculating methods for determining the air-flow rate, the exhaust temperature, the compressor outlet pressure and the turbine inlet pressure are compared.
对四冲程柴油机增压系统的空气流量，排气温度、压气机出口压力和涡轮进口压力的若干种计算方法进行了分析。
The performance of gas turbine has relation with the environmental temperature and its output is reduced with increase of gas inlet temperature, which can be solved by means of cooling the inlet gas.
燃气轮机的性能与环境温度有关，其出力随燃气进气温度升高而降低的问题可通过冷却燃气进气来解决。
The performance of gas turbine has relation with the environmental temperature, and its output is reduced with increase of gas inlet temperature.
燃气轮机的性能与环境温度有关，其出力随空气进气温度升高而降低，燃气轮机的进气冷却是增加其出力的最有效的方法。
The performance of gas turbine has relation with the environmental temperature, and its output is reduced with increase of gas inlet temperature.
燃气轮机的性能与环境温度有关，其出力随空气进气温度升高而降低，燃气轮机的进气冷却是增加其出力的最有效的方法。
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