Turbine exhaust temperature is an important thermal parameter in gas turbine power plants and its measured value is affected by sensors state.

燃气轮机电厂实际运行中，涡轮排气温度是一个重要的热参数，其传感器的状态直接影响到排气温度观测值。

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The formation mechanism of bulging and cracking of combustor inner liner and his influence on gas turbine exhaust temperature dispersity was analyzed.

分析了火焰筒鼓包和破裂的形成机制对燃气轮机排气温度分散度的影响，提出了相应措施，以防止因燃烧恶化对热通道部件的伤害。

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The thesis expresses velocity distribution of the exit of the exhaust hood of 300MW turbine effect on temperature difference of the condenser.

介绍了300MW汽轮机组排汽通道出口速度分布对凝汽器传热端差的影响。

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