Title: Temperature control and performance test of gas turbine
Abstract: A method for gas turbine inlet temperature control is presented, and the effect of this method upon the power output and heat consumption rate of a unit during the performance test is also discussed. The results of the research indicate that the accuracy of temperature control correction parameter will affect gas turbine inlet temperature, and hence affect the basis of gas turbine performance test. A calculation method for gas turbine inlet temperature through shift power balance and energy balance is also presented, providing a reference for combined cycle unit's performance test.
Publication Year: 2006
Publication Date: 2006-01-01
Language: en
Type: article
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