Invention Grant
US07752847B2 Liquid injection in a gas turbine during a cooling down phase 失效
在冷却阶段期间在燃气轮机中进行液体喷射

Liquid injection in a gas turbine during a cooling down phase
Abstract:
The invention relates to a method for cooling a gas turbine comprising a rotor, said method being carried out after the operation of the gas turbine and whereby the rotor is driven at least intermittently during a cooling phase at a reduced nominal speed. To provide a gas turbine with a reduced down time, a liquid is introduced at least intermittently into the air stream upstream of the compressor during the cooling phase.
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