发明名称 Method of cooling a gas turbine blade and apparatus therefor
摘要 Part of high-pressure air is extracted from the vicinity of the final stage of a compressor and is introduced into a water spraying chamber, and water at the normal temperature is injected into the high-pressure air from a nozzle installed in the water spraying chamber, to prepare a cooled coolant. The coolant sometimes contains water drops. The cooled coolant is fed into coolant passageways which are provided inside a moving blade in a manner to extend from the root part to the tip of the moving blade. When the coolant passes through the passageways, the moving blade is cooled by the coolant, and after the cooling, the coolant is emitted into a turbine main gas passageway. In case where the water drops are contained in the coolant, they vaporize during the cooling of the moving blade, to cool the air of the coolant, to suppress the temperature rise of the coolant and to enhance the cooling effect.
申请公布号 US4338780(A) 申请公布日期 1982.07.13
申请号 US19780964632 申请日期 1978.11.29
申请人 HITACHI, LTD. 发明人 SAKAMOTO, TAKESHI;ANZAI, SHUNICHI;KOBAYASHI, NARIYOSHI;OSHIMA, RYOICHIRO
分类号 F01D5/08;F01D5/18;F02C3/30;F02C7/18;(IPC1-7):F02C7/18 主分类号 F01D5/08
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