发明名称 IMPROVED OPERATION METHOD OF COOLER FOR GAS TURBINE AND SUPPORT DEVICE
摘要 PURPOSE: A method for cooling a gas turbine and a support device is provided to smoothly and continuously operate the gas turbine and the support device by changing a supply line to prevent an area which does not satisfy the temperature standard of the gas turbine from being expanding. CONSTITUTION: A method for cooling a gas turbine and support device is provided to cool a gas turbine and a support device by including upper and lower cooling devices. The upper and lower cooling devices independently operate in a normal operating state. When the lower cooling device does not satisfy a temperature standard, cold air supplied through the upper cooling device flows into the lower cooling device through a fluid path conversion unit. The fluid path conversion unit is an opening and closing valve. The fluid path conversion unit is an automatic or manual damper device.
申请公布号 KR20130010266(A) 申请公布日期 2013.01.28
申请号 KR20110070947 申请日期 2011.07.18
申请人 HYUNDAI HEAVY INDUSTRIES CO., LTD. 发明人 SONG, YOO SEOK;KIM, JUNG RAE;CHA, HOON
分类号 F02C7/12;F01D25/12;F02C7/18 主分类号 F02C7/12
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