发明名称 INTAKE AIR COOLING SYSTEM
摘要 PROBLEM TO BE SOLVED: To collect drain that cannot be collected in a drain pan of a cooling coil (cooling portion).SOLUTION: An intake air cooling system 100 of a gas turbine 28 includes: an intake air duct 12 introducing intake air taken in from an intake air inlet 22 to a compressor 14; a cooling portion 26 provided in the intake air duct 12, and cooling the intake air by heat exchange with a cooling medium introduced from an outside; a convex stepped portion 13 formed into a convex shape relative to bottom surfaces 12a1 and 12a2 of the intake air duct 12 provided on a wake flow side of the cooling portion 26; and drain hole portions 110 that are formed in the bottom surfaces 12a1 and 12a2 of the intake air duct 12 provided on the wake flow side of the cooling portion 26, and that can discharge drain generated on a surface of the cooling portion 26 and dropping to an outside of the intake air duct 12.
申请公布号 JP2014190252(A) 申请公布日期 2014.10.06
申请号 JP20130066828 申请日期 2013.03.27
申请人 MITSUBISHI HEAVY IND LTD 发明人 FUJII KEITA;TOMITA YASUOKI;ASAKINO JIRO;TAKAMATSU MASARU;NISHIO TADAKUNI;NAGASHIMA TATSUNAO;HOTTA KATSUHIRO;NISHIMURA MASASHI
分类号 F02C7/143;F01D25/32;F02C7/04;F02C7/045 主分类号 F02C7/143
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