发明名称 IMPINGEMENT COOLING STRUCTURE
摘要 An impingement cooled structure includes a plurality of shroud members disposed in a circumferential direction to constitute a ring-shaped shroud surrounding a hot gas stream, and a shroud cover mounted on radial outside faces of the shroud members to form a cavity therebetween. The shroud cover has a first impingement cooling hole which communicates with the cavity and allows cooling air to be jetted to an inside thereof so as to cool an inner surface of the cavity by impingement. The shroud members each has a hole fin. The hole fin divides the cavity into a plurality of sub-cavities. Further, the hole fin has a second impingement cooling hole which allows the cooling air having flowed through the first impingement cooling hole to be jetted obliquely toward a bottom surface of the sub-cavity adjacent thereto.
申请公布号 CA2644099(A1) 申请公布日期 2007.09.07
申请号 CA20072644099 申请日期 2007.02.26
申请人 IHI CORPORATION;JAPAN AEROSPACE EXPLORATION AGENCY 发明人 OHKITA, YOUJI;FUKUYAMA, YOSHITAKA;YOSHIDA, TOYOAKI;FUJIMOTO, SHU;YAMANE, TAKASHI;MATSUSHITA, MASAHIRO
分类号 F01D25/24;F02C7/18 主分类号 F01D25/24
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