发明名称 Gas turbine bucket with cooled platform leading edge and method of cooling platform leading edge
摘要 In a turbine bucket having an airfoil portion and a root portion with a substantially planar platform at an interface between the airfoil portion and the root portion, a platform cooling arrangement including a cavity extending along the forward portion of the platform, and at least one inlet bore extending from a source of cooling medium to the cavity, and at least one outlet opening for expelling cooling medium from the cavity.
申请公布号 US2007116574(A1) 申请公布日期 2007.05.24
申请号 US20050282704 申请日期 2005.11.21
申请人 GENERAL ELECTRIC COMPANY 发明人 ITZEL GARY M.;WEBBON WAYLON W.
分类号 F01D11/00 主分类号 F01D11/00
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