发明名称 Turbine blade with film cooling hole diffusers and method of its manufacture
摘要 <p>An article is disclosed that includes a substrate (50) having a first surface (52) and a second surface (54) and a coating (58) disposed on the second surface (54). In addition, the article includes an angled trench (12) at least partially defined in the coating (58). The angled trench (12) may include a bottom surface (66), a first sidewall (68) and a second sidewall (70) disposed downstream of the first sidewall (68). The first and second sidewalls (68, 70) may extend from the bottom surface (66) at an angle (72, 74) of less than about 60 degrees. Moreover, the article may include a plurality of holes (14) defmed between the first surface (52) and the bottom surface (66). </p>
申请公布号 EP2559855(A3) 申请公布日期 2014.08.27
申请号 EP20120171837 申请日期 2012.06.13
申请人 GENERAL ELECTRIC COMPANY 发明人 LACY, BENJAMIN PAUL
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
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