发明名称 Turbine shroud, casting core and manufacture method
摘要 A blade outer air seal (BOAS) casting core (200) has first and second end portions (202, 204) and a plurality of legs. Of these legs, first legs (210, 214, 218) each have: a first end (230, 240, 250) joining the first end portion (202); a main body portion; and a second end (230, 242, 252). Second legs (212, 216, 220) each have: a second end (239, 256, 254) joining the second end portion (204); a main body portio; and a first end (236, 246, 248). At least one of the second legs (212, 216, 220) may have its first end (236, 246, 248) joining the core first end portion (202) and a plurality of apertures (272) in the main body portion. Alternatively, at least one of the first legs (210, 214, 218) may have its second end (230, 242, 252) joining the core second end portion (204) and a plurality of apertures (272) in its main body portion.
申请公布号 EP1905958(A2) 申请公布日期 2008.04.02
申请号 EP20070252977 申请日期 2007.07.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 THOLEN, SUSAN M.
分类号 B22C9/04;B22C9/10;F01D9/04 主分类号 B22C9/04
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