发明名称 Turbine engine component manufacture
摘要 A cooled turbine engine component is made by providing first and second pieces (46,44) respectively having first and second surfaces (64,68). At least one circuit (100) is formed in at least one of the first and second surfaces (68). A first plurality of apertures (114) is provided in the first piece (46) to form inlets to the at least one circuit (100). A second plurality of apertures (140) is provided in the second piece (44) to form outlets to the at least one circuit (100). A combination of the first and second pieces is assembled and integrated.
申请公布号 EP1629938(A3) 申请公布日期 2006.06.14
申请号 EP20050253843 申请日期 2005.06.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HUDSON, ERIC A.;HARDING, BENJAMIN R.
分类号 B23P15/04;F01D5/18 主分类号 B23P15/04
代理机构 代理人
主权项
地址