发明名称 Cooled component, casting core for manufacturing such a component, as well as method for manufacturing such a component
摘要 A cooled component, such as a turbine blade for gas turbines is provided, having efficient internal cooling, with an interior cooling passageway having a round cross-section. A row of feeding holes for the coolant are arranged spaced from each other in the direction of the longitudinal axis of the cooling passageway and originating from a common coolant channel. Each of the feeding holes intersects the cooling passageway tangentially. The ease of manufacturing the cooling component is improved in that the majority of the feeding holes have a hole diameter that is smaller than half of the hydraulic diameter of the cooling passageway, and selected feeding holes have a hole diameter that is greater than half of the hydraulic diameter of the cooling channel.
申请公布号 US2002051706(A1) 申请公布日期 2002.05.02
申请号 US20010984204 申请日期 2001.10.29
申请人 HAEHNLE HARTMUT;EL-NASHAR IBRAHIM;KELLERER RUDOLF;ARX BEAT VON 发明人 HAEHNLE HARTMUT;EL-NASHAR IBRAHIM;KELLERER RUDOLF;ARX BEAT VON
分类号 B22C9/10;B22C9/24;F01D5/18;(IPC1-7):F01D5/18 主分类号 B22C9/10
代理机构 代理人
主权项
地址