发明名称 Blade for a turbine engine and method for production of said blade
摘要 The invention relates to a blade for a turbine engine with a base body, made from a titanium alloy, with a first and a second component piece, which are connected in the connection region by means of a bonding process. A groove with a groove wall runs through the connection region, to prevent local concentration of tension, such that the above borders directly on the second component piece and forms therewith a connection angle greater than 70 degrees.
申请公布号 US2005076503(A1) 申请公布日期 2005.04.14
申请号 US20040486607 申请日期 2004.10.08
申请人 PICKERT URSULA;TIEMANN PETER;OLTMANNS IRIS 发明人 PICKERT URSULA;TIEMANN PETER;OLTMANNS IRIS
分类号 B23K20/02;B23P15/04;F01D5/14;F01D5/18;F01D5/28;F02C7/00;(IPC1-7):B63H1/26;F03B3/12 主分类号 B23K20/02
代理机构 代理人
主权项
地址