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.
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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 |
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代理人 |
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主权项 |
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地址 |
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