发明名称 Metal Injection Moulding Process for Bimetalllic Applications and Airfoils
摘要 A method of producing an airfoil (12; fig 1) including the steps of providing a first perform (32; fig 2) having a metallic powder of a first alloy, the first preform defining an airfoil body having curved pressure and suction sides (20, 22; fig 1). A tip cap (28; fig 2) is disposed between the pressure and suction sides of the airfoil at a radially outer end of the airfoil body. A partial height squealer tip (30; fig 2) extends radially outwards from the tip cap to provide a second preform (34; fig 2) that is a metallic powder of a second alloy different from the first alloy. The tip cap is formed in the shape of an extension of the squealer tip. The first and second preforms are sintered to consolidate the metal powders. An airfoil according to the method is also disclosed.
申请公布号 GB2448031(A) 申请公布日期 2008.10.01
申请号 GB20080004607 申请日期 2008.03.12
申请人 GENERAL ELECTRIC COMPANY 发明人 STEPHEN JOSEPH FERRIGNO
分类号 B22F5/04;B22F7/06;F01D5/14;F01D5/20;F01D5/28 主分类号 B22F5/04
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