发明名称 METHOD AND APPARATUS FOR MOLDING
摘要 <P>PROBLEM TO BE SOLVED: To provide a technique for configuring certain components by a spinning molding, such as leading edges of blades or parts around nacelles of airplanes, made of a titanium alloy plate with high yield strength and poor ductibility. <P>SOLUTION: The method for molding a titanium alloy material using a stick-like tool by a spinning molding includes a step of a heat molding that a working point of the material to which the tool works is locally heated by a high-frequency induction heating during a spinning molding. <P>COPYRIGHT: (C)2012,JPO&INPIT
申请公布号 JP2011218427(A) 申请公布日期 2011.11.04
申请号 JP20100092292 申请日期 2010.04.13
申请人 SOCIETY OF JAPANESE AEROSPACE CO INC;JAPAN AIRCRAFT MFG CO LTD 发明人 SUZUKI NOBUYUKI
分类号 B21D22/16;B21D53/92;C22F1/00;C22F1/18 主分类号 B21D22/16
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