发明名称 GAS TURBINE PARTS USING POROUS METAL, AND ITS MANUFACTURING METHOD
摘要 PROBLEM TO BE SOLVED: To manufacture gas turbine parts (a panel having an insertion hole, for example) only by simple casting and fabrication. SOLUTION: In this lotus root-shaped porous metal manufacturing method, an advancing direction of a solid-liquid interface at solidifying as a determination factor of a growing direction of a pore is controlled to be slant, whereby the panel having the insertion hole can be manufactured only by the simple casting and the fabrication. At this time, by controlling an atmospheric gas pressure and a solidifying speed, a pore diameter and a porosity are controlled, thereby realizing predetermined cooling property and heat insulating property. COPYRIGHT: (C)2004,JPO&NCIPI
申请公布号 JP2004257335(A) 申请公布日期 2004.09.16
申请号 JP20030050448 申请日期 2003.02.27
申请人 KAWASAKI HEAVY IND LTD;NAKAJIMA HIDEO 发明人 SUNANO KOZO;MIZUTA AKIYOSHI;MATSUZAKI YUJI;KIMURA HIDEO;NAKAJIMA HIDEO
分类号 F01D25/00;B22D25/00;B22D25/02;B22D27/04;B22D27/13;B22D27/20;B23P15/00;C22C1/08;F01D5/18;F01D25/24;F02C7/00;(IPC1-7):F02C7/00 主分类号 F01D25/00
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