首页> 外国专利> METHOD FOR MANUFACTURING COMBUSTOR CONSTITUENT MEMBER, COMBUSTOR CONSTITUENT MEMBER, GAS TURBINE COMBUSTOR, AND GAS TURBINE

METHOD FOR MANUFACTURING COMBUSTOR CONSTITUENT MEMBER, COMBUSTOR CONSTITUENT MEMBER, GAS TURBINE COMBUSTOR, AND GAS TURBINE

机译:制造燃烧室成分,燃烧室成分,燃气轮机燃烧室和燃气轮机的方法

摘要

A method for manufacturing a combustor constituent member has: a step of obtaining a sheet joining body (4) in such a way that a first sheet member (4a) formed of a heat-resistant alloy and a second sheet member (4b) formed of a heat-resistant alloy and having a plurality of fins (5) on the surface are braze-joined by interposing a brazing filler metal including a melting point lowering element so that the fins (5) face the first sheet member (4a); a press forming step for obtaining the combustor constituent member having a desired shape by press-forming the sheet joining body (4); a step of identifying a deformed portion where a deformation occurring, depending on the shape of the combustor constituent member, during the press forming step exceeds a predetermined value; a step of locally heating the portion of the sheet joining body (4) corresponding to the identified deformed portion; and a step of performing cold press forming of the sheet joining body (4) while maintaining the temperature of the heated corresponding portion at a desired temperature.
机译:制造燃烧器构成部件的方法包括:以使得由耐热合金形成的第一片状部件(4a)和由耐热合金形成的第二片状部件(4b)的方式获得片状接合体(4)的步骤。通过插入包括熔点降低元素的钎焊金属使这些翅片(5)面对第一片状构件(4a),从而将表面上具有多个翅片(5)的耐热合金钎焊连接。压制成形步骤,用于通过对片材接合体(4)进行压制成型而获得具有期望形状的燃烧器构成部件。识别变形部的步骤,在该变形部中,在冲压成形步骤中根据燃烧器构成部件的形状而发生的变形超过预定值。局部加热片材接合体(4)的对应于识别出的变形部分的部分的步骤;进行片材接合体(4)的冷压成形,并且将被加热的对应部位的温度维持在期望的温度的工序。

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