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It exceeds Si and 1.0mass below 2.0mass

机译:超过Si且低于2.0mass%1.0mass%

摘要

PROBLEM TO BE SOLVED: To provide a fin material for brazing which is superior in strength, thermal conductivity and the corrosion resistance of itself after having been heated for brazing, in diffusion resistance against a brazing filler while being heated for brazing, and in corrugate formability, and to provide a method for stably manufacturing the fin material.;SOLUTION: An aluminum alloy for the fin material for brazing comprises 0.8 mass% to 2.0 mass% Si, more than 1.0 mass% but 3.0 mass% or less Mn, and more than 0.10 mass% but less than 0.7 mass% Fe. The method for manufacturing the fin material comprises: final-intermediate-annealing a sheet with a thickness of 0.1 mm or thinner made from the aluminum alloy so as to give it a crystalline structure in which recrystallized grains having a diameter of 10 mm or larger in a rolling direction occupy 80% or more of the surface area when viewed from the surface; and then cold-rolling it with a sheet-thickness rolling reduction of less than 30%. The fin material is manufactured with the manufacturing method.;COPYRIGHT: (C)2006,JPO&NCIPI
机译:解决的问题:提供一种用于钎焊的翅片材料,该翅片材料在被加热以进行钎焊之后具有优异的强度,导热性和自身的耐腐蚀性,在被加热以进行钎焊时对钎焊填料的扩散阻力以及波纹状可成形性。解决方案:用于钎焊的翅片材料的铝合金包含0.8质量%至2.0质量%的Si,大于1.0质量%但小于或等于3.0质量%的Mn,以及更多。 Fe小于0.10质量%但小于0.7质量%。鳍片材料的制造方法包括:将由铝合金制成的厚度为0.1mm或更薄的片材进行最终中间退火,以使其具有晶体结构,在该晶体结构中,直径为10mm或更大的重结晶晶粒在表面上退火。从表面观察时,轧制方向占表面积的80%以上。然后冷轧,板厚压下率小于30%。翅片材料采用制造方法制造。版权所有:(C)2006,日本特许厅

著录项

  • 公开/公告号JP4669712B2

    专利类型

  • 公开/公告日2011-04-13

    原文格式PDF

  • 申请/专利权人 古河スカイ株式会社;

    申请/专利号JP20050041211

  • 发明设计人 川原 晃;新倉 昭男;

    申请日2005-02-17

  • 分类号C22C21/00;C22F1/04;C22F1/00;F28F21/08;

  • 国家 JP

  • 入库时间 2022-08-21 18:18:30

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