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钎焊间隙对K465高温合金接头微观组织与拉伸性能的影响

王浩 丁宁 翟智梁 任新宇 陈波

航空材料学报2026,Vol.46Issue(4):99-107,9.
航空材料学报2026,Vol.46Issue(4):99-107,9.DOI:10.11868/j.issn.1005-5053.2025.000224

钎焊间隙对K465高温合金接头微观组织与拉伸性能的影响

Effect of brazing gap on microstructures and tensile properties of K465 superalloy joint

王浩 1丁宁 2翟智梁 1任新宇 1陈波1

作者信息

  • 1. 中国航发北京航空材料研究院 焊接与塑性成形研究所,北京 100095
  • 2. 空军装备部驻北京地区第六军事代表室,北京 100013
  • 折叠

摘要

Abstract

To improve the high-temperature performance of brazed repair joints for service cracks in K465 superalloy blades,a novel Co-Cr-Ni-W-Al-Ti-Ta-B brazing filler metal is employed to braze K465 superalloy with gap widths of 0.05 mm and 0.2 mm under the condition of 1220℃/15 min.The microstructure,elemental distribution,and high-temperature tensile properties of two joints are analyzed.The results show that the brazing filler metal exhibits excellent metallurgical compatibility with the base metal,with significant interdiffusion of elements occurring during the brazing process.The joint with a 0.05 mm gap consists of a γ/γ' dual phase matrix with dispersed γ' phase,as well as compound phases including(W,Cr)B,Ti-rich boride,and NiAl.For the joint with a 0.2 mm gap,the introduction of superalloy powder as a filler material results in dispersed and refined compound phases,while the phase types remain unchanged.The high-temperature tensile properties at 1000℃of two joints are comparable:the tensile strength of the 0.05 mm and 0.2 mm gap joint is 383 MPa and 396 MPa,respectively,reaching approximately 70%of the K465 base metal.Due to the favorable metallurgical compatibility between the brazing filler metal and the base metal,as well as the strengthening effect of the B2-ordered NiAl phase,two kinds of brazed joints exhibit excellent high-temperature tensile properties.

关键词

K465高温合金/钎焊修复/钎焊间隙/接头微观组织/高温抗拉强度

Key words

K465 superalloy/brazing repair/brazing gap/joint microstructure/high-temperature tensile strength

分类

矿业与冶金

引用本文复制引用

王浩,丁宁,翟智梁,任新宇,陈波..钎焊间隙对K465高温合金接头微观组织与拉伸性能的影响[J].航空材料学报,2026,46(4):99-107,9.

基金项目

国家自然科学基金(52201050) (52201050)

航空材料学报

1005-5053

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