钎焊间隙对K465高温合金接头微观组织与拉伸性能的影响OA
Effect of brazing gap on microstructures and tensile properties of K465 superalloy joint
为了提高 K465高温合金叶片服役裂纹钎焊修复接头的高温性能,采用新型 Co-Cr-Ni-W-Al-Ti-Ta-B钎料,在 1220℃/15 min条件下分别对 0.05 mm和 0.2 mm两种间隙 K465高温合金钎焊连接进行研究,分析两种接头微观组织、元素分布规律和高温拉伸性能.结果表明,钎料对母材有优异的冶金相容性,钎焊过程中发生明显元素互扩散.0.05 mm间隙接头由 γ'相弥散分布的 γ/γ'双相基体和(W,Cr)B、富 Ti硼化物、NiAl等化合物相组成;对于0.2 mm间隙接头,由于引入高温合金粉末填充材料,化合物相弥散分布、尺寸细化,但相种类未发生改变.两种间隙接头 1000℃高温拉伸性能相当,0.05 mm和 0.2 mm间隙钎焊接头抗拉强度分别为 383 MPa和 396 MPa,约为K465合金母材的 70%.由于钎料与母材之间良好的冶金相容性以及 B2有序 NiAl相的强化作用,两种间隙钎焊接头均表现出优异的高温拉伸性能.
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.
王浩;丁宁;翟智梁;任新宇;陈波
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空军装备部驻北京地区第六军事代表室,北京 100013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
矿业与冶金
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
K465 superalloybrazing repairbrazing gapjoint microstructurehigh-temperature tensile strength
《航空材料学报》 2026 (4)
99-107,9
国家自然科学基金(52201050)
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