首页|钛合金扩散连接技术及其层合结构疲劳裂纹扩展研究进展

钛合金扩散连接技术及其层合结构疲劳裂纹扩展研究进展

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本文主要对钛合金的扩散连接及层合结构疲劳裂纹扩展行为的研究进展进行了综述,总结了扩散连接钛合金界面的微观组织演变和疲劳裂纹扩展特性.首先概述了超塑成形/扩散连接技术的应用背景和优势,以及提高钛合金扩散连接界面质量的辅助技术(如添加中间层、热氢处理、脉冲电流加热和表面改性).从钛合金扩散连接和钛合金与其他合金扩散连接两方面综述了界面组织和力学性能,指出组织演变严重依赖界面处合金元素种类和元素相互扩散能力.扩散连接技术可用来制备同种和异种合金的层合结构,且可灵活控制界面焊合与未焊合区域的形状与分布.最后,简述了同种或异种钛合金扩散连接层合结构可降低疲劳裂纹扩展速率,从而优化钛合金构件的疲劳损伤容限性能.
Research Progress on Diffusion Bonding of Titanium Alloys and Fatigue Crack Growth of Their Laminates
In this work,the research progress on diffusion bonding of titanium alloys and fatigue crack growth(FCG)behavior of their laminates are briefly reviewed.Furthermore,the microstructural evolution and FCG characteristics at the interfaces of titanium alloys subjected to diffusion bonding are summarized.Firstly,the application background and advantages of superplastic forming/diffusion bonding technology are outlined,as well as some auxiliary technologies to improve the diffusion bonding interface quality of titanium alloys,such as the interlayer addition,thermohydrogen treatment,pulse current heating,and surface modification.The microstructures and mechanical properties of the bonded interfaces are shown based on the diffusion bonding of titanium alloys and titanium alloys with other alloys.The strong dependence of microstructural evolution on the alloy elements and interdiffusion ability of elements at the bonded interfaces is clarified.Diffusion bonding process can be used to fabricate the laminates of the same and different alloys,and the shape and distribution of the bonded and unbonded zones at the interfaces can be flexibly controlled.Finally,the diffusion bonding laminates with the same or different titanium alloys can be used to reduce the FCG rate.Therefore,the fatigue damage tolerance of titanium alloy components is optimized.

Titanium alloyDiffusion bondingMicrostructureLaminateFatigue crack growth(FCG)

李细锋、钟李欣、张骞文、李天乐、姜森宝、吴会平、陈军

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上海交通大学材料科学与工程学院塑性成形技术与装备研究院,上海 200030

中航西安飞机工业集团股份有限公司,西安 710089

航空工业成都飞机工业(集团)有限责任公司,成都 610091

钛合金 扩散连接 微观组织 层合结构 疲劳裂纹扩展(FCG)

辽宁联合基金上海市优秀学术带头人计划

U190822922XD1421600

2024

航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
年,卷(期):2024.67(1)
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