李细锋,钟李欣,张骞文,李天乐,姜森宝,吴会平,陈军. 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[J]. 航空制造技术, 2024, 67(1/2): 14-26. LI Xifeng, ZHONG Lixin, ZHANG Qianwen, LI Tianle, JIANG Senbao, WU Huiping, CHEN Jun. Research Progress on Diffusion Bonding of Titanium Alloys and Fatigue Crack Growth of Their Laminates[J]. Aeronautical Manufacturing Technology, 2024, 67(1/2): 14-26.
LI Xifeng, ZHONG Lixin, ZHANG Qianwen, et al. Research Progress on Diffusion Bonding of Titanium Alloys and Fatigue Crack Growth of Their Laminates[J]. Aeronautical Manufacturing Technology, 2024, 67(1/2).
李细锋,钟李欣,张骞文,李天乐,姜森宝,吴会平,陈军. 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[J]. 航空制造技术, 2024, 67(1/2): 14-26. LI Xifeng, ZHONG Lixin, ZHANG Qianwen, LI Tianle, JIANG Senbao, WU Huiping, CHEN Jun. Research Progress on Diffusion Bonding of Titanium Alloys and Fatigue Crack Growth of Their Laminates[J]. Aeronautical Manufacturing Technology, 2024, 67(1/2): 14-26. DOI: 10.16080/j.issn1671-833x.2024.01/02.014.
LI Xifeng, ZHONG Lixin, ZHANG Qianwen, et al. Research Progress on Diffusion Bonding of Titanium Alloys and Fatigue Crack Growth of Their Laminates[J]. Aeronautical Manufacturing Technology, 2024, 67(1/2). DOI: 10.16080/j.issn1671-833x.2024.01/02.014.
Research Progress on Diffusion Bonding of Titanium Alloys and Fatigue Crack Growth of Their Laminates
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.