马云龙1,湛利华2,3,徐永谦2,童璨瑜2,谭景升3. 高强铝合金板材电脉冲辅助时效热处理工艺研究*[J]. 航空制造技术, 2017, 60(23/24): 42-47. MA Yunlong1, ZHAN Lihua2,3, XU Yongqian2, TONG Canyu2, TAN Jingsheng3. Study on Electric Pulse Assisted Aging Process of High-Strength Aluminum Alloy Plates. Aeronautical Manufacturing Technology, 2017, 60(23/24): 42-47.
MA Yunlong, ZHAN Lihua, XU Yongqian, et al. Study on Electric Pulse Assisted Aging Process of High-Strength Aluminum Alloy Plates[J]. Aeronautical Manufacturing Technology, 2017, 60(23/24).
马云龙1,湛利华2,3,徐永谦2,童璨瑜2,谭景升3. 高强铝合金板材电脉冲辅助时效热处理工艺研究*[J]. 航空制造技术, 2017, 60(23/24): 42-47. MA Yunlong1, ZHAN Lihua2,3, XU Yongqian2, TONG Canyu2, TAN Jingsheng3. Study on Electric Pulse Assisted Aging Process of High-Strength Aluminum Alloy Plates. Aeronautical Manufacturing Technology, 2017, 60(23/24): 42-47. DOI: 10.16080/j.issn1671-833x.2017.23/24.042.
MA Yunlong, ZHAN Lihua, XU Yongqian, et al. Study on Electric Pulse Assisted Aging Process of High-Strength Aluminum Alloy Plates[J]. Aeronautical Manufacturing Technology, 2017, 60(23/24). DOI: 10.16080/j.issn1671-833x.2017.23/24.042.
Study on Electric Pulse Assisted Aging Process of High-Strength Aluminum Alloy Plates
The electric pulse assisted aging process of 2219 aluminum alloy plates is simulated and studied by experiments.The effect of electric pulse on the current density distribution
Joule heat effect
mechanical properties and precipitates microstructure is investigated by simulation analysis
electric pulse assisted aging test
tensile test and transmission electron microscopy observation. The results show that the peak current density of the electric pulse assisted aged plate is symmetrically distributed. Under the current density of 80A/cm2
the peak current density in most areas of the sheet is between 40 and 120A/cm2. Meanwhile
the temperature rise of the plate is less than 1℃ . Compared with the conventional aging process
the aging precipitation process is accelerated and the distribution of precipitates is homogenized after the electric pulse assisted aging process. The peak aging time was shortened from 15h to 10h
peak aging yield strength also increased from 283MPa to 303MPa. Furthermore
it indicated that the electric pulse assisted aging process can shorten the production time and improve the mechanical properties of the studied alloy.
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Related Author
GAO Hongliang
SU Haijun
GUO Yinuo
YANG Peixin
XIA Le
ZHANG Zhuo
GUO Min
Lü Qizhao
Related Institution
Shenzhen Research Institute of Northwestern Polytechnical University
School of Material Science and Engineering, Northwestern Polytechnical University
College of Mechanical & Power Engineering of Three Gorges University
School of Mechanical Science & Engineering of Huazhong University of Seience and Technology
Aviation Key Laboratory of Science and Technology on Precision Manufacturing Technology, AVIC Beijing Precision Engineering Institute for Aircraft Industry