期刊
CHINESE JOURNAL OF AERONAUTICS
卷 35, 期 10, 页码 8-34出版社
ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2021.10.019
关键词
Aluminum alloy; Creep age forming; Integrated manufacturing; Springback compensation; Tool design
资金
- Key Program of the National Natural Science Foundation of China [51235010]
- National Science Fund for Excellent Young Scholars [51522509]
- National Natural Science Foundation of China [51905424]
Creep age forming (CAF) is an advanced forming technology that combines creep deformation and age hardening processes. It has many advantages such as low residual stress, dimensional stability, good performance, and short production cycle, making it optimal for manufacturing large-scale complicated thin-walled components of high strength aluminum alloys in aviation and aerospace industries. However, a major challenge of CAF is the occurrence of springback after unloading, which affects the accuracy of shaping components.
Creep age forming (CAF) is an advanced forming technology that combines creep deformation and age hardening processes. When compared with the conventional forming technologies including roll bending and shot-peen forming, CAF has many advantages of low residual stress, excellent dimensional stability, good service performance and short production cycle. It is an optimal technique for precise manufacturing for shape and properties of large-scale complicated thinwalled components of light-weight and high strength aluminum alloys in the aviation and aerospace industries. Nevertheless, CAF has an inevitable disadvantage that a large amount of springback occurs after unloading, which brings a challenge on the accurate shape forming and property tailoring of components. Therefore, how to achieve accurate prediction and control of springback has always been a bottleneck hindering the development of CAF to more industrial applications. After the factors of affecting springback and measures of reducing springback are summarized from the internal and external aspects, constitutive models for predicting springback and springback compensation methods for CAF of aluminum alloy panel components are reviewed. Then, a review of research progresses on tool design for CAF is presented. Finally, in view of the key issue that it is difficult to predict and control the shape and properties of components during CAF, the technical challenges are discussed and future development trends of CAF are prospected. (C) 2021 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
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