TY - JOUR
T1 - Advances and challenges on springback control for creep age forming of aluminum alloy
AU - ZHANG, Liwen
AU - LI, Heng
AU - BIAN, Tianjun
AU - WU, Changhui
AU - GAO, Yang
AU - LEI, Chao
N1 - Publisher Copyright:
© 2021 Chinese Society of Aeronautics and Astronautics
PY - 2022/10
Y1 - 2022/10
N2 - 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 thin-walled 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.
AB - 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 thin-walled 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.
KW - Aluminum alloy
KW - Creep age forming
KW - Integrated manufacturing
KW - Springback compensation
KW - Tool design
UR - http://www.scopus.com/inward/record.url?scp=85121153517&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2021.10.019
DO - 10.1016/j.cja.2021.10.019
M3 - 文献综述
AN - SCOPUS:85121153517
SN - 1000-9361
VL - 35
SP - 8
EP - 34
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 10
ER -