TY - JOUR
T1 - Precise output loads control of load-diffusion components with topology optimization
AU - CAO, Yinfeng
AU - GU, Xiaojun
AU - ZHU, Jihong
AU - ZHANG, Weihong
N1 - Publisher Copyright:
© 2019 Chinese Society of Aeronautics and Astronautics
PY - 2020/3
Y1 - 2020/3
N2 - The purpose of this paper is to present a novel topology optimization approach to control precisely the output loads under static loads and harmonic excitations. We introduce the Artificial Bar Element (ABE) at the designated output positions, where the output loads are equivalently measured and constrained with the nodal displacements of ABE. Optimization model is then formulated considering the output load constraints as well as the minimization of strain energy and dynamic displacement responses respectively under the static and dynamic conditions. The influences of the ABEs stiffness, different material usages of the design domain, widths of the output loads constraint intervals and variation ratios of output loads are discussed in detail. The proposed method is verified with several numerical examples with clear and reasonable load transfer paths.
AB - The purpose of this paper is to present a novel topology optimization approach to control precisely the output loads under static loads and harmonic excitations. We introduce the Artificial Bar Element (ABE) at the designated output positions, where the output loads are equivalently measured and constrained with the nodal displacements of ABE. Optimization model is then formulated considering the output load constraints as well as the minimization of strain energy and dynamic displacement responses respectively under the static and dynamic conditions. The influences of the ABEs stiffness, different material usages of the design domain, widths of the output loads constraint intervals and variation ratios of output loads are discussed in detail. The proposed method is verified with several numerical examples with clear and reasonable load transfer paths.
KW - Artificial bar elements
KW - Dynamic response
KW - Kreisselmeier-Steinhauser (KS) function
KW - Precise control of output loads
KW - Topology optimization
UR - http://www.scopus.com/inward/record.url?scp=85072027433&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2019.07.023
DO - 10.1016/j.cja.2019.07.023
M3 - 文献综述
AN - SCOPUS:85072027433
SN - 1000-9361
VL - 33
SP - 933
EP - 946
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 3
ER -