TY - JOUR
T1 - Integrated layout and topology optimization design of multi-component structure system under harmonic force excitation
AU - Zhu, Jihong
AU - Zhao, Hua
AU - Liu, Tao
AU - Zhang, Weihong
N1 - Publisher Copyright:
© 2018, Press of Chinese Journal of Aeronautics. All right reserved.
PY - 2018/1/25
Y1 - 2018/1/25
N2 - This paper presents an integrated layout and topology optimization of the multi-component structure system under harmonic force excitation. The configuration of the supporting structure and the component layout are simultaneously optimized to minimize the displacement responses that are obtained by using the Mode Acceleration Method (MAM). The Multi-Point Constraint (MPC) scheme is employed to simulate the rivets and bolts connecting components and supporting structures. The Finite Circle Method (FCM) is used to avoid overlaps among different components and boundaries of supporting structures. The mathematical model for the integrated layout and topology optimization of multi-component structure system is established, and the sensitivities of the objective function to design variables are deduced. Numerical examples are presented to demonstrate the effectiveness and validity of the proposed method for solving problems under harmonic force excitation.
AB - This paper presents an integrated layout and topology optimization of the multi-component structure system under harmonic force excitation. The configuration of the supporting structure and the component layout are simultaneously optimized to minimize the displacement responses that are obtained by using the Mode Acceleration Method (MAM). The Multi-Point Constraint (MPC) scheme is employed to simulate the rivets and bolts connecting components and supporting structures. The Finite Circle Method (FCM) is used to avoid overlaps among different components and boundaries of supporting structures. The mathematical model for the integrated layout and topology optimization of multi-component structure system is established, and the sensitivities of the objective function to design variables are deduced. Numerical examples are presented to demonstrate the effectiveness and validity of the proposed method for solving problems under harmonic force excitation.
KW - Finite circle method
KW - Harmonic force excitation
KW - Integrated layout and topology optimization
KW - Mode acceleration method
KW - Multi-point constraint
UR - http://www.scopus.com/inward/record.url?scp=85045397165&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2017.221575
DO - 10.7527/S1000-6893.2017.221575
M3 - 文章
AN - SCOPUS:85045397165
SN - 1000-6893
VL - 39
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 1
M1 - 221575
ER -