TY - JOUR
T1 - 航空铆钉连接件的抗冲击性能
AU - Wang, Cunxian
AU - Gao, Haomai
AU - Gong, Xu
AU - Suo, Tao
AU - Li, Yulong
AU - Tang, Zhongbin
AU - Xue, Pu
AU - Hou, Liang
AU - Lin, Jiajian
N1 - Publisher Copyright:
© 2019, Press of Chinese Journal of Aeronautics. All right reserved.
PY - 2019/1/25
Y1 - 2019/1/25
N2 - Using the split Hopkinson tensile bar device, a series of special riveting specimens for MS20615 rivet are designed, and the dynamic mechanical tests of riveting structures are performed under different loading angles and loading rates. In addition, the quasi-static mechanical properties of riveting structures are also obtained by conducting tests of the pure shear, 30°tension-shear coupling, 45°tension-shear coupling, 60°tension-shear coupling, and pure tension. Results show that the failure modes of riveting structures are significantly influenced by the loading angles and loading rates. Moreover, using the financial software LS-Dyna, the simplified finite element models (FE models) are established. The comparisons of force-displacement curves for the experiments and simulations are conducted to verify the feasibility of the simplified model. Meanwhile, the mesh correlation analysis is also performed as a supplementary verification.
AB - Using the split Hopkinson tensile bar device, a series of special riveting specimens for MS20615 rivet are designed, and the dynamic mechanical tests of riveting structures are performed under different loading angles and loading rates. In addition, the quasi-static mechanical properties of riveting structures are also obtained by conducting tests of the pure shear, 30°tension-shear coupling, 45°tension-shear coupling, 60°tension-shear coupling, and pure tension. Results show that the failure modes of riveting structures are significantly influenced by the loading angles and loading rates. Moreover, using the financial software LS-Dyna, the simplified finite element models (FE models) are established. The comparisons of force-displacement curves for the experiments and simulations are conducted to verify the feasibility of the simplified model. Meanwhile, the mesh correlation analysis is also performed as a supplementary verification.
KW - Failure load
KW - Failure mode
KW - Finite element simulation
KW - Mechanical property
KW - Riveting structures
KW - Split Hopkinson tension bar
UR - http://www.scopus.com/inward/record.url?scp=85064457323&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2018.22484
DO - 10.7527/S1000-6893.2018.22484
M3 - 文章
AN - SCOPUS:85064457323
SN - 1000-6893
VL - 40
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 1
M1 - 522484
ER -