Acta Aeronautica et Astronautica Sinica ›› 2023, Vol. 44 ›› Issue (14): 428029-428029.doi: 10.7527/S1000-6893.2022.28029
• Material Engineering and Mechanical Manufacturing • Previous Articles
Jiangbo CHEN, Kai ZENG(), Baoying XING, Hongshen ZHANG, Yanfang DING, Xiaocong HE
Received:
2022-09-21
Revised:
2022-11-03
Accepted:
2022-11-28
Online:
2022-12-02
Published:
2022-11-29
Contact:
Kai ZENG
E-mail:kmzk201109@163.com
Supported by:
CLC Number:
Jiangbo CHEN, Kai ZENG, Baoying XING, Hongshen ZHANG, Yanfang DING, Xiaocong HE. Aluminum alloy clinch-bonding with hot melt adhesive film and joint failure analysis[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(14): 428029-428029.
Table 2
Testing schemes and results of clinch-bonded joints
组号 | 冲压力 | 胶膜厚度 | 板材硬度 | 失效载荷 | 能量吸收值 |
---|---|---|---|---|---|
1 | 44.6 | 0.06 | 56 | 7 517.9 | 5.2 |
2 | 37.2 | 0.10 | 18 | 5 706.4 | 5.9 |
3 | 44.6 | 0.10 | 32 | 6 067.5 | 5.0 |
4 | 37.2 | 0.15 | 32 | 6 064.1 | 7.8 |
5 | 52.6 | 0.10 | 18 | 5 888.4 | 5.3 |
6 | 44.6 | 0.06 | 18 | 5 815.6 | 5.4 |
7 | 37.2 | 0.06 | 32 | 5 697.9 | 7.1 |
8 | 52.6 | 0.06 | 32 | 6 085.5 | 5.8 |
9 | 52.6 | 0.10 | 56 | 7 656.3 | 5.8 |
10 | 44.6 | 0.10 | 32 | 5 521.8 | 6.3 |
11 | 44.6 | 0.15 | 56 | 7 694.6 | 6.1 |
12 | 52.6 | 0.15 | 32 | 6 127.2 | 7.6 |
13 | 44.6 | 0.15 | 18 | 5 971.4 | 7.8 |
14 | 37.2 | 0.10 | 56 | 5 908.1 | 3.7 |
15 | 44.6 | 0.10 | 32 | 6 249.8 | 6.2 |
Table 3
Variance analysis of model
目标量 | 因素 | 平方和 | 自由度 | 均方差 | ||
---|---|---|---|---|---|---|
失效载荷 | 模型 | 6 | 9.47 | 0.002 8 | ||
1 | 8.42 | 0.020 9 | ||||
68 535.27 | 1 | 68 535.27 | 0.60 | 0.461 5 | ||
1 | 32.50 | 0.000 5 | ||||
1 | 6.33 | 0.036 1 | ||||
1 | 2.22 | 0.174 8 | ||||
1 | 4.76 | 0.060 8 | ||||
失拟项 | 6 | 0.73 | 0.676 0 | |||
能量吸收值 | 模型 | 15.62 | 6 | 2.60 | 7.70 | 0.005 5 |
0.08 | 1 | 0.08 | 0.23 | 0.645 1 | ||
4.29 | 1 | 4.29 | 12.69 | 0.007 4 | ||
1.56 | 1 | 1.56 | 4.60 | 0.064 4 | ||
2.24 | 1 | 2.24 | 6.62 | 0.033 0 | ||
3.69 | 1 | 3.69 | 10.92 | 0.010 8 | ||
1.85 | 1 | 1.85 | 5.47 | 0.047 6 | ||
失拟项 | 1.68 | 6 | 0.28 | 0.54 | 0.761 3 |
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