Research Article
Research on Optimization of Structural Parameters of Equipment Cabin Bottom Cover
Table 5
Surrogate model training samples.
| No. | /mm | /mm | /mm | Equivalent stress/MPa |
| 1 | 19.76 | 2.55 | 48.78 | 78.0 | 2 | 36.04 | 2.14 | 40.20 | 67.2 | 3 | 32.16 | 1.57 | 38.67 | 115.6 | 4 | 46.90 | 1.37 | 39.90 | 85.9 | 5 | 36.82 | 1.08 | 40.82 | 129.0 | 6 | 38.37 | 1.61 | 42.65 | 73.9 | 7 | 12.78 | 1.74 | 36.53 | 218.2 | 8 | 23.63 | 1.90 | 47.55 | 95.8 | 9 | 50.00 | 2.47 | 46.33 | 31.3 | 10 | 12.00 | 2.18 | 46.63 | 127.8 | 11 | 43.80 | 2.96 | 37.76 | 37.4 | 12 | 34.49 | 2.63 | 37.14 | 59.9 | 13 | 25.18 | 2.43 | 39.59 | 82.4 | 14 | 28.29 | 1.94 | 42.96 | 86.5 | 15 | 35.27 | 1.82 | 46.94 | 65.8 | 16 | 29.06 | 2.51 | 44.18 | 62.2 | 17 | 15.10 | 2.84 | 40.51 | 113.2 | 18 | 17.43 | 1.29 | 38.98 | 211.3 | 19 | 31.39 | 2.35 | 48.47 | 54.1 | 20 | 15.88 | 1.04 | 43.57 | 241.2 | 21 | 30.61 | 1.45 | 50.00 | 88.7 | 22 | 24.41 | 1.49 | 35.31 | 191.9 | 23 | 20.53 | 2.71 | 35.92 | 116.2 | 24 | 27.51 | 1.00 | 38.06 | 199.8 | 25 | 42.24 | 1.41 | 49.39 | 78.0 | 26 | 44.57 | 1.12 | 45.10 | 84.9 | 27 | 18.20 | 2.22 | 42.96 | 110.1 | 28 | 45.35 | 2.02 | 49.08 | 113.2 | 29 | 18.98 | 2.80 | 44.80 | 44.9 | 30 | 25.96 | 1.33 | 42.35 | 79.3 | 31 | 41.47 | 2.59 | 49.69 | 142.5 | 32 | 22.86 | 1.16 | 47.24 | 162.8 | 33 | 13.55 | 2.31 | 38.37 | 33.2 | 34 | 33.71 | 1.25 | 46.02 | 151.5 | 35 | 16.65 | 1.65 | 43.88 | 104.0 | 36 | 26.73 | 3.00 | 41.73 | 150.8 | 37 | 39.92 | 2.27 | 44.49 | 61.3 | 38 | 39.14 | 1.20 | 36.22 | 46.4 | 39 | 47.67 | 1.98 | 41.12 | 124.5 | 40 | 43.02 | 1.78 | 36.84 | 48.1 | 41 | 14.33 | 1.53 | 48.16 | 69.8 | 42 | 21.31 | 2.06 | 35.00 | 160.3 | 43 | 49.22 | 2.67 | 42.04 | 161.0 | 44 | 40.69 | 2.88 | 45.71 | 31.8 | 45 | 32.16 | 2.06 | 35.61 | 35.5 | 46 | 22.08 | 1.86 | 39.29 | 97.5 | 47 | 37.59 | 2.76 | 41.43 | 121.4 | 48 | 48.45 | 1.69 | 45.41 | 45.3 | 49 | 46.12 | 2.39 | 37.45 | 56.2 | 50 | 29.84 | 2.92 | 47.86 | 44.5 |
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