Acta Aeronautica et Astronautica Sinica ›› 2026, Vol. 47 ›› Issue (7): 232500.doi: 10.7527/S1000-6893.2025.32500
• Solid Mechanics and Vehicle Conceptual Design •
Received:2025-07-01
Revised:2025-08-20
Accepted:2025-09-10
Online:2025-09-19
Published:2025-09-18
Contact:
Xiaofan HE
Supported by:CLC Number:
Liang HAN, Xiaofan HE. Dynamic risk assessment of metallic lap-joint structures based on diagnosis and prognosis[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(7): 232500.
Table 5
C and m distribution parameters at different checkpoints
| 试件 | 检查周期/次 | C (对数正态分布) | m (正态分布) | ||
|---|---|---|---|---|---|
| µ | σ | µ | σ | ||
| #1 峰值载荷10 kN | t 0 | -25.383 7 | 1.108 3 | 2.733 7 | 0.048 1 |
| t 0+6 000 | -25.648 3 | 0.952 1 | 2.729 0 | 0.047 1 | |
| t 0+12 000 | -25.773 2 | 0.901 7 | 2.726 3 | 0.046 4 | |
| t 0+18 000 | -25.823 9 | 0.845 2 | 2.723 1 | 0.045 2 | |
| t 0+24 000 | -25.863 8 | 0.805 9 | 2.721 1 | 0.044 3 | |
| #3 峰值载荷8 kN | t 0 | -25.376 2 | 1.103 0 | 2.733 8 | 0.048 0 |
| t 0+20 000 | -25.829 4 | 0.889 9 | 2.726 8 | 0.046 2 | |
| t 0+40 000 | -26.046 6 | 0.841 1 | 2.724 1 | 0.044 8 | |
| t 0+60 000 | -26.197 3 | 0.781 8 | 2.723 6 | 0.043 9 | |
| t 0+80 000 | -26.304 6 | 0.731 0 | 2.724 3 | 0.045 1 | |
Table 6
Calculation time for SFPOF
| 诊断间隔 | 时间/s | |||||
|---|---|---|---|---|---|---|
| #1 | #2 | #1和#2平均 | #3 | #4 | #3和#4平均 | |
| ΔT = 250 | 978.36 | 1 083.72 | 1 031.04 | 2 253.22 | 1 356.02 | 1 804.62 |
| ΔT = 500 | 746.67 | 660.54 | 703.605 | 1 113.78 | 689.26 | 901.52 |
| ΔT = 1 000 | 339.7 | 406.08 | 372.89 | 585.67 | 373.09 | 479.38 |
| ΔT = 2 000 | 110.13 | 294.58 | 202.355 | 314.05 | 180.51 | 247.28 |
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