Acta Metallurgica Sinica (English Letters) ›› 2018, Vol. 31 ›› Issue (1): 105-112.DOI: 10.1007/s40195-017-0692-2
Special Issue: 2018年复合材料专辑
• Orginal Article • Previous Articles
Li-Fang Zheng1, Lu-Ning Wang2(), Zhao-Zhong Wang1, Li Wang1
Received:
2017-02-19
Online:
2018-01-20
Published:
2018-02-08
Li-Fang Zheng, Lu-Ning Wang, Zhao-Zhong Wang, Li Wang. Effects of γ-Ray Irradiation on the Fatigue Strength, Thermal Conductivities and Thermal Stabilities of the Glass Fibres/Epoxy Resins Composites[J]. Acta Metallurgica Sinica (English Letters), 2018, 31(1): 105-112.
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Fig. 2 SEM images of tensile-tensile fatigue fractures of the glass fibres/epoxy resins composites under different γ-ray irradiation doses: a 0 kGy, b 20 kGy, c 100 kGy, d 200 kGy (gas pores are circled by blue circles; debris of epoxy resin is circled by orange circles). (Color figure online)
Irradiation dose (kGy) | Mean static tensile strength (MPa) | Stress level, r (%) | Mean stress, σ m(MPa) | Stress amplitude, σa (MPa) | Fatigue cycle number, N (cycle) | ln(1 - r) | ln N |
---|---|---|---|---|---|---|---|
0 | 190.63 | 80 | 83.60 | 68.40 | 526.75 | - 1.6094 | 6.2667 |
60 | 62.70 | 51.30 | 4569 | 0.9163 | 8.4271 | ||
55 | 57.48 | 47.03 | 8209 | 0.7985 | 9.0130 | ||
40 | 41.80 | 34.20 | 243,162 | 0.5108 | 12.4015 | ||
20 | 184.50 | 80 | 81.40 | 66.60 | 954 | - 1.6094 | 6.8607 |
60 | 61.05 | 49.95 | 5852 | - 0.9163 | 8.6745 | ||
55 | 55.96 | 45.79 | 13,188 | - 0.7985 | 9.4871 | ||
40 | 40.70 | 33.30 | 353,245 | - 0.5108 | 12.7749 | ||
100 | 182.99 | 80 | 79.20 | 64.80 | 1091.25 | - 1.6094 | 6.9951 |
60 | 59.40 | 48.60 | 6637 | - 0.9163 | 8.8004 | ||
55 | 54.45 | 44.55 | 14,973 | - 0.7985 | 9.6140 | ||
40 | 39.60 | 32.40 | 467,244 | - 0.5108 | 13.0546 | ||
200 | 176.14 | 80 | 77.44 | 63.36 | 1166 | - 1.6094 | 7.0613 |
60 | 58.08 | 47.52 | 8337 | - 0.9163 | 9.0285 | ||
55 | 53.24 | 43.56 | 16,970 | - 0.7985 | 9.7392 | ||
40 | 38.72 | 31.68 | 600,128 | - 0.5108 | 13.3049 |
Table 1 Results of fatigue test for the glass fibres/epoxy resins composites before and after γ-ray irradiation
Irradiation dose (kGy) | Mean static tensile strength (MPa) | Stress level, r (%) | Mean stress, σ m(MPa) | Stress amplitude, σa (MPa) | Fatigue cycle number, N (cycle) | ln(1 - r) | ln N |
---|---|---|---|---|---|---|---|
0 | 190.63 | 80 | 83.60 | 68.40 | 526.75 | - 1.6094 | 6.2667 |
60 | 62.70 | 51.30 | 4569 | 0.9163 | 8.4271 | ||
55 | 57.48 | 47.03 | 8209 | 0.7985 | 9.0130 | ||
40 | 41.80 | 34.20 | 243,162 | 0.5108 | 12.4015 | ||
20 | 184.50 | 80 | 81.40 | 66.60 | 954 | - 1.6094 | 6.8607 |
60 | 61.05 | 49.95 | 5852 | - 0.9163 | 8.6745 | ||
55 | 55.96 | 45.79 | 13,188 | - 0.7985 | 9.4871 | ||
40 | 40.70 | 33.30 | 353,245 | - 0.5108 | 12.7749 | ||
100 | 182.99 | 80 | 79.20 | 64.80 | 1091.25 | - 1.6094 | 6.9951 |
60 | 59.40 | 48.60 | 6637 | - 0.9163 | 8.8004 | ||
55 | 54.45 | 44.55 | 14,973 | - 0.7985 | 9.6140 | ||
40 | 39.60 | 32.40 | 467,244 | - 0.5108 | 13.0546 | ||
200 | 176.14 | 80 | 77.44 | 63.36 | 1166 | - 1.6094 | 7.0613 |
60 | 58.08 | 47.52 | 8337 | - 0.9163 | 9.0285 | ||
55 | 53.24 | 43.56 | 16,970 | - 0.7985 | 9.7392 | ||
40 | 38.72 | 31.68 | 600,128 | - 0.5108 | 13.3049 |
Irradiation dose (kGy) | c 1 | B 1 | Two-parameter fatigue life model | N (Cycle) |
---|---|---|---|---|
0 | 0.3022 | 32.98622 | N = [32.98622335(1 - r)]1/0.30220 | < 104 |
20 | 0.32103 | 44.06783 | N = [44.06782833(1 - r)]1/0.32103 | |
100 | 0.32197 | 46.29898 | N = [46.29898321(1 - r)]1/0.32197 | |
200 | 0.31341 | N = [44.98998907(1 - r)]1/0.31341 | ||
Irradiation dose (kGy) | c 2 | B 2 | Two-parameter fatigue life model | N (Cycle) |
0 | 0.09025 | 5.153108 | N = [5.153107857(1 - r)]1/0.09025 | ≥ 104 |
20 | 0.09362 | 5.513998 | N = [5.513998276(1 - r)]1/0.09362 | |
100 | 0.09587 | 5.740292 | N = [5.740291540(1 - r)]1/0.09587 | |
200 | 0.09801 | 5.987476 | N = [5.987476273(1 - r)]1/0.09801 |
Table 2 Two-parameter fatigue life model of the glass fibres/epoxy composites with 20, 100 and 200 kGy irradiation doses
Irradiation dose (kGy) | c 1 | B 1 | Two-parameter fatigue life model | N (Cycle) |
---|---|---|---|---|
0 | 0.3022 | 32.98622 | N = [32.98622335(1 - r)]1/0.30220 | < 104 |
20 | 0.32103 | 44.06783 | N = [44.06782833(1 - r)]1/0.32103 | |
100 | 0.32197 | 46.29898 | N = [46.29898321(1 - r)]1/0.32197 | |
200 | 0.31341 | N = [44.98998907(1 - r)]1/0.31341 | ||
Irradiation dose (kGy) | c 2 | B 2 | Two-parameter fatigue life model | N (Cycle) |
0 | 0.09025 | 5.153108 | N = [5.153107857(1 - r)]1/0.09025 | ≥ 104 |
20 | 0.09362 | 5.513998 | N = [5.513998276(1 - r)]1/0.09362 | |
100 | 0.09587 | 5.740292 | N = [5.740291540(1 - r)]1/0.09587 | |
200 | 0.09801 | 5.987476 | N = [5.987476273(1 - r)]1/0.09801 |
Fig. 6 Variation of elongation and CTE with respect to the temperature under different γ-ray irradiation doses: a 0 kGy, b 20 kGy, c100 kGy, d 200 kGy
Fig. 7 TG, DTG and DSC curves of the glass fibres/epoxy composites under different γ-ray irradiation doses: a 0 kGy, b 20 kGy, c 100 kGy and d 200 kGy
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