采用单向碳/环氧复合材料补片真空袋压工艺单面修复含中心裂纹铝合金板,进行0-1700h盐雾梯度腐蚀试验,测试并对比分析了各腐蚀时间结点上试件修复前后的疲劳性能,从疲劳寿命、疲劳临界裂纹长度和Paris公式材料常数(C和m)的变化三个方面考察不同盐雾腐蚀深度对铝合金裂纹板修复前后的疲劳性能差异.结果表明:碳/环氧补片胶接修复铝合金板能大幅度提高疲劳寿命,且未经修复的裂纹板在腐蚀1700小时后疲劳寿命下降53.8%,而修复板仅为38.6%.修复板疲劳裂纹临界长度αcr大于未修复裂纹板,且随盐雾腐蚀时间延长,裂纹板和修复板αcr变化不大,可作准判据使用.由试验数据得到的不同腐蚀时间上试样的材料常数C和m随腐蚀时间延长而减小.利用Paris公式可较好拟合铝合金板疲劳寿命及Paris区内的疲劳裂纹扩展行为,但疲劳寿命预测值与实际值的差异由未经腐蚀时的5%左右增大到腐蚀1500h时的10%左右.
参考文献
[1] | BAKER A A.Repair of cracked or defective metallic air-craft-components with advanced fiber composites[J].Computers & Structures,1984(02):153-234. |
[2] | ERDOGAN F;ARIN K A.Sandwich plate with a part-through and a debonding crack[J].Engineering Fracture Mechanics,1972(02):449-458. |
[3] | V. Sabelkin;S. Mall;J.B. Avram .Fatigue crack growth analysis of stiffened cracked panel repaired with bonded composite patch[J].Engineering Fracture Mechanics,2006(11):1553-1567. |
[4] | SANKARAN K K;PEREZ R;JATA K V .Effects of putting corrosion on the fatigue behavior of aluminum alloy70752T 6:modeling and experimental studies[J].Materials Science and Engineering A:Structural Materials Properties Microstructure and Processing,2001,297:223-229. |
[5] | DU M L;CHIANG F P;KAGWADE S V et al.Damage of Al 2024 alloy due to sequential expo sure to fatigue[J].Corrosion and Fatigue Int J Fatigue,1998,20(10):743-748. |
[6] | SCHUBBE J J .Thickness effects on a cracked aluminum plate with composite patch repair[D].US,Philosophy of air force institute of technology of Wright-Patterson AFB,Ohio,1997. |
[7] | H. Hosseini-Toudeshky .Effects of composite patches on fatigue crack propagation of single-side repaired aluminum panels[J].Composite structures,2006(3):243-251. |
[8] | H. Hosseini-Toudeshky;S. Bakhshandeh;B. Mohammadi;H.R. Daghyani .Experimental investigations on fatigue crack growth of repaired thick aluminium panels in mixed-mode conditions[J].Composite structures,2006(1/4):437-443. |
[9] | TAI G C;SHEN S B .Fatigue analysis of cracked thick aluminum plate bonded with composite patches[J].Computers & Structures,2004,64:79-90. |
[10] | PYUN S I;MOON S M;LEE E J .Effect of electrolyte layer thickness on atmospheric corrosion of Al-1Si-0.5Cu[J].British Corrosion Journal,1994,29(03):190-193. |
[11] | 何建平,陈素晶,袁庆铭,樊蔚勋.NaCl电解液薄层下LC4CS铝合金腐蚀疲劳性能[J].南京航空航天大学学报,2004(04):412-416. |
[12] | 乔海霞 .铝绞线复合材料芯的性能研究[D].长沙:国防科学技术大学,2006. |
[13] | 朱波,蔡珣,刘建军,蔡华甦.单向碳纤维/环氧树脂复合材料疲劳裂纹扩展的研究[J].工程塑料应用,2002(11):44-46. |
[14] | PAN J;LIN S H.Fracture mechanics and fatigue crack propagation[A].Oxford:Elsevier,2005:237-284. |
[15] | 王遵 .复合材料单面补强含裂纹铝合金薄板的残余热应力及其影响研究[D].国防科学技术大学,2007. |
[16] | ALAWI H;SALEH I E .Fatigue crack growth retardation by bonding patches[J].Engineering Fracture Mechanics,1992,42(05):861-868. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%