Fatigue Crack Growth Behavior of 7050-T7451 Aluminium Alloy Attachment Lug with Different Structures
摘 要
对7050-T7451铝合金直耳片、对称斜耳片和非对称斜耳片进行了不同方向、不同大小载荷下的疲劳裂纹扩展试验, 对比分析了疲劳裂纹扩展曲线和裂纹扩展路径。结果表明: 在加载方向和载荷峰值相同时, 对称斜耳片的疲劳寿命高于直耳片的, 且增大斜切角有利于提高其疲劳寿命; 对称斜耳片受纵向疲劳载荷时的疲劳寿命高于受斜向疲劳载荷时的, 初始裂纹在斜切角较小侧的非对称斜耳片更容易发生疲劳断裂; 随着加载角度的增大, 耳片的裂纹扩展方向与载荷方向的夹角逐渐减小; 受横向斜载荷的斜耳片, 其耳孔内侧首先出现裂纹, 其扩展方向与载荷方向的夹角约为45°。
Abstract
The fatigue crack growth experiments under different loads in different directions were conducted on the straight lug, symmetrical and unsymmetrical tapered lug of 7050-T7451 aluminum alloy, and then the fatigue crack growth curves and crack growth paths were analyzed and compared. The results show that under the same loading direction and peak load, the fatigue lives of the symmetrical tapered lugs were higher than those of the straight lugs and the increase of the oblique angle was in favor to improve the fatigue life. The fatigue life of the symmetrical tapered lug subjected to the vertical load was higher than that under the oblique load. The unsymmetrical tapered lugs with initial cracks at the side of relatively large oblique angle were relatively prone to fatigue fracture. With the increase of the loading angle, the angle between the crack extension direction and the loading direction decreased gradually. The cracks first appeared at the inside lug hole of the tapered lug subjected to the lateral load and the angle between the extension direction and the loading direction was about 45°.
中图分类号 TB301 DOI 10.11973/jxgccl201610020
所属栏目 材料性能及应用
基金项目
收稿日期 2015/6/15
修改稿日期 2016/7/25
网络出版日期
作者单位点击查看
备注杨卓君(1978—) , 男, 陕西岐山人, 讲师, 硕士。
引用该论文: YANG Zhuo-jun,WU Li-ming,WU Wei,LIU Zhan,DU Jin-qiang. Fatigue Crack Growth Behavior of 7050-T7451 Aluminium Alloy Attachment Lug with Different Structures[J]. Materials for mechancial engineering, 2016, 40(10): 89~93
杨卓君,伍黎明,武 卫,刘 展,杜金强. 7050-T7451铝合金不同结构耳片疲劳裂纹的扩展行为[J]. 机械工程材料, 2016, 40(10): 89~93
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参考文献
【1】RIGBY R, ALIABADI M H. Stress intensity factors for cracks at attachment lugs[J]. Engineering Failure Analysis, 1997,4(2): 133-146.
【2】KIM J H, LEE S B, HONG S G. Fatigue crack growth behavior of Al7075-T7451 attachment lugs under flight spectrum variation[J]. Eng Fract Mech,2003, 40: 135-144.
【3】黄其青. 对称与非对称斜削耳片危险部位及应力强度因子的有限元分析[J]. 航空学报, 1998, 19(4): 466-470.
【4】周丽君, 隋福成. 受轴向拉伸载荷作用的耳片强度研究[J]. 飞机设计, 2005(3): 30-32.
【5】伍黎明, 何宇廷, 张海威, 等. 铝合金耳片连接件结构参数对其断裂特性影响的有限元法模拟[J]. 机械工程材料, 2013, 37(12) : 92-95.
【6】伍黎明, 何宇廷, 张腾, 等.非对称斜耳片钉孔单边穿透裂纹应力强度因子计算研究[J].机械工程学报, 2012, 48(8): 39-43.
【7】伍黎明, 何宇廷, 张海威, 等.耳片斜切角对孔边疲劳裂纹扩展速率的影响[J].机械工程材料, 2012, 36(11): 106-112.
【2】KIM J H, LEE S B, HONG S G. Fatigue crack growth behavior of Al7075-T7451 attachment lugs under flight spectrum variation[J]. Eng Fract Mech,2003, 40: 135-144.
【3】黄其青. 对称与非对称斜削耳片危险部位及应力强度因子的有限元分析[J]. 航空学报, 1998, 19(4): 466-470.
【4】周丽君, 隋福成. 受轴向拉伸载荷作用的耳片强度研究[J]. 飞机设计, 2005(3): 30-32.
【5】伍黎明, 何宇廷, 张海威, 等. 铝合金耳片连接件结构参数对其断裂特性影响的有限元法模拟[J]. 机械工程材料, 2013, 37(12) : 92-95.
【6】伍黎明, 何宇廷, 张腾, 等.非对称斜耳片钉孔单边穿透裂纹应力强度因子计算研究[J].机械工程学报, 2012, 48(8): 39-43.
【7】伍黎明, 何宇廷, 张海威, 等.耳片斜切角对孔边疲劳裂纹扩展速率的影响[J].机械工程材料, 2012, 36(11): 106-112.
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