Reliability analysis methods based on the linear damage accumulation law (LDAL) and load-life interference model are studied in this paper. According to the equal probability rule, the equivalent loads are derived, an...Reliability analysis methods based on the linear damage accumulation law (LDAL) and load-life interference model are studied in this paper. According to the equal probability rule, the equivalent loads are derived, and the reliability analysis method based on load-life interference model and recurrence formula is constructed. In conjunction with finite element analysis (FEA) program, the reliability of an aero engine turbine disk under low cycle fatigue (LCF) condition has been analyzed. The results show the turbine disk is safety and the above reliability analysis methods are feasible.展开更多
针对SUS304不锈钢点焊接头进行静力学和疲劳试验,采用三参数幂函数方法建立点焊接头的载荷-寿命曲线;采用超声扫描显微镜对接头点焊区域进行超声波C扫描成像,分析焊接电流对点焊熔核直径及抗拉强度的影响.结果表明:基于熔核C扫描图像的...针对SUS304不锈钢点焊接头进行静力学和疲劳试验,采用三参数幂函数方法建立点焊接头的载荷-寿命曲线;采用超声扫描显微镜对接头点焊区域进行超声波C扫描成像,分析焊接电流对点焊熔核直径及抗拉强度的影响.结果表明:基于熔核C扫描图像的灰度值分布特征,可清晰甄别点焊接头熔核直径以及过烧、飞溅等熔核内部缺陷,实现点焊接头的无损检测;当焊接电流为8.5~10.5 k A时,点焊接头熔核直径从4.03 mm增至5.04 mm,接头抗拉强度呈先增大后减小的变化趋势,在焊接电流10.0 k A时,抗拉强度值出现拐点,接头最大抗拉强度为12.91 k N.在30%载荷水平时,点焊接头疲劳断裂形式为纽扣断裂;在20%和15%载荷水平时,基板呈眉状裂纹疲劳断裂.展开更多
基金Supports provided by Aviation Basic Science Foundation(00B53010)Aerospace Science Foundation(N3CH0502)Shaanxi Province Natural Science Foundation(N3CS0501)are gratefully appreciated.
文摘Reliability analysis methods based on the linear damage accumulation law (LDAL) and load-life interference model are studied in this paper. According to the equal probability rule, the equivalent loads are derived, and the reliability analysis method based on load-life interference model and recurrence formula is constructed. In conjunction with finite element analysis (FEA) program, the reliability of an aero engine turbine disk under low cycle fatigue (LCF) condition has been analyzed. The results show the turbine disk is safety and the above reliability analysis methods are feasible.
文摘针对SUS304不锈钢点焊接头进行静力学和疲劳试验,采用三参数幂函数方法建立点焊接头的载荷-寿命曲线;采用超声扫描显微镜对接头点焊区域进行超声波C扫描成像,分析焊接电流对点焊熔核直径及抗拉强度的影响.结果表明:基于熔核C扫描图像的灰度值分布特征,可清晰甄别点焊接头熔核直径以及过烧、飞溅等熔核内部缺陷,实现点焊接头的无损检测;当焊接电流为8.5~10.5 k A时,点焊接头熔核直径从4.03 mm增至5.04 mm,接头抗拉强度呈先增大后减小的变化趋势,在焊接电流10.0 k A时,抗拉强度值出现拐点,接头最大抗拉强度为12.91 k N.在30%载荷水平时,点焊接头疲劳断裂形式为纽扣断裂;在20%和15%载荷水平时,基板呈眉状裂纹疲劳断裂.
