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民用飞机金属结构局部应力强度研究
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作者 宋猛 《中文科技期刊数据库(全文版)工程技术》 2024年第2期0143-0146,共4页
本研究旨在对民用飞机金属结构的局部应力强度进行研究。通过对2024-T42和7050-T6的标准试样和开孔试样的试验和分析,探讨了局部应力对飞机金属结构强度和可靠性的影响。研究结果表明,局部应力是导致金属结构疲劳破坏和裂纹扩展的主要... 本研究旨在对民用飞机金属结构的局部应力强度进行研究。通过对2024-T42和7050-T6的标准试样和开孔试样的试验和分析,探讨了局部应力对飞机金属结构强度和可靠性的影响。研究结果表明,局部应力是导致金属结构疲劳破坏和裂纹扩展的主要因素之一,孔折减系数起决定性影响的是材料的屈服应力与极限应力之间的差值,差值越大,孔折减系数越小。因此,对局部应力进行准确的评估和控制对于确保飞机结构的安全性具有重要意义。 展开更多
关键词 民用飞机 金属结构 局部应力强度
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双相钢搭接点焊接头疲劳寿命分析 被引量:24
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作者 许君 张延松 +1 位作者 朱平 陈关龙 《焊接学报》 EI CAS CSCD 北大核心 2008年第5期45-48,115,共5页
研究了双相钢焊点特征,对不同匹配双相钢搭接焊点进行了疲劳试验,获得了焊点的载荷寿命曲线。研究了双相钢焊点的疲劳裂纹扩展及失效形式,分析和解释了疲劳过程中的现象,并根据裂纹的实际扩展路径,提出了局部等效张开应力强度因子keq,... 研究了双相钢焊点特征,对不同匹配双相钢搭接焊点进行了疲劳试验,获得了焊点的载荷寿命曲线。研究了双相钢焊点的疲劳裂纹扩展及失效形式,分析和解释了疲劳过程中的现象,并根据裂纹的实际扩展路径,提出了局部等效张开应力强度因子keq,从断裂力学的角度对双相钢焊点的疲劳失效进行了分析。结果表明,keq能够有效地关联具有不同厚度,不同熔核直径的搭接焊点试样的疲劳寿命,是反映双相钢焊点疲劳强度的有效参量,能够用来预测焊点疲劳寿命。 展开更多
关键词 双相钢 点焊 疲劳强度 局部等效应力强度因子
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Mechanical properties of strengthened surface layer in Ti-6Al-4V alloy induced by wet peening treatment 被引量:5
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作者 李康 付雪松 +2 位作者 陈国清 周文龙 李志强 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2016年第11期2868-2873,共6页
A modified surface layer was formed on Ti-6Al-4V alloy by wet peening treatment. The variations of the residual stress,nano-hardness and microstructure of the modified layer with depth from surface were studied using ... A modified surface layer was formed on Ti-6Al-4V alloy by wet peening treatment. The variations of the residual stress,nano-hardness and microstructure of the modified layer with depth from surface were studied using X-ray diffraction analysis,nano-indentation analysis, scanning electron microscopy and transmission electron microscopy observations. The results show thatboth the compressive residual stress and hardness decrease with increasing depth, and the termination depths are 160 and 80 μm,respectively. The microstructure observation indicates that within 80 μm, the compressive residual stress and the hardness areenhanced by the co-action of the grain refinement strengthening and dislocation strengthening. Within 80–160 μm, the compressiveresidual stress mainly derives from the dislocation strengthening. The strengthened layer in Ti-6Al-4V alloy after wet peeningtreatment was quantitatively analyzed by a revised equation with respect to a relation between hardness and yield strength. 展开更多
关键词 Ti-6Al-4V alloy wet peening nano-hardness compressive residual stress local yield strength
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Segmentation of copper alloys processed by equal-channel angular pressing
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作者 Omid NEJADSEYFI Ali SHOKUHFAR Vahid MOODI 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2015年第8期2571-2580,共10页
This research provides experimental evidence for localized shear, billet cracking, and segmentation during the processing of various copper alloys. The results demonstrate that although many parameters affect the shea... This research provides experimental evidence for localized shear, billet cracking, and segmentation during the processing of various copper alloys. The results demonstrate that although many parameters affect the shear localization, there is a direct relation between segmentation and alloy strength (hardness) that is related to the alloying elements and constitutive phases. For instance, alpha brass is successfully processed by ECAP at room temperature, but alpha/beta brasses fail even at a temperature of 350 °C. Finite element simulation of cracking and segmentation was performed using DEFORMTM to investigate the influence of different parameters on segmentation. The results confirm that friction and processing speed have narrow effects on attaining a perfect billet. However, employing back pressure could be reliably used to diminish shear localization, billet cracking, segmentation, and damage. Moreover, diminishing the flow localization using back pressure leads to uniform material flow and the billet homogeneity increases by 36.1%, when back pressure increases from 0 to 600 MPa. 展开更多
关键词 back pressure BRASS BRONZE DAMAGE flow localization stress-strain behavior tensile strength DUCTILITY
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