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7A65铝合金喷丸强化表面完整性及疲劳性能 被引量:2
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作者 贺柏涵 周文龙 +4 位作者 程旭 盖鹏涛 李春艳 陈国清 付雪松 《精密成形工程》 北大核心 2023年第6期1-10,共10页
目的以7A65高强度铝合金为研究对象,研究喷丸强度、弹丸介质(铸钢丸和陶瓷丸)对靶材疲劳性能的影响规律。方法利用扫描电镜、激光共聚焦显微镜、X射线衍射仪等仪器表征喷丸强化7A65铝合金表面完整性和疲劳失效断口,分析喷丸工艺参数与... 目的以7A65高强度铝合金为研究对象,研究喷丸强度、弹丸介质(铸钢丸和陶瓷丸)对靶材疲劳性能的影响规律。方法利用扫描电镜、激光共聚焦显微镜、X射线衍射仪等仪器表征喷丸强化7A65铝合金表面完整性和疲劳失效断口,分析喷丸工艺参数与疲劳性能、断裂模式的相关性。结果喷丸强化后铝合金表面粗糙化严重,表面粗糙度从初始0.622μm增加至4.736μm(铸钢丸、喷丸强度为0.22 mmA),并出现褶皱损伤;在相同喷丸强度下陶瓷丸喷丸表面粗糙度较低,无褶皱损伤。2种弹丸在金属表面引入的残余应力场基本相同,残余压应力层深约300μm,最大残余压应力值为-480.6 MPa,其产生位置为距离表面75μm处(喷丸强度为0.22 mmA)。铝合金疲劳性能对铸钢丸介质敏感性较高,当喷丸强度较低(0.11 mmA)时喷丸强化效果最佳,疲劳寿命是原始寿命的5倍多,疲劳源从表面转移至次表面(500μm);当喷丸强度增至0.22 mmA时,裂纹源向表面靠近,疲劳寿命为原始寿命的2倍。铝合金疲劳性能对陶瓷丸介质敏感性较低,在喷丸强度为0.11~0.22 mmA时疲劳寿命较为稳定,在喷丸强度为0.11 mmA时疲劳寿命最高,为原始寿命的7倍。结论7A65高强度铝合金经喷丸强化后疲劳寿命显著提升,强化效果受弹丸介质影响,陶瓷丸介质强化效果更好、喷丸强化工艺窗口更宽。 展开更多
关键词 7a65铝合金 疲劳寿命 喷丸强化 表面完整性 表面粗糙度 残余应力
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基于正交铣削试验的7A65-T7451铝合金表面粗糙度预测模型 被引量:9
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作者 武洵德 王文理 《制造技术与机床》 北大核心 2021年第11期89-95,共7页
采用正交试验方法对新型铝合金7A65-T7451进行铣削试验,获得了大量该铝合金的表面粗糙度工艺参数。对试验数据进行了极差和均值分析,确定了各参数对表面粗糙度的影响顺序和影响趋势。基于多元线性回归分析,建立了表面粗糙度的预测模型,... 采用正交试验方法对新型铝合金7A65-T7451进行铣削试验,获得了大量该铝合金的表面粗糙度工艺参数。对试验数据进行了极差和均值分析,确定了各参数对表面粗糙度的影响顺序和影响趋势。基于多元线性回归分析,建立了表面粗糙度的预测模型,并对模型进行了误差检验。该预测模型为7A65-T7451铝合金铣削参数的合理选择提供了依据,对未来7A65铝合金应用于航空结构件时降低表面粗糙度及提高疲劳寿命有一定意义。 展开更多
关键词 7a65-T7451铝合金 正交试验 极差分析 多元线性回归 表面粗糙度预测
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Effect of Solution Treatment on Recrystallization,Texture and Mechanical Properties of 7A65-T74 Aluminum Alloy Super-thick Hot Rolled Plate
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作者 LI Chen WANG Hao +5 位作者 WANG Wenbo YE Chengtong JIN Zuheng ZHANG Xinquan ZHANG Hu JIA Lina 《Journal of Wuhan University of Technology(Materials Science)》 SCIE EI CAS 2022年第3期460-469,共10页
The effects of the solution treatment on the microstructure,recrystallization,texture composition and properties of 7A65-T7451(120 mm)hot rolled plates at H/2(1/2 thickness)and H/4(1/4 thickness)were studied.The resul... The effects of the solution treatment on the microstructure,recrystallization,texture composition and properties of 7A65-T7451(120 mm)hot rolled plates at H/2(1/2 thickness)and H/4(1/4 thickness)were studied.The results show that the hot rolled microstructure mainly contains a large amount of MgZn_(2) phases and minor Al_(7)Cu_(2)Fe phase.After solid solution treatments,a large amount of MgZn_(2) phases are dissolved back into the aluminum matrix.The main texture types at H/4 are R-Cube,Cube and part of Brass texture,and the main texture types at H/2 are Cube,R,and Copper texture.The qualitative analysis by Schmidt's law reveals that Copper texture at H/2 will deepen the anisotropy of plate metal properties.For the plate with the same thickness,the two-stage solution state has better mechanical properties due to the lower degree of recrystallization and stronger grain boundary strengthening effects.Under the two-stage solution system of 460℃/165 min+477℃/165 min,the composite mechanical properties of the alloy plate at H/4 are the best and the anisotropy is not obvious.The tensile strength,yield strength,and elongation along the rolling direction are 561.9 MPa,523.4 MPa,and 10.6%,respectively.. 展开更多
关键词 7a65 thick plate solid solution treatment TEXTURE RECRYSTALLIZATION ANISOTROPIC
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Hot deformation behavior of high Zn-containing 7A65 Al alloy 被引量:2
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作者 Chen Li Zhuo Chen +2 位作者 Xin-Quan Zhang Wen-Long Xiao Yue Ma 《Rare Metals》 SCIE EI CAS CSCD 2023年第1期302-312,共11页
Hot deformation behavior and microstructural evolution of as-homogenized 7A65 Al alloy under isothermal compression at temperatures of 573-713 K and strain rates of 0.1-10.0 s-1were investigated.It was found that the ... Hot deformation behavior and microstructural evolution of as-homogenized 7A65 Al alloy under isothermal compression at temperatures of 573-713 K and strain rates of 0.1-10.0 s-1were investigated.It was found that the flow stress of 7A65 Al alloy exhibited a typical dynamic recovery characteristic at high-temperature deformation conditions,and a sixth-order polynomial strain compensated Arrhenius constitutive equation was proposed to describe the flow behavior.Based on the dynamic material model and the Prasad standard,the hot processing map was established.The optimal processing conditions were within the temperature range of 633-713 K and the strain rate range of 0.1-0.5 s^(-1)when the true strain exceeded 0.6.Deformation temperature and strain rate had an obvious effect on the micros tructure evolution of 7A65Al alloy,and the deformed microstructures were mainly composed of deformed grains and recovery structure.The main softening mechanism was dynamic recovery at the temperature of 573-713 K and the strain rate of 0.1-10.0s-1,but dynamic recrystallization was enhanced with the increase in temperature. 展开更多
关键词 7a65 Al alloy Hot deformation behavior Constitutive model Processing map MICROSTRUCTURE
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