期刊文献+
共找到7篇文章
< 1 >
每页显示 20 50 100
喷丸成形压力对7B50-T7751铝合金力学性能的影响 被引量:2
1
作者 尹佳 胡彦华 +2 位作者 徐刚 张炜 姜伟 《精密成形工程》 北大核心 2023年第4期74-82,共9页
目的 研究7B50-T7751铝合金在不同喷丸成形压力下力学性能的变化规律,探究喷丸成形压力对材料表面形貌、疲劳寿命及静力性能的影响。方法 在不同的喷丸成形压力(0.42、0.50 MPa)下对7B50-T7751铝合金进行处理,分析材料的表面形貌。在此... 目的 研究7B50-T7751铝合金在不同喷丸成形压力下力学性能的变化规律,探究喷丸成形压力对材料表面形貌、疲劳寿命及静力性能的影响。方法 在不同的喷丸成形压力(0.42、0.50 MPa)下对7B50-T7751铝合金进行处理,分析材料的表面形貌。在此基础上,通过细节额定疲劳基准值和截止值进行计算,并进行压缩试验,结合铝合金材料在喷丸前后应变层的位错密度和形态,分析喷丸成形压力对合金材料疲劳寿命和静力性能的影响。结果 与未喷丸试件相比,在0.42 MPa的成形压力下,合金材料的疲劳寿命和静力性能均有所提高。喷丸成形之后,材料表层引入了一定深度的残余压应力层,形成位错密度较大的加工硬化组织,阻碍裂纹扩展,宏观上提高了材料的强度。在0.50 MPa的成形压力下,材料表面更加粗糙,裂纹易在晶粒连接薄弱处萌生,导致合金材料的疲劳寿命有所降低。结论 随着喷丸成形压力的增大,合金材料的疲劳寿命先增大后减小,抗压强度有所增大。在0.50 MPa的成形压力下,部分裂纹易于在弹坑边缘萌生,在一定程度上会降低合金材料的疲劳强度。 展开更多
关键词 喷丸成形压力 7b50-t7751铝合金 力学性能 疲劳寿命 抗压强度
下载PDF
宽幅7B50-T7751铝合金厚板不均匀性与疲劳性能研究
2
作者 雷越 郝敏 +2 位作者 陈高红 伊琳娜 臧金鑫 《材料工程》 EI CAS CSCD 北大核心 2023年第11期103-110,共8页
采用力学万能试验机、扫描电镜等分析测试手段研究80 mm厚宽幅7B50-T7751板材不同宽度、不同厚度位置的组织与性能均匀性,并与7050-T7451板材疲劳性能进行对比与讨论。结果表明:宽幅7B50-T7751厚板力学性能优异,在L和LT方向上,1/2厚度... 采用力学万能试验机、扫描电镜等分析测试手段研究80 mm厚宽幅7B50-T7751板材不同宽度、不同厚度位置的组织与性能均匀性,并与7050-T7451板材疲劳性能进行对比与讨论。结果表明:宽幅7B50-T7751厚板力学性能优异,在L和LT方向上,1/2厚度的拉伸屈服强度分别达到568 MPa和545 MPa,抗拉强度分别达到612 MPa和591 MPa,压缩屈服强度分别达到575 MPa和587 MPa,L-T向与T-L向的断裂韧度达到30.16 MPa·m^(1/2)和26.47 MPa·m^(1/2)。宽幅厚板在不同宽度位置存在一定的各向异性,LT方向上的性能均匀性优于L方向。1/4厚度不同宽度位置性能无明显差异,1/2厚度宽度边缘位置性能优于宽度中心位置。1/4厚度未形成明显强织构,在1/2厚度宽度中心的主要织构为S织构和Brass织构,边缘的主要织构为R织构、S织构和Brass织构。在应力比为0.06时,宽幅7B50-T7751厚板的T-L向抗疲劳裂纹扩展速率性能优于同厚度7050-T7451板材,LT向光滑试样(Kt=1)的疲劳极限低于7050-T7451板材约7.6%,缺口试样(Kt=3)的疲劳极限高于7050-T7451板材约3.7%。 展开更多
关键词 7b50-t7751 宽幅厚板 不均匀性 微观组织 疲劳性能
下载PDF
7B50-T7751铝合金喷丸强化表面形态衍化及其对疲劳性能的影响 被引量:6
3
作者 高国强 陈金祥 +2 位作者 薛红前 张贤杰 杨辉 《中国表面工程》 EI CAS CSCD 北大核心 2022年第4期187-195,共9页
采用陶瓷弹丸对7B50-T7751铝合金进行不同覆盖率(100%、300%、600%、1000%)的表面喷丸强化处理,探究了7B50-T7751铝合金表面粗糙度、表面微观组织以及残余应力场等表面形态因素在不同喷丸覆盖率作用下的衍化规律。通过应力比R=0.06的轴... 采用陶瓷弹丸对7B50-T7751铝合金进行不同覆盖率(100%、300%、600%、1000%)的表面喷丸强化处理,探究了7B50-T7751铝合金表面粗糙度、表面微观组织以及残余应力场等表面形态因素在不同喷丸覆盖率作用下的衍化规律。通过应力比R=0.06的轴向加载疲劳试验,分析表面形态改变对疲劳强度的影响。结果表明,不同覆盖率的喷丸强化处理均能改善该材料的疲劳性能,其中在100%~300%喷丸覆盖率下,疲劳强化增益效果最为明显,其机理是试件在喷丸处理后表面形态得以改善,同时表层形成较高水平的残余压应力,这两种效应的共同作用使疲劳裂纹源从材料表面缺陷处向内迁移到材料内部容易产生应力集中的夹杂处。 展开更多
关键词 喷丸强化 覆盖率 7b50-t7751铝合金 表面形态 疲劳强度
下载PDF
Computation of synthetic surface heat transfer coefficient of 7B50 ultra-high-strength aluminum alloy during spray quenching 被引量:6
4
作者 Lei KANG Gang ZHAO +1 位作者 Ni TIAN Hai-tao ZHANG 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2018年第5期989-997,共9页
According to inverse heat transfer theory, the evolutions of synthetic surface heat transfer coefficient(SSHTC) of the quenching surface of 7B50 alloy during water-spray quenching were simulated by the Pro CAST soft... According to inverse heat transfer theory, the evolutions of synthetic surface heat transfer coefficient(SSHTC) of the quenching surface of 7B50 alloy during water-spray quenching were simulated by the Pro CAST software based on accurate cooling curves measured by the modified Jominy specimen and temperature-dependent thermo-physical properties of 7 B50 alloy calculated using the JMat Pro software. Results show that the average cooling rate at 6 mm from the quenching surface and 420-230 ℃(quench sensitive temperature range) is 45.78℃/s. The peak-value of the SSHTC is 69 kW/(m^2·K) obtained at spray quenching for 0.4 s and the corresponding temperature of the quenching surface is 160 ℃. In the initial stage of spray quenching, the phenomenon called "temperature plateau" appears on the cooling curve of the quenching surface. The temperature range of this plateau is 160-170℃ with the duration about 3 s. During the temperature plateau, heat transfer mechanism of the quenching surface transforms from nucleate boiling regime to single-phase convective regime. 展开更多
关键词 7b50 aluminum alloy water-spray quenching inverse heat transfer theory synthetic surface heat transfer coefficient cooling curve
下载PDF
四种典型大气环境下7B50铝合金的腐蚀行为研究 被引量:6
5
作者 钟勇 苏艳 +8 位作者 罗来正 吴洋 杨华明 陈喜栋 赵全成 吴帅 朱玉琴 舒畅 滕俊鹏 《装备环境工程》 CAS 2021年第11期143-150,共8页
目的研究湿热海洋、干热沙漠、寒冷乡村、暖温高原四种典型大气环境对7B50铝合金腐蚀行为的影响。方法采用户外大气自然环境暴露试验,通过宏观腐蚀形貌分析、金相显微形貌分析、腐蚀深度分析和拉伸性能分析,对比研究7B50-T7751和7B50-T7... 目的研究湿热海洋、干热沙漠、寒冷乡村、暖温高原四种典型大气环境对7B50铝合金腐蚀行为的影响。方法采用户外大气自然环境暴露试验,通过宏观腐蚀形貌分析、金相显微形貌分析、腐蚀深度分析和拉伸性能分析,对比研究7B50-T7751和7B50-T77511两种铝合金在不同大气环境中的腐蚀行为和规律。结果暴露试验周期为3 a时,7B50-T7751铝合金在湿热海洋大气环境中腐蚀严重,局部最大腐蚀深度为166μm,抗拉强度和断后伸长率分别下降了5%和25%;在干热沙漠大气环境下腐蚀较重,局部最大腐蚀深度为44μm;在寒冷乡村、暖温高原大气环境下未见明显腐蚀。7B50-T77511铝合金在四种典型大气环境下均表现出明显腐蚀,局部最大腐蚀深度分别为141、80、42、29μm。结论两种7B50铝合金在典型大气环境中表现出不同的耐蚀性,在微观上均表现为点蚀和晶间腐蚀的混合腐蚀,具有明显的晶间腐蚀和剥蚀倾向。两种铝合金暴露在相同大气环境中时,7B50-T7751板材耐蚀性较7B50-T77511型材略好。 展开更多
关键词 7b50铝合金 7b50-t7751 7b50-t77511 大气环境 暴露试验 腐蚀行为
下载PDF
Through-thickness heterogeneity in creep properties of friction stir welding 7B50-T7451 aluminum alloy thick plate joint:Experiments and modeling 被引量:2
6
作者 Huan WANG Weifeng XU Hongjian LU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2023年第6期378-389,共12页
Through-thickness heterogeneity in creep properties of 7B50-T7451 aluminum alloy Friction Stir Welding(FSW)joints was investigated.Creep tests for three slices of the FSW joint were conducted at the temperature of 150... Through-thickness heterogeneity in creep properties of 7B50-T7451 aluminum alloy Friction Stir Welding(FSW)joints was investigated.Creep tests for three slices of the FSW joint were conducted at the temperature of 150-200℃ and applied stress of 60-225 MPa.The theta projection method was used to predict creep curves and minimum creep rate.The results show that the minimum creep rate increases and creep rupture life decreases with the increase of creep temperature and applied stress.Creep properties of the FSW joint deteriorate along the thickness direction from the top to the bottom.The threshold stress of all three slices of the FSW joint decreases with the increase of creep temperature and even disappears at 200℃ for the bottom slice.Creep activation energy approaches the activation energy of the lattice self-diffusion of aluminum.The value of true stress exponent for different slices is approximately equal to three.The predominant creep mechanism of the FSW joint is dislocation viscous glide by lattice self-diffusion.What is more,a constitutive model is established based on the theta method to accurately describe creep behavior ofdifferent slices of the FSW joint. 展开更多
关键词 7b50 high strength aluminum alloy Creep mechanism Creep modeling Friction stir welding Theta projection method Through-thickness heterogeneity
原文传递
Prediction of properties distribution of 7B50 alloy thick plates after quenching and aging by quench factor analysis method 被引量:2
7
作者 Lei Kang Yi-Ran Zhou +2 位作者 Gang Zhao Kun Liu Ni Tian 《Rare Metals》 SCIE EI CAS CSCD 2019年第11期1043-1050,共8页
In the present work,continuous cooling curves were accurately measured by the modified Jominy specimen of 7B50 alloy during water-spray quenching tests.Besides,the time-temperature-properties(TTP) curves of this alloy... In the present work,continuous cooling curves were accurately measured by the modified Jominy specimen of 7B50 alloy during water-spray quenching tests.Besides,the time-temperature-properties(TTP) curves of this alloy were obtained during isothermal treatments.Based on the accurate cooling curves and TTP curves,the hardness distribution along the thickness direction of 7B50 alloy thick plates was predicted by quench factor analysis method.It is found that the quench sensitive temperature range of 7B50 alloy is 240-410℃,the nose temperature is 335℃,and the incubation period at the nose temperature is about 0.87 s.When 7B50 alloy was isothermal treated at 180-400℃ after solid solution treatment(470℃ for 1 h followed by 483℃ for 2 h),the exponent(n) in the Johnson-Mehl-Avrami equation is close to 1 until transformed fraction of new precipitates is up to 60%,indicating that new precipitates first grow into rodlike shape and then coarsen or thicken.When the distance is less than 65 mm from the spray quenching surface of the modified Jominy specimen,the deviation between the predicted and measured hardness is less than 2.7%,confirming the quench factor analysis method as the feasible way to predict the hardness distribution along the thickness direction of 7B50 alloy thick plates.When the distance from the spray quenching surface is 25 mm,the average cooling rate in quench sensitive temperature range is 9.93 ℃·s^-1,while the quench factor(τ) is 9.89 and the corresponding predicted hardness is HV 185.1 equivalent to 97.3% of the maximum measured hardness of 7B50 alloy in T6 temper. 展开更多
关键词 7b50 aluminum alloy QUENCH factor analysis method Time-temperature-properties CURVE Continuous cooling CURVE PROPERTIES PREDICTION
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部