2024－T3铝合金包铝薄板抗疲劳特性DFR截止值的试验研究

用一种新的ＤＦＲ概念比较国产和美国产２０２４－Ｔ３铝合金包铝薄板的抗疲劳特性，试验分析认为，在相同试验条件下，两国产２０２４－Ｔ３包铝薄板抗疲劳特性相当，没有显著差异。     

2024－T3铝合金包铝薄板抗疲劳特性DFR截止值的试验研究EI

用一种新的ＤＦＲ概念比较国产和美国产２０２４－Ｔ３铝合金包铝薄板的抗疲劳特性，试验分析认为，在相同试验条件下，两国产２０２４－Ｔ３包铝薄板抗疲劳特性相当，没有显著差异。     

7060铝合金热处理工艺对气瓶疲劳性能的影响

热处理工艺的选择决定了气瓶的材料性能及使用性能。7060铝合金强度很高,应用于铝合金无缝气瓶表现为疲劳性能较差。经过工艺筛选,可以制定一种既满足气瓶疲劳性能要求且强度较高的热处理工艺,以满足生产需要。经过疲劳试验结果对比,通过过时效工艺将铝瓶的强度控制在极限强度的80%可以满足气瓶的疲劳性能要求,且三级过时效工艺优于双级过时效工艺。     

纤维铝合金层板的研究进展

纤维铝合金层板是由铝合金和纤维增强复合材料组成的一种混杂结构材料,是一种新型的航空结构材料,广泛应用于飞机较为关键的疲劳结构件上.主要介绍了ARALL和GLARE两种纤维铝合金层板的疲劳性能、拉伸性能、抗损伤性能的研究现状,并进一步提出了今后的研究方向和工作重点.     

DZ125定向凝固高温合金在不同状态下的超高周疲劳行为研究

研究了常规热处理和长期时效状态的DZ125定向凝固高温合金在室温和700℃下的超高周疲劳特征及其差异。利用超声疲劳试验机测试了合金的超高周疲劳性能,采用扫描电镜研究了合金的疲劳断口特征,借助电子探针和纳米压痕测量仪分别测试了合金枝晶间和枝晶干的成分和弹性模量。结果表明:两种热处理制度下DZ125合金的枝晶间和枝晶干的弹性模量以及合金元素分配和偏析比差异不大;DZ125合金在700℃下的超高周疲劳性能低于室温,合金在室温下存在明显的频率效应,但在700℃下不存在频率效应;室温和700℃下,合金经过长期时效后的疲劳性能均有所降低,特别在700℃下合金性能降低得更多。室温下,DZ125合金的两种热处理制度的超高周疲劳裂纹均起源于试样的表面;700℃下,两种热处理制度的超高周疲劳裂纹均起源于试样的亚表面。     

铝-铜-镁-银合金的低温时效组织特征

铝-铜-镁-银合金是新型损伤容限型2000系铝合金,是下一代超音速飞机的候选材料。与其他可热处理强化铝合金类似,时效温度的选择对该合金的组织和性能有决定性的影响。主要利用DSC和TEM两种方法研究低温时效对合金时效析出行为的影响。结果表明,时效温度对合金的时效析出行为影响显著,在65℃长时间时效时,合金的析出相为以{100}α为惯析面的G.P.区,无明显特征表明发生Ω相析出;     

室温大气环境下不同时效态2A12合金的疲劳行为

在拉-压疲劳试验机上对室温大气环境下欠时效态、峰时效态、过时效态和自然时效态2A12合金的疲劳行为进行研究,并采用扫描电镜(SEM)分析室温大气环境下不同时效态对疲劳断口形貌的影响.结果表明:在室温大气环境下,四种时效态2A12合金的疲劳断裂循环次数均随着循环应力的减小而明显增加.循环应力水平越低,疲劳寿命提高越明显;各时效态的疲劳断口均为穿晶断口.断口中均出现疲劳条纹、台阶和韧窝,并在较低循环应力下,疲劳条纹出现的区域较多;欠时效态和峰时效态断口上还可观察到轮胎花样.自然时效态表现出最好的疲劳裂纹扩展阻力,其次是欠时效态、峰时效态,过时效态的疲劳裂纹扩展阻力最低.对室温大气环境下各时效态2A12合金疲劳行为进行了讨论.     

晶向对铝合金构件微动疲劳初始起裂的影响研究EI北大核心CSCD

交变荷载作用下铝合金板材及结构组件的微动疲劳问题是飞机安全服役所面临的主要挑战和技术难题,而微动疲劳影响因素辨识是微动疲劳评估及控制的关键。为促进飞机构件微动疲劳评估及控制技术的发展,利用晶体塑性有限元方法和子模型-全局模型耦合技术研究了飞机机身铆钉-平板结构在压、剪交变应力循环作用下裂纹萌生特征,探讨了以晶向表征的材料细观织构分布对铝合金试样微动疲劳的影响。研究发现,晶向分布将对晶体材料的弹性模量和屈服及硬化强度造成明显影响;晶向分布对微动疲劳接触面起裂部位的影响不明显,而对亚表面起裂部位影响比较显著;晶向分布对微动疲劳初始起裂寿命的影响比较明显。研究结果表明,晶向分布这一细观织构影响了晶体材料宏观尺度的弹性强度特征和塑性变形特征,并对金属构件微动疲劳初始起裂寿命、亚表面裂缝发轫位置及扩展特征均造成了影响。基于该研究结论,利用材料加工方法改变金属晶体试样浅表层的晶向分布状态,将可以对微动疲劳裂缝发轫及扩展起到抑制作用。     

T6I6处理对Al-Si-Mg-Cu铸铝时效析出及疲劳行为的影响

利用硬度测试、力学拉伸测试、疲劳测试和透射电镜分析(TEM)等方法研究了T6I6处理对Al-Si-Mg-Cu铸铝时效析出和疲劳行为的影响。研究结果表明:在T6和T6I6峰时效阶段,Al-Si-Mg-Cu铸造铝合金的主要强化相为GP区和β″相,T6I6处理能够明显提高峰时效态合金强化相的密度。与T6峰时效态合金相比,T6I6峰时效态合金的屈服强度和抗拉强度分别提高了7.3 MPa和11.5 MPa,同时延伸率也提高了4.1%。相同加载条件下,T6I6峰时效态合金的疲劳寿命更长,在最大应力为175 MPa时,疲劳寿命提高了63.0%。     

时效制度对7B04铝合金断裂韧性的影响

为研究不同时效制度对7B04铝合金断裂韧性的影响,测定了15种时效工艺的常规力学性能和断裂韧度,并利用扫描电镜对拉伸断口进行分析.通过比较不同时效工艺制度的性能指标和断口形貌,总结出时效制度对7B04铝合金断裂韧度的影响规律.结果表明:随着第二级时效温度的提高和时效时间的延长,7B04铝合金强度下降,断裂韧性提高,其中,温度对性能的影响更大;采用115℃×7 h 185℃×13 h双级时效工艺时,对应的强度和断裂韧度指标均比T73和T76工艺对应的指标高.     

A study of stochastic fatigue crack growth modeling through experimental data

To capture the statistical nature of fatigue crack growth, many stochastic models have been proposed in the literature. These models may have been verified by only one data set, and therefore not appreciated by other fellow researchers. Part of the reason is the difficulty and time-consuming in obtaining the statistically meaningful fatigue crack growth data. In the present study, experimental work is carried out to obtain the fatigue crack growth data of a batch of 2024-T351 aluminum alloy specimens. A rather universal stochastic fatigue crack growth model proposed by Yang and Manning is employed to analyze the data. The solution of the stochastic differential equation associated with the stochastic model gives us the crack exceedance probability as well as the probability of random time to reach a specified crack size. Through comparison between the analytical and experimental results, it is found the model with a minor modification can fit the experimental data rather well. Once the appropriate stochastic model is established, it can be used for the fatigue reliability prediction of structures made of the tested material. In the present study, in particular, it can be used for the reliability assessment of aging aircraft made of 2024-T351 aluminum alloy.     

定量研究2024-T351铝合金搅拌摩擦焊过程中的时效相行为

采用差示扫描量热法研究了2024-T351铝合金搅拌摩擦焊接过程中时效相回溶或粗化的相对值,给出了一种定量研究搅拌摩擦焊接过程中时效相行为的方法.结果表明:相对于母材,焊缝不同区域时效相的回溶或粗化值可通过公式f=Sx/SBM-1来计算;当搅拌摩擦焊搅拌头转速为700r·min-1,焊接速度为200mm·min-1时,...     

金属材料疲劳裂纹扩展曲线的拟合方法研究

提出了一种金属材料疲劳裂纹扩展曲线(a~N曲线)的拟合方法,即修正的双曲函数拟合方法。为检验这种曲线拟合方法的适用性,利用2024-T42铝合金CCT试样的疲劳裂纹扩展试验数据,对该铝合金的疲劳裂纹扩展曲线进行了拟合分析,并给出了疲劳裂纹扩展速率和扩展寿命。通过疲劳裂纹扩展寿命计算结果和试验结果的对比分析,证明这种拟合方法具有较高的拟合精度。     

Enhancement on Fatigue Property of Aluminum Alloy Welded Joint by Utilizing Trailing Peening

The fatigue properties of 2024T3 aluminum alloy welded joint treated by different peening methods were examined. The different effects on fatigue performance of high strength aluminum welded joints were compared with each other by carry out a series tests     

一种新的铝合金应变疲劳计算方法

提出了一种在铝合金构件应变疲劳分析中,计算局部应力和应变变程的新方法。这种方法称作应力功恒等法。采用这种新方法,计算了2024-T42铝合金试件在恒幅循环载荷作用下的疲劳寿命,并将疲劳寿命计算结果与试验结果进行了对比分析。对比分析结果表明,采用这种新方法计算构件应力集中处的局部应力和应变变程,具有较高的计算精度。     

Influence of frequency and exposure to a saline solution on the corrosion fatigue crack growth behavior of the aluminum alloy 2024

The aim of this study is to identify domains where the interactions between mechanical, environmental and microstructural parameters may occur during corrosion fatigue crack growth in the aluminum alloy 2024. The scope considered encompasses the influence of frequency and of alternate immersion in saline solution. Corrosion fatigue crack propagation tests have been carried out under sinusoidal and saw-tooth waveforms, and at different frequencies, load ratios, grain orientations and tempers, in air, distilled water and 3.5% NaCl in permanent and alternate immersion. The stress corrosion cracking behavior of the alloy 2024 has also been considered in order to evaluate the possible contribution of this type of damage during corrosion fatigue crack growth. In 3.5% NaCl, growth rates were found to decrease with decreasing frequency. In alternate immersion, growth rates were increased by up to an order of magnitude for the ΔK values considered compared to permanent immersion and air. The possible mechanisms that govern the corrosion fatigue behavior of the 2024 alloy are discussed in terms of a competition between passivation and anodic dissolution and/or hydrogen embrittlement. Finally, it is proposed that the fatigue crack growth enhancement observed during permanent immersion is related to a crack-tip hydrogen embrittlement mechanism. Hydrogen would be produced by anodic dissolution in relation with film rupture periodicity and then be dragged into the process zone. In alternate immersion, precipitate-free zone dissolution would govern crack advance, as during stress corrosion cracking.     

Variation of the cyclic strain-hardening exponent in advanced aluminium alloys

The cyclic strain-hardening exponents for five fatigue-resistant aluminium alloys were determined throughout the fatigue life to study the degree of cyclic stability of these alloys. Data were compared with results for 2024-T4 aluminum and for two high-pressure steels. The strain-hardening exponent increased logarithmically in all cases except 2024-T4, although the increase was small and did not exceed 33% over the fatigue life. 7475-T351 aluminium alloy was found to be entirely stable, and 7075-T7351 almost so. These were followed in order of rising sensitivity by 2014-T6, 7050-T73651, and 2124-T851 aluminium alloys, and 28NiCrMo7.4 and 30CrNiMo8 steels. 2024-T4 aluminum alloy demonstrated a strong decrease in strain-hardening exponent with fatigue life.     

The effect of pre-stress cycles on fatigue crack growth—an analysis of crack growth mechanism

Cyclic pre-stress increases subsequent fatigue crack growth rate in 2024-T351 aluminum alloy. This increase in growth rate, caused by the pre-stress, and the increased rate, caused by temper embrittlement as observed by Ritchie and Knott, cannot be explained by the crack tip blunting model alone. Each fatigue crack increment consists of two components, a brittle and a ductile component. They are respectively controlled by the ductility of the material and its cyclic yield strength.     

位错对高体积分数SiCP/2024Al时效行为的影响

采用粒径为1μm的SiC颗粒,用挤压铸造法制备出体积分数为45 %的SiC_P/2024Al复合材料,研究了位错对高体积分数SiC_P/2024Al时效行为的影响。结果表明,复合材料中的高密度位错可以湮灭大量的淬火空位,这在一定程度上抑制了GP区的析出。但是,高密度位错的存在降低了其它析出相的热扩散激活能,促进了析出相形核;还能为原子的管道扩散提供通道,促进了溶质原子的扩散,加速析出相的长大,在宏观上表现为对时效行为的促进,使峰时效提前。高密度的位错为强烈依赖于位错等缺陷形核的θ'和S'相提供许多优先形核的场所,使复合材料中的形核密度增加,同时使析出相的尺寸减小,所以复合材料中的析出相呈现细小弥散的分布特点。