LOW CYCLE FATIGUE AND DEFORMATION BEHAVIOR IN AN 8090 Al-Li ALLOY

1.IntroductionAl-Liall0ysrepresentanewclass0flightweight,highmodulusandhighstrengtheconomica1structuralmaterials.Theref0re,theseall0ysareespeciallyattractivet0aero-nauticalandaer0spaceindustries.Tensilepr0pertiesandfracturet0ughnessinAl-Liall0ysaswellaseffectofprecipitates0nthemhavebeenextensivelyinvestigated[1w7].Fatiguefracture0fmaterialsacc0untsf0rthemaj0rity0fin-servicefailureinengineeringc0mpo-nents,andl0wcyclefatiguebehaviorisimportantforlifetimepredicti0ninpracticalalloys-Severalresea…     

FATIGUE CRACK PROPAGATION IN Al-Li ALLOY 8090

Fatigue crack growth rates of Al-Li alloy 8090 in air were found to be strongly dependent up-on the aging conditions.The naturally aged and underaged specimens showed the highest re-sistance to the fatigue crack propagation.The fatigue crack growth resistance of the overagedspecimen is the lowest and that of the peakaged specimen in between.As compared to air,3.5% NaCl solution does not change the effect of aging conditions on the fatigue crackgrowth,but causes a decrease of the resistance to the fatigue crack growth under the same ag-ing condition.Both short cracks from notch and physically short cracks showed much higherrates of fatigue crack propagation in comparison with long cracks under the same aging condi-tion and stress intensity level.The growth behavior of the short crack depends on its type.Thegrowth rate of short crack from notch decreases first to a minimum and then increases with in-creasing △K.However,the physically short crack grows at a progressively increasing rate.The effects of aging conditions are explained in terms of the slip planarity of dislocations andthe cyclic slip reversibility.The observed short crack behavior is considered to be dependent onthe crack closure and the local plasticity near the crack tip.     

8090Al—Li合金的疲劳裂纹扩展

研究了8090型Al—Li合?疲劳裂纹扩展行为以及组织结构和环境的影响,结果表明,在空气中,自然时效和欠时效?现出最好的疲劳裂纹扩展阻力,其次是峰时效状态,而过时效状态的疲劳裂纹扩展阻力最低,在3.5%NaCl水溶液中,时效状态对疲劳裂纹扩展行为有着同空气中相同的影响规律,但在同样的时效条件下,在3.5%NaCl水溶液中的疲劳裂纹扩展阻力要比空气中的低,在相同的应力强度因子范围△K作用下,缺口短裂纹和物理短裂纹均表现出比长裂纹高的扩展速率,用位错的平面滑移性和循环滑移可逆性解释了时效的影响,用裂纹的闭合效应和裂纹尖端塑性区尺寸说明了长短裂纹扩展行为的差别。     

Al—Li合金在慢拉伸条件下的形变与断裂行为

研究了Ａｌ－Ｌｉ合金在单向受力状态下的形变特征与断裂行为，测试了不同时效状态合金的慢拉伸裂纹扩展速率与应力强度因子的关系。结果表明，不同时效合金的范性形变机制、微观断裂模式和慢拉伸裂纹扩展阻力不同，它们视微观组织和晶界性态而异，应变局部化是低塑性的根源。     

一种Al-Li-Zn-Zr合金在室温与低温下的反常拉伸断裂行为SCIEI

本文研究了一种Al-Li-Zn-Zr合金从室温到77K范围内的拉伸性能与断裂行为,结果表明,随实验温度的降低,合金的拉伸极限强度与延伸率均提高,屈服强度基本不变;合金在室温时为明显的穿晶断裂,而77K则主要为沿晶断裂形式;断口附近室温及低温下的变形模式基本相同,但室温时断裂主要与平面滑移有关,而低温时平面滑移倾向大大减弱,此时合金的断裂与位错和晶界的交互作用有关。     

极低温度下8090Al—Li合金的力学性能

本文研究了极低温度下8090Al-Li合金的力学性能,发现它在极低温度下的强度、延性和韧性均优于室温下的性能,且均在20K左右达到最大值;时效制度不同仅对其低温下的屈服强度及延伸率产生影响。     

MICROSTRUCTURE AND MECHANICAL PROPERTIES OF 8090 Al-Li ALLOY

The change of mechanical properties of the 8090 Al-Li alloy influenced by aging is attributedto the change of δ′-phase particle size and the precipitation of S′-phase.The δ′-phase mayeasily precipitate and rapidly grow,but the S′-phase can only precipitate with a longer stageof incubation.The precipitation of S′-phase would be promoted by cold working prior to ag-ing.The co-precipitation of δ′- and S′-phase could improve the strength and plastieity of thealloy,for which aging at 190℃.for 20—30 h seems to be optimal.In addition,the precipitatefree zone( PFZ)can form at high angle grain boundary and its width is over 200 nm in peakaging condition.But at sub-grain boundary,the formation of PFZ is difficult.     

Al—Li合金的疲劳性能

研究了8090Al—Li合金在自然和人工时效状态下光滑样品的室温疲劳寿命,以及在100,150和200℃下的高温疲劳性能。结果表明:人工时效的8090合金的疲劳寿命高于自然时效的;在两种时效状态下,与传统的高强Al合金LC4和LY12相比较,Al—Li合金的疲劳寿命均高。人工时效的8090合金随实验温度的升高,疲劳寿命明显降低;自然时效的8090和LY12合金,高温疲劳寿命虽然略有降低,但在200和150℃时分别有所提高。断口观察表明:Al—Li合金的疲劳裂纹均在表面和亚表面的冶金缺陷处萌生;且层状断裂特征比传统的Al合金更加明显。     

MECHANICAL PROPERTIES OF Al-Li ALLOY 8090 AT CRYOGENIC TEMPERATURES

Cryogenic strength,ductility and toughness of AI-Li alloy 8090 were found to be superior tothose at ambient temperature,and up to optima at about 20 K.Different aging regimes mayonly influence on its cryogenic yield strength and elongation.     

8090Al-Li合金晶间腐蚀与剥落腐蚀性能研究

本文研究了8090Al—Li合金的点蚀、晶间腐蚀和剥落腐蚀性能,探讨了热处理制度对耐腐蚀性能的影响。结果表明:Al-2.79Li-1.3Cu-0.7Mg-0.12Zr合金自然时效态抗晶间腐蚀和剥落腐蚀性能最佳,峰时效状态耐腐蚀性能最差,欠时效比过时效略好。显微组织观察表明合金的耐蚀性能与显微组织密切相关,峰时效条件下,粗大T_2相连续分布于晶界上,它的电位比基体电位低因此晶界构成阳极通道,从而使合金耐蚀性能恶化。     

ELECTROCHEMICAL IMPEDANCE SPECTROSCOPY DURING CORROSION PROCESS OF 8090 Al-Li ALLOY IN EXCO SOLUTION

1.IntroductionAl-Li alloys, compared to traditional Al alloys, have more excellent properties, such as lower density, greater elastic modulus and higher specific strength[1,2]. In the near future, they would be widely applied to airplane structures. While, exfoliation, a main kind of localized corrosion, lowers their strength, plasticity and fatigue properties, and also decreases their service life[3, 4]. So investigating their exfoliation would be very important to their application.Usua…     

THRESHOLD OF SHORT FATIGUE CRACK FOR Al-Li ALLOY 8090

Threshold of fatigue for short through cracks for Al-Li alloy 8090 was evaluated to be lowerthan that of long cracks,and to decrease with the shortening of the crack length.The correla-tion among the threshold,crack wake,and crack tip shielding of the short fatigue cracks wasdiscussed.The super demarcation length and lowest theoretical threshold of short through fa-tigue cracks were presented.     

8090Al—Li合金定向凝固界面形态与溶质偏析

本文阐述了定向凝固参数对8090Al-Li合金固液界面形态和溶质偏析行为的影响。结果表明:当下拉速度R<0.13mm/min(温度梯度G_L=130℃/cm)时,可得到平面凝固组织,当R>0.75mm/min(G_L=130℃/cm)时,可获得枝晶组织,且R越大,枝晶越细小。胞晶组织存在范围很窄,元素Cu偏析较严重,杂质元素Fe,Si也有很大偏析,界面形态对溶质偏析行为有显著影响。以粗枝晶凝固时,偏析比较大,凝固组织粗大。     

Ti3Al基合金的拉伸形变和断裂

测试了三种显微组织Ｔｉ３Ａｌ基合金的室、高温拉伸性能；并用ＳＥＭ和ＴＥＭ详细观察样品的形变和断裂特征，结果发现，材料的力学性能与断口和位错组态的变化密切相关，随实验温度升高，强度降低，延性增加；随固溶温度提高，强度增加，延性降低，三种组织室温拉伸均为解理断裂，温度呈现解理与沿晶混合断裂。     

平衡相对8090Al－Li合金力学性能的影响

研究了一种８０９０Ａｌ－Ｌｉ合金中平衡相Ｔ２（Ａｌ６ＣｕＬｉ３）和δ（ＡｌＬｉ）数量变化对合金室温力学性能的影响。结果表明，合金经过双级时效（２１０－３００℃，４ｈ＋回复处理＋１６０℃，１００ｈ）后，Ｔ２相的大量析出会使合金的强度有所降低，塑性有一定程度升高，而δ相的大量析出迅速降低合金的强度，大幅度提高塑性。     

平衡相对8090Al—Li合金力学性能的影响

研究了一种８０９０Ａｌ－Ｌｉ合金中平衡相Ｔ２（Ａｌ６ＣｕＬｉ３）和δ（ＡｌＬｉ）数量变化对合金室温力学性能的影响。结果表明，合金经过双级时效（２１０－３００℃，４ｈ＋回复处理＋１６０℃，１００ｈ）后，Ｔ２相的大量析出会使合金的强度有所降低，塑性有一定程度升高，而δ相的大量析出迅速降低合金的强度，大幅度提高塑性。     

微量Ag对自然时效态Al—Li—Cu—Mg—Zr合金低温拉伸行为的影响

本文研究了两种不同量的Ag的加入对自然时效状态Al-Li-Cu—Mg—Zr合金在290—77K温度范围内的拉伸性能及断裂行为的影响。结果表明,随着实验温度的降低,合金的拉伸性能在153—77K之间明显改善,不含Ag合金的延伸率则基本保持不变;所有合金在室温时的变形与断裂模式基本相同,主要为平面滑移引起的穿晶剪切断裂;但低温下的拉伸行为随Ag的加入而表现出不同的特点,即含Ag合金的变形在低温下趋于均匀,其低温延伸率的改善可归因于此;低温下合金分层及沿晶开裂的倾向增加     

8090Al—Li合金焊缝金属形核机制

８０９０Ａｌ—Ｌｉ合金焊缝凝固组织中除了柱状枝晶和等轴枝晶外，还有一种极细小的等轴非枝晶，它主要分布在熔合区边缘，有时也能呈带状出现在焊缝中部．等轴枝晶与柱状枝晶的结晶核心是平衡态四方Ａｌ_３Ｚｒ粒子，而等轴非枝晶的结晶核心是亚稳态立方Ａｌ_３Ｚｒ粒子．     

INTERFACE MORPHOLOGIES AND SOLUTE SEGREGATION OF Al-Li ALLOY 8090 DURING UNIDIRECTIONAL SOLIDIFICATION

The solid-liquid interface morphology and solute segregation behaviour of AI-Li alloy 8090during unidirectional solidification were studied by the liquid metal quenehing method undervaried processing conditions.When solidification rate,RO.75 mm/min (temper-ature gradient,G_L=130℃/cm),the structure revealed of planar or dendritic interfacerespectively.With the increase of R,the interface morphology becomes cellular from planargradually,within a narrow range.And the greater the R,the,finer the dendrite.Segregationof element Cu and impurity elements Fe and Si are quite severe,the interface morphologymarkedly influences on solute segregation.During solidification at coarse dendrite interface,their segregation ratios are rather great and solidified structure is coarse.     

8090Al—Li合金疲劳短裂纹门槛值的研究

本文研究了8090Al-Li合金穿透疲劳短裂纹的门槛值,测定了不同长度短裂纹的门槛值和裂纹闭合效应,探讨了该合金疲劳短裂纹门槛值、裂纹尾迹和裂尖屏蔽之间的关系,给出了该合金穿透疲劳短裂纹的上界值和理论最低门槛值。