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Effect of thermo-mechanical treatment process on microstructure and mechanical properties of 2A97 Al-Li alloy 被引量:11
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作者 高崇 栾阳 +1 位作者 于俊川 马岳 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2014年第7期2196-2202,共7页
2A97 Al-Li alloy was processed by thermo-mechanical treatment at different pre-stretch deformations of 0, 3% and 6%. The microstrucatre observation results reveal that some δ' and T1 precipitates are found in a(Al... 2A97 Al-Li alloy was processed by thermo-mechanical treatment at different pre-stretch deformations of 0, 3% and 6%. The microstrucatre observation results reveal that some δ' and T1 precipitates are found in a(Al) matrix of 2A97 alloy processed by the heat treatment with no pre-stretch deformation. When the pre-stretch deformation is 3% and 6%, respectively, amounts of tiny T1 and a few of S' precipitates precipitates are observed in the microstructures of 2A97 alloy. The tensile test results show that the tensile properties of 2A97 alloys are improved via thermo-mechanical treatment. When the pre-stretch deformation is from 0, 3% to 6%, the ultimate tensile strength values of the 2A97 alloys increase gradually from 447.7, 516.5 to 534.3 MPa, and the elongations decrease from 17.6%, 12.8% to 10.2%, respectively. Moreover, with increasing pre-stretch deformation amount from 0 to 6%, the in-plane anisotropy value of 2A97 alloys becomes more obvious. 展开更多
关键词 2a97 al-li alloy thermo-mechanical treatment pre-stretch deformation microstructure mechanical properties
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Fatigue crack initiation and early propagation behavior of 2A97 Al-Li alloy 被引量:6
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作者 钟警 钟申 +2 位作者 郑子樵 张海锋 罗先甫 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2014年第2期303-309,共7页
The fatigue crack initiation and early propagation behavior of 2A97 Al-Li alloy was studied. The smooth specimens were fatigued at room temperature under constant maximum stress control when stress ratio (R) is 0.1 ... The fatigue crack initiation and early propagation behavior of 2A97 Al-Li alloy was studied. The smooth specimens were fatigued at room temperature under constant maximum stress control when stress ratio (R) is 0.1 and frequency (f) is 40 Hz. Microstructure observations were examined by optical microscopy, transmission electron microscopy, scanning electron microscopy and electron back scattered diffusion, in order to investigate the relationship between microstructure and fatigue crack initiation and early propagation behavior of 2A97 alloy. The results show that the fatigue cracks are predominantly initiated at inclusions and coarsen secondary phases on the surface of 2A97 alloy. The fatigue crack early propagation behavior of 2A97 alloy is predominantly influenced by the interactions between grain structure and dislocations or persistent slip bands (PSBs). When the misorientation of two neighbouring grains is close to the orientations of the favorable slip plane within these two grains, high-angle grain boundary severely hinders the PSBs passing through, and thus leads to crack bifurcation and deflection. 展开更多
关键词 2a97 al-li alloy fatigue crack initiation fatigue crack early propagation
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TEMPERATURE DEPENDENCE OF PERMEABILITY OF Co_(66)Fe_4Mo_2Si_(16)B_(12) ALLOY 被引量:1
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作者 Y.J. Zhang X.H. Li +1 位作者 S. Wang K.Y. He 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 2007年第4期284-286,共3页
At different annealing temperatures, the saturation magnetostrictions and the correlation between the permeability μi and the temperature T (μi-T curves) of the Co66Fe4Mo2Si16B12 alloy were investigated using a sm... At different annealing temperatures, the saturation magnetostrictions and the correlation between the permeability μi and the temperature T (μi-T curves) of the Co66Fe4Mo2Si16B12 alloy were investigated using a small-angle magnetization tester and core tester. The experimental results showed that the μi-T curves had different shapes at different ranges of annealing temperature; the permeability μi of the alloy improved with the increase of the annealing temperatures below 460℃; when the alloy was annealed above 480℃, the poor magnetic properties were considered to be caused by larger saturation magnetostriction. 展开更多
关键词 Co66Fe4Mo2Si16B12 alloy amorphous nanocrystalline alloy PERMEABILITY saturation magnetostriction
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Behavior of Growth and Coarsening of T_1(Al_2CuLi) Precipitates in Al-Li Alloys 2090 and 2090+Ce
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作者 Zhilong Zhao, Lin Liu, Zheng Chen Dopartment of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China 《Rare Metals》 SCIE EI CAS CSCD 2001年第3期174-177,共4页
The behavior of growth and coarsening of T-1(Al2CuLi) precipitates was comparatively studied by means of TEM technique in two Al-Li alloys 2090 and 2090+Ce (with cerium content less than 0.1% in mass fraction). Statis... The behavior of growth and coarsening of T-1(Al2CuLi) precipitates was comparatively studied by means of TEM technique in two Al-Li alloys 2090 and 2090+Ce (with cerium content less than 0.1% in mass fraction). Statistical analysis results show that T-1 precipitates in alloy 2090+Ce have smaller aspect ratio, which is connected with the more intersections between different T-1 variants in this alloy. It is also found that the variation of maximum length of T-1 precipitates with aging time can be obviously divided into two stages of growth and coarsening. The diffusion coefficients of solute atoms of Cu and Li are calculated via growth kinetics curves of T-1 precipitates. The results show that the diffusion of atom Cu plays a more important role in the formation of T-1 precipitates. 展开更多
关键词 al-li alloy T-1(Al2CuLi) precipitates growth and coarsening trace addition of cerium
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铝锂合金的发展及一种新型铝锂合金-X2A66 被引量:20
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作者 翟彩华 冯朝辉 +3 位作者 柴丽华 陆政 聂祚仁 陈子勇 《材料科学与工程学报》 CAS CSCD 北大核心 2015年第2期302-306,301,共6页
Al-Li合金是一种低密度、高比强度、高比刚度、高弹性模量、抗疲劳性能优良的航空航天材料,具有很好的应用前景。本文综述了Al-Li合金的发展历史,重点介绍了航空材料研究院结合飞机机身壁板整体挤压技术研发的一种新型的Al-Li合金(X2A66... Al-Li合金是一种低密度、高比强度、高比刚度、高弹性模量、抗疲劳性能优良的航空航天材料,具有很好的应用前景。本文综述了Al-Li合金的发展历史,重点介绍了航空材料研究院结合飞机机身壁板整体挤压技术研发的一种新型的Al-Li合金(X2A66)。X2A66合金的整体挤压壁板结构能实现密度减重和结构减重,同时还提高了壁板的密封性。 展开更多
关键词 al-li合金 X2a66 机身壁板
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Texture evolution behavior and anisotropy of 2A97 Al-Li alloy during recrystallization at elevated temperature 被引量:2
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作者 Dong Wang Chong Gao +2 位作者 Hong-Yun Luo Yong-Hong Yang Yue Ma 《Rare Metals》 SCIE EI CAS CSCD 2023年第9期3139-3149,共11页
2A97 Al-Li alloy was cold-rolled to 2 mm and then thermally exposed at different temperatures for 1 h and at 723 K for different time,respectively.The texture evolution behavior and the anisotropy of 2A97 Al-Li alloy ... 2A97 Al-Li alloy was cold-rolled to 2 mm and then thermally exposed at different temperatures for 1 h and at 723 K for different time,respectively.The texture evolution behavior and the anisotropy of 2A97 Al-Li alloy were investigated.The result shows that the{001}<120>and{011}<233>textures are the dominant recrystallization texture.The{124}<211>texture is the final recrystallization texture.In case of low-temperature thermal exposure(473,573 K),the{011}<211>texture is aggregated to the{112}<111>and{123}<634>textures.During the recrystallization at 723 K,the{001}<110>,{111}<112>and{011}<100>textures are the intermediate transition grain orientations.The concurrent precipitation of Al_(20)Cu_(2)Mn_(3)and Al_(3)Zr results in the occurrence of unusually sharp{011}<233>and{001}<120>texture components during recrystallization.The alloy with both recrystallization and deformation texture possesses the smallest anisotropic,and the texture is the direct reason that results in the anisotropy. 展开更多
关键词 al-li alloy 2a97 Crystallographic texture Texture evolution ANISOTROPY
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