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Ballistic behavior of boron carbide reinforced AA7075 aluminium alloy using friction stir processing-An experimental study and analytical approach 被引量:1
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作者 I.SUDHAKAR G.MADHUSUDHAN REDDY K.SRINIVASA RAO 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2016年第1期25-31,共7页
High strength-to-weight ratio of non-ferrous alloys, such as aluminium, magnesium and titanium alloys, are considered to be possible replacement of widely accepted steels in transportation and automobile sectors. Amon... High strength-to-weight ratio of non-ferrous alloys, such as aluminium, magnesium and titanium alloys, are considered to be possible replacement of widely accepted steels in transportation and automobile sectors. Among these alloys, magnesium is self explosive and titanium is costlier, and aluminium is most likely to replace steels. Application of aluminium or its alloys is also thought of as an appropriate replacement in defence field, especially to enhance the easiness in mobility of combat vehicles while maintaining the same standard as that of conventional armour grade steels. Hence most of the investigations have been confined to aluminium or its alloys as base material and open an era of developing the newer composite materials to address the major limitation, i.e. tribological properties. The surface composites can be fabricated by incorporating the ceramic carbides like silicon carbide, carbides of transition metals and oxides of aluminium using surface modification techniques, such as high energy laser melt treatment, high energy electron beam irradiation and thermal spray process which are based on fusion route. These techniques yield the fusion related problems, such as interfacial reaction, pin holes, shrinkage cavities or voids and other casting related defects, and pave the way to need of an efficient technique which must be based on solid state. Recently developed friction stir processing technique was used in the present investigation for surface modification of AA7075 aluminum alloy, which is an alternative to steels. In the present investigation, 160 μm sized boron carbide powder was procured and was reduced to 60 μm and 30 μm using high energy ball mill. Subsequently these powders were used to fabricate the surface composites using friction stir processing.Ballistic performance testing as per the military standard(JIS.0108.01) was carried out. In the present work, an analytical method of predicting the ballistic behavior of surface composites was developed. This method was based on energy balance, i.e., the initial energy of impact is same as that of energy absorbed by multi layers. An attempt also has been made to validate the analytical results with the experimental findings. Variation between the analytical and experimental results may be accounted due to the assumptions considering such as isotropic behavior of target and shearing area of contact as cylindrical instead of conical interface As the analytical model yields the ballistic performance in the closer proximity of experimentally obtained, it can be considered to be an approximation to evaluate the ballistic performance of targets. 展开更多
关键词 AA7075 aluminium alloy Friction stir processing(FSP) Surface metal matrix composite(SMMC) Boron carbide(B4C) Ballistic performance TARGET
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Enhancement of wear and ballistic resistance of armour grade AA7075 aluminium alloy using friction stir processing 被引量:7
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作者 I.SUDHAKAR V.MADHU +1 位作者 G.MADHUSUDHAN REDDY K.SRINIVASA RAO 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2015年第1期10-17,共8页
Industrial applications of aluminium and its alloys are restricted because of their poor tribological properties. Thermal spraying, laser surfacing, electron beam welding are the most widely used techniques to alter t... Industrial applications of aluminium and its alloys are restricted because of their poor tribological properties. Thermal spraying, laser surfacing, electron beam welding are the most widely used techniques to alter the surface morphology of base metal. Preliminary studies reveal that the coating and layering of aluminium alloys with ceramic particles enhance the ballistic resistance. Furthermore, among aluminium alloys,7075 aluminium alloy exhibits high strength which can be compared to that of steels and has profound applications in the designing of lightweight fortification structures and integrated protection systems. Having limitations such as poor bond integrity, formation of detrimental phases and interfacial reaction between reinforcement and substrate using fusion route to deposit hard particles paves the way to adopt friction stir processing for fabricating surface composites using different sizes of boron carbide particles as reinforcement on armour grade 7075 aluminium alloy as matrix in the present investigation. Wear and ballistic tests were carried out to assess the performance of friction stir processed AA7075 alloy. Significant improvement in wear resistance of friction stir processed surface composites is attributed to the change in wear mechanism from abrasion to adhesion. It has also been observed that the surface metal matrix composites have shown better ballistic resistance compared to the substrate AA7075 alloy. Addition of solid lubricant Mo S2 has reduced the depth of penetration of the projectile to half that of base metal AA7075 alloy. For the first time, the friction stir processing technique was successfully used to improve the wear and ballistic resistances of armour grade high strength AA7075 alloy. 展开更多
关键词 Armour GRADE aluminium alloy Friction STIR processing Boron carbide Molybdenum DISULPHIDE WEAR BALLISTIC RESISTANCE
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STUDY ON STRENGTHENING AVIATION ALUMINIUM ALLOY BY LASER SHOCK PROCESSING 被引量:1
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作者 Q.L.Deng1) ,W.D.Huang1) ,Y.H.Zhou1) ,C.Y.Yu2) ,Y.K.Zhang2) , Y.X.Tang2) and H.Zhang2) 1) State Key Lab .of Solidification Processing, Northwestern Polytechnical University ,Xi’an 710072 ,China 2) Mechanical Department,Nanjing University of Aeronautics 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 1999年第4期719-724,共6页
The mechanism oflasershock processing wasanalyzedinthispaper. Westudyexperimentallythelasershock processingon 2024 T62 aviation aluminium alloys. Theexperimental results show thefatiguelife of 2024 T62 aviation alumin... The mechanism oflasershock processing wasanalyzedinthispaper. Westudyexperimentallythelasershock processingon 2024 T62 aviation aluminium alloys. Theexperimental results show thefatiguelife of 2024 T62 aviation aluminium alloysshocked by a laserisimprovedgreatly. 展开更多
关键词 lasershock processING AVIATION aluminium alloy fatiguelife
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Modified constitutive model and workability of 7055 aluminium alloy in hot plastic compression 被引量:15
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作者 ZHANG Tao ZHANG Shao-hang +2 位作者 LI Lei LU Shi-hong GONG Hai 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第11期2930-2942,共13页
To obtain flow behavior and workability of 7055 aluminium alloy during hot deformation,hot compression tests at different temperatures and strain rates are conducted.True stress?strain curves of 7055 aluminium alloy u... To obtain flow behavior and workability of 7055 aluminium alloy during hot deformation,hot compression tests at different temperatures and strain rates are conducted.True stress?strain curves of 7055 aluminium alloy under different conditions are obtained and the flow stress increases with ascending strain rate and descending temperature.For Arrhenius constitutive equation,each material parameter is set as a constant,which will bring forth large error for predicting flow behavior.In this work,material parameters are fitted as a function of temperature or strain rate based on experimental results and a modified constitutive equation is established for more accurate prediction of flow behavior of 7055 aluminium alloy.The effects of temperature and strain rate on power dissipation and instability are analyzed to establish a processing map of 7055 aluminium alloy.The dominant deformation mechanism for microstructure evolution at different deformation conditions can be determined and high efficiency of power dissipation may be achieved from power dissipation map.Meanwhile,proper processing parameters to avoid flow instability can be easily acquired in instability map.According to the processing map,optimized processing parameters of 7055 aluminium alloy are temperature of 673?723 K and strain rate of 0.01?0.4 s^?1,during which its efficiency of power dissipation is over 30%.Finite element method(FEM)is used to obtain optimized parameter in hot rolling process on the basis of processing map. 展开更多
关键词 7055 aluminium alloy flow behavior modified constitutive equation processing map optimized parameters
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Effects of Cu and Mg on thixoformability and mechanical properties of aluminium alloy 2014 被引量:2
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作者 M.A.M.ARIF M.Z.OMAR +1 位作者 Z.SAJURI M.S.SALLEH 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2020年第2期275-287,共13页
Thixoforming is a processing method that deforms metal in a semisolid state.The advantages of this process include the production of parts with good surface finish,fine microstructures and superior mechanical properti... Thixoforming is a processing method that deforms metal in a semisolid state.The advantages of this process include the production of parts with good surface finish,fine microstructures and superior mechanical properties.However,the process mostly produces parts from aluminium cast grades,thereby not fully utilising the true potential of this method.Hence,thermodynamic modelling can be used to formulate alloy compositions that favour this processing method.Here,the effects of reducing copper content and increasing silicon and magnesium contents on the thixoformability of aluminium alloy 2014 were presented.The work consists of both the modelling and experimental validation.Results showed that by increasing Si and decreasing Cu content in the alloy,the solidification interval temperature was decreased and the temperature working window between the stipulated liquid fractions was widened,two of the characteristics favouring the process.A high solid-solution temperature employed resulted in the dissolution of unfavourable Mg2Si compound.An increase in Mg content used also resulted in the formation of the compactπ-Al8FeMg3Si6 phase and the decrease in the amount of the sharp and plate-like structure of theβ-Al5FeSi phase,improving the strength of the modified alloy.Subsequent T6 heat treatment successfully further increased the strength of the modified alloy. 展开更多
关键词 JMatPro wrought 2014 aluminium alloy thixoformability semisolid processing mechanical properties
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Nickel-Phosphorus Deposition on Pretreated Aluminium Alloys during Immersion in Electroless Nickel Bath
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作者 Chike F. Oduoza Enam Khan 《材料科学与工程(中英文A版)》 2011年第4X期457-471,共15页
关键词 化学镀镍磷 预处理过程 浸泡时间 镍沉积 铝合金 X射线光电子能谱 扫描电子显微镜 氧化还原反应
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Microstructural evolution during semisolid state strain induced melt activation process of aluminum 7075 alloy 被引量:17
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作者 A.BOLOURI M.SHAHMIRI E.N.H.CHESHMEH 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2010年第9期1663-1671,共9页
The effects of compression ratio on the microstructure evolution of semisolid 7075 Al alloy produced by the strain induced melt activation (SIMA) process were investigated. The samples were cold deformed by compress... The effects of compression ratio on the microstructure evolution of semisolid 7075 Al alloy produced by the strain induced melt activation (SIMA) process were investigated. The samples were cold deformed by compression into the different heights up to 40% reduction. The isothermal holding treatments were carried out at 625 ℃ for predetermined time intervals. The results reveal that the average grain size is gradually reduced with the increase of the compression ratio. When the compression ratio surpasses 30%, the above descending trend is not as evident as that below 30% reduction. During the subsequent heat treatments, the recrystallization is induced in the deformed samples by the increasingly accumulated strain energy. The grain growth mechanisms and the microstructural coarsening of the SIMA processed 7075 Al alloy were discussed and confirmed. 展开更多
关键词 THIXOFORMING thermomechanical processing aluminium alloys semi-solid metal
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Effect of processing routes on microstructure and mechanical properties of 2014 Al alloy processed by equal channel angular pressing 被引量:7
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作者 P.VENKATACHALAM S.RAMESH KUMAR +2 位作者 B.RAVISANKAR V.THOMAS PAUL M.VIJAYALAKSHMI 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2010年第10期1822-1828,共7页
Al-Cu alloy was deformed through equal channel angular pressing(ECAP) by routes A,Ba,Bc and C up to 5 passes.ECAP was done using a 90° die for three different conditions,namely 1) as received,2) solutionised at 7... Al-Cu alloy was deformed through equal channel angular pressing(ECAP) by routes A,Ba,Bc and C up to 5 passes.ECAP was done using a 90° die for three different conditions,namely 1) as received,2) solutionised at 768 K for 1 h and 3) solutionised at 768 K for 1 h + aged at 468 K for 5 h.The microstructure,microhardness and tensile strength were studied for all the three conditions and four routes.Significant improvement in hardness(HV 184 after five passes) and strength(602 MPa after three passes) was observed in solutionised and aged 2014 Al alloy deformed through route Bc.Microstructure evolution was reasonably equiaxed in route Bc with aspect ratio of 1.6.Solutionised and aged 2014 Al alloy deformed through route Bc was identified to have better microstructure and mechanical property than the other processing routes and conditions. 展开更多
关键词 ECAP processing route 2014 aluminium alloy
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Effects of processing parameters on corrosion properties of dissimilar friction stir welds of aluminium and copper 被引量:4
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作者 Esther T.AKINLABI Anthony ANDREWS Stephen A.AKINLABI 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2014年第5期1323-1330,共8页
The influence of friction stir welding processing parameters on dissimilar joints conducted between aluminium alloy (AA5754) and commercially pure copper (C11000) was studied. The welds were produced by varying th... The influence of friction stir welding processing parameters on dissimilar joints conducted between aluminium alloy (AA5754) and commercially pure copper (C11000) was studied. The welds were produced by varying the rotational speed from 600 to 1200 r/min and the feed rate from 50 to 300 mm/min. The resulting microstructure and the corrosion properties of the welds produced were studied. It was found that the joint interfacial regions of the welds were characterized by interlayers of aluminium and copper. The corrosion tests revealed that the corrosion resistance of the welds was improved as the rotational speed was increased. The corrosion rates of the welds compared to the base metals were improved compared with Cu and decreased slightly compared with the aluminium alloy. The lowest corrosion rate was obtained at welds produced at rotational speed of 950 r/min and feed rate of 300 mm/min which corresponds to a weld produced at a low heat input. 展开更多
关键词 aluminium alloy COPPER CORROSION friction stir weld processing parameters
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Impact strength and structural refinement of A380 aluminum alloy produced through gas-induced semi-solid process and Sr addition 被引量:1
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作者 M.HONARMAND M.SALEHI +1 位作者 S.G.SHABESTARI H.SAGHAFIAN 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2022年第5期1405-1415,共11页
Semi-solid processing of A380 aluminum alloy was performed by gas induced semi-solid(GISS)process.The effects of argon inert gas flow rate,starting temperature and duration of gas purging as key GISS parameters and al... Semi-solid processing of A380 aluminum alloy was performed by gas induced semi-solid(GISS)process.The effects of argon inert gas flow rate,starting temperature and duration of gas purging as key GISS parameters and also modification with Sr on the structural refinements,hardness and impact strength of GISS alloys were investigated.Microstructural evolution shows that there is an important effect of the pouring temperature and Sr addition on the morphology and size of primaryα(A1)in the alloy to change from coarse dendritic to fine globular structure.The best sample which has fine grains of 51.18μm in average size and a high level of globularity of 0.89 is achieved from a GISS processing of Sr modified alloy in which the gas purging started at 610℃.The impact strength of the GISS optimized samples((4.67±0.18)J/cm^(2))shows an increase of about 40%with respect to the as-cast sample due to the globular structure and fibrous Si morphology.Moreover,the hardness of the optimized GISS sample((89.34±2.85)HB)increases to(93.84±3.14)HB by modification with the Sr and GISS process.The fracture surface of Sr modified alloy is also dominated by complex topography showing typical ductile fracture features. 展开更多
关键词 gas-induced semi-solid process impact strength A380 aluminium alloy globular structure modification
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Effect of Gas Bubbling Filtration Treatment on Microporosity Variation in A356 Aluminium Alloy
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作者 Choongdo Lee Taeil So Kwangseon Shin 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 2016年第7期638-646,共9页
In the present study, the contribution of the gas bubbling filtration (GBF) process to the microporosity variation, microstructural characteristics and tensile properties of A356 aluminium alloy was investigated. Th... In the present study, the contribution of the gas bubbling filtration (GBF) process to the microporosity variation, microstructural characteristics and tensile properties of A356 aluminium alloy was investigated. The test specimens were fabricated through gravity casting in terms of the process variables: the degassing time, the impeller rotation and the aperture size of gas inlet hole. The density measurement and scanning electron microscope fractography analyses were conducted to evaluate the variation of the volumetric porosity and fractographic porosity with the GBF process, respec- tively. The fractographic porosity of the specimens can be minimised under specific GBF conditions in terms of the buoyant velocity and the absorbing capacity of gas bubbles, the inclusion of oxide films, whereas the volumetric porosity can be wholly reduced on the lapse of degassing time. The ultimate tensile strength (UTS) and elongation at optimal conditions were improved to approximately 30 MPa and 1.5% compared with no GBF treatment. Even though an extension of the degassing time and/or excessive stirring action of the melt may induce the inclusion of bifilm oxides and the increase of fractographic porosity, the tensile properties of over-treated specimens were maintained to a level which is similar to those that did not undergo GBF treatment due to the grain refinement accompanying with the GBF process. In addition, the defect susceptibility of UTS and elongation to microporosity variation could be remarkably improved at an optimal GBF condition. 展开更多
关键词 aluminium alloy MICROPOROSITY Gas bubbling filtration process (GBF) Tensile property
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Friction stir surfacing of cast A356 aluminiumesilicon alloy with boron carbide and molybdenum disulphide powders 被引量:2
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作者 R.SRINIVASU A.SAMBASIVA RAO +1 位作者 G.MADHUSUDHAN REDDY K.SRINIVASA RAO 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2015年第2期140-146,共7页
Good castability and high strength properties of Ale Si alloys are useful in defence applications like torpedoes,manufacture of Missile bodies,and parts of automobile such as engine cylinders and pistons.Poor wear res... Good castability and high strength properties of Ale Si alloys are useful in defence applications like torpedoes,manufacture of Missile bodies,and parts of automobile such as engine cylinders and pistons.Poor wear resistance of the alloys is major limitation for their use.Friction stir processing(FSP) is a recognized surfacing technique as it overcomes the problems of fusion route surface modification methods.Keeping in view of the requirement of improving wear resistance of cast aluminiumesilicon alloy,friction stir processing was attempted for surface modification with boron carbide(B4C) and molybdenum disulfide(Mo S2) powders.Metallography,micro compositional analysis,hardness and pin-on-disc wear testing were used for characterizing the surface composite coating.Microscopic study revealed breaking of coarse silicon needles and uniformly distributed carbides in the A356 alloy matrix after FSP.Improvement and uniformity in hardness was obtained in surface composite layer.Higher wear resistance was achieved in friction stir processed coating with carbide powders.Addition of solid lubricant Mo S2 powder was found to improve wear resistance of the base metal significantly. 展开更多
关键词 A356合金 二硫化钼 堆焊技术 硅合金 钼粉末 碳化硼 摩擦 铸铝
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单点渐进成形工艺参数对铝合金圆锥台表面粗糙度的影响
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作者 刘长喜 姜旭 +3 位作者 孙建华 毕凤阳 王晓宏 解凯 《黑龙江工程学院学报》 CAS 2024年第2期7-11,22,共6页
表面粗糙度是影响渐进成形零件质量的关键因素之一,为了探究工艺参数对零件表面粗糙度的影响,采用单点渐进成形技术对5052铝合金板料进行成形实验,研究工艺参数轴向进给量、主轴转速、进给速度对圆锥台表面质量的影响,并使用粗糙度仪测... 表面粗糙度是影响渐进成形零件质量的关键因素之一,为了探究工艺参数对零件表面粗糙度的影响,采用单点渐进成形技术对5052铝合金板料进行成形实验,研究工艺参数轴向进给量、主轴转速、进给速度对圆锥台表面质量的影响,并使用粗糙度仪测量外表面粗糙度R_(a)值。实验结果表明:降低轴向进给量可以改善零件表面质量;随着主轴转速增大,零件粗糙度R_(a)呈先减小后增大趋势;进给速度对粗糙度R_(a)影响较小,随着进给速度增大,粗糙度R_(a)呈先减小后增大趋势,受零件尺寸限制,进给速度超过2817 mm·min^(-1)时,内表面“鱼鳞纹”和粗糙度R_(a)几乎没有变化。 展开更多
关键词 渐进成形 铝合金 粗糙度 圆锥台 工艺参数
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基于热处理工艺的拖拉机发动机铝合金组织性能研究
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作者 汤金金 李好娜 《农机化研究》 北大核心 2025年第1期243-247,共5页
采用不同时长的热处理工艺,对拖拉机发动机铝合金组织性能进行了对比分析。结果表明:热处理后,铝合金性能得到了较大程度的提高,若优先考虑材料性能,则应该采用180℃×4 h的单级热处理时效;若优先考虑工艺效率和成本,则可以采用150... 采用不同时长的热处理工艺,对拖拉机发动机铝合金组织性能进行了对比分析。结果表明:热处理后,铝合金性能得到了较大程度的提高,若优先考虑材料性能,则应该采用180℃×4 h的单级热处理时效;若优先考虑工艺效率和成本,则可以采用150℃×1 h+170℃×1 h的双级热处理时效。 展开更多
关键词 热处理工艺 拖拉机 发动机 铝合金 组织性能
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微弧氧化处理对6061铝合金电偶腐蚀防护 被引量:1
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作者 李鹏飞 郭泉忠 +2 位作者 王勇 左晓姣 汪川 《装备环境工程》 CAS 2024年第5期121-131,共11页
目的提高船舶上铝合金的耐蚀性能。方法使用双极性脉冲电源对6061铝合金进行微弧氧化处理,并使用环氧树脂进行封孔,通过电化学测试、扫描电子显微镜(SEM)、能谱仪(EDS)、浸泡腐蚀试验和电偶腐蚀试验等方法,对膜层的表面形貌、截面形貌... 目的提高船舶上铝合金的耐蚀性能。方法使用双极性脉冲电源对6061铝合金进行微弧氧化处理,并使用环氧树脂进行封孔,通过电化学测试、扫描电子显微镜(SEM)、能谱仪(EDS)、浸泡腐蚀试验和电偶腐蚀试验等方法,对膜层的表面形貌、截面形貌、物相组成和耐蚀性能进行测试。结果制备的6061铝合金微弧氧化膜层厚度约为40μm,致密均匀。在240h浸泡试验后,仍具有较强的耐蚀性,与316L不锈钢耦合的电流密度从约47μA/cm^(2)下降到20μA/cm^(2)左右,对6061铝合金的耐蚀性有显著提升。封孔处理后,浸泡腐蚀240h,未发现明显腐蚀,电偶电流进一步下降到11μA/cm^(2)。结论对6061铝合金进行微弧氧化处理,可以有效提高其耐蚀性能,对电偶腐蚀有较好的抑制作用,封孔处理则可以进一步提高铝合金的耐蚀性能。 展开更多
关键词 铝合金 微弧氧化 封孔 电化学 电偶腐蚀 腐蚀过程
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6082-T1铝合金的热变形行为及组织演变
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作者 钱成 张庆彪 +2 位作者 单强超 李祖来 肖寒 《塑性工程学报》 CAS CSCD 北大核心 2024年第10期148-158,共11页
为了深入探究6082-T1铝合金热变形的微观机制,如动态再结晶过程的微观机制、晶粒细化行为以及其对最终材料性能的影响,采用Gleeble-1500热模拟试验机对6082-T1铝合金进行热压缩试验,研究了合金在变形温度420~510℃,应变速率0.1~10 s^(-1... 为了深入探究6082-T1铝合金热变形的微观机制,如动态再结晶过程的微观机制、晶粒细化行为以及其对最终材料性能的影响,采用Gleeble-1500热模拟试验机对6082-T1铝合金进行热压缩试验,研究了合金在变形温度420~510℃,应变速率0.1~10 s^(-1)条件下的热变形行为,基于Arrhenius双曲正弦本构关系建立本构方程,基于动态材料模型建立了热加工图,并研究了微观组织演变规律。结果表明,6082-T1铝合金在合适变形温度区间中,随着温度升高,小角度晶界逐渐转变为大角度晶界,为再结晶提供形核场所,从而增加再结晶晶粒的含量,再结晶的形核和长大消除了合金的晶格畸变,晶粒取向更有利于滑移,从而导致变形抗力减小。 展开更多
关键词 6082-T1铝合金 本构方程 热加工图 组织演变
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5052铝合金板材渐进成形工艺参数双目标优化及试验验证
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作者 姜旭 朱冠昱 +2 位作者 王晓宏 谢文强 姚永涛 《铝加工》 CAS 2024年第5期43-48,共6页
针对金属板材单点渐进成形工艺,选用具有较强成形性能的5052铝合金板材进行研究。基于Abaqus建立单点渐进成形有限元模型,以工具头直径、轴向进给量、板材初始厚度为研究变量,成形后圆锥台结构的最大Mises应力和最大减薄率为优化目标,... 针对金属板材单点渐进成形工艺,选用具有较强成形性能的5052铝合金板材进行研究。基于Abaqus建立单点渐进成形有限元模型,以工具头直径、轴向进给量、板材初始厚度为研究变量,成形后圆锥台结构的最大Mises应力和最大减薄率为优化目标,设计了正交试验,并对每组参数进行模拟分析,采用田口分析和方差分析对工艺参数进行优化。优化结果表明,轴向进给量和板材初始厚度是对最大Mises应力影响的显著项,最终的优化工艺参数组合为工具头直径8 mm、轴向进给量0.5 mm、板材初始厚度0.5 mm,该工艺参数分析的圆锥台结构最大Mises为213.35 MPa,最大减薄率为38.32%。通过单点渐进成形试验进行验证,成形后的圆锥台结构表面质量较好,这也表明该工艺参数组合具备实际应用的可行性。 展开更多
关键词 5052铝合金 渐进成形 有限元 工艺参数 田口法
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AA7075-T6铝合金电阻点焊工艺参数优化研究
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作者 邱飒蔚 蒋家传 +3 位作者 叶拓 张越 雷贝 王涛 《材料导报》 EI CAS CSCD 北大核心 2024年第17期254-261,共8页
轻量化结构设计在保证了结构强度的前提下降低了整车质量,减少了能量消耗,成为汽车工业和航空航天的研究重点。本工作通过建立正交实验获取AA7075-T6铝合金的最佳焊接工艺参数。对接头进行拉伸剪切实验、金相观察和显微硬度测试,并对最... 轻量化结构设计在保证了结构强度的前提下降低了整车质量,减少了能量消耗,成为汽车工业和航空航天的研究重点。本工作通过建立正交实验获取AA7075-T6铝合金的最佳焊接工艺参数。对接头进行拉伸剪切实验、金相观察和显微硬度测试,并对最优参数组合进行数值模拟,以研究焊接工艺参数对接头质量的影响。结果表明:当焊接时间为60 ms、焊接电流为17 kA、电极压力为0.22 MPa时,点焊接头的综合力学性能最好;焊接参数对电阻点焊接头力学性能的影响顺序为焊接时间>焊接电流>电极压力。焊接过程数值模拟得到的熔核尺寸与实验结果一致。焊接过程发生飞溅和熔核存在缩孔缺陷,导致接头的力学性能较差,失效模式为界面断裂。由于焊接过程接头显微组织发生变化,接头显微硬度变化呈“W”形。 展开更多
关键词 AA7075-T6铝合金 电阻点焊(RSW) 工艺参数 显微硬度 数值模拟
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Effects of pre-deformation on microstructure and tensile properties of Al-Zn-Mg-Cu alloy produced by modified strain induced melt activation 被引量:1
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作者 Behzad Mohasel AFSHARI Seyed Sajad MIRJAVADI +4 位作者 Yousef Askari DOLATABAD Mojtaba AGHAJANI Mohammad Kazem Besharati GIVI Mohammad ALIPOUR M.EMAMY 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2016年第9期2283-2295,共13页
The effects of Al-8B grain refiner on microstructure and tensile properties of an Al-12Zn-3Mg-2.5Cu alloy produced by modified strain induced melt activation process were investigated. Pre-deformation of 60% was used ... The effects of Al-8B grain refiner on microstructure and tensile properties of an Al-12Zn-3Mg-2.5Cu alloy produced by modified strain induced melt activation process were investigated. Pre-deformation of 60% was used by hot working at 300 ℃. After pre-deformation, the samples were heated to a temperature above the solidus and below the liquidus point and maintained in the isothermal conditions at three different temperatures(500, 550 and 590 ℃) for varying time(10, 20 and 40 min). It was observed that strain induced melt activation has caused the globular morphology of α(Al) grains. Microstructural study was carried out on the alloy by using optical microscope and scanning electron microscope in both unrefined and B-refined conditions. The results showed that for the desired microstructures of the alloy during SIMA process, the optimum temperature and time are 550 ℃ and 10 min, respectively. After the T6 heat treatment, the average tensile strengths increased from 278 to 585 MPa and 252 to 560 MPa for samples refined with 3.75% Al-8B before and after SIMA process, respectively. The ultimate strength of SIMA specimens is lower than that of B-refined specimens. 展开更多
关键词 aluminium alloy CASTING grain refinement strain induced melt activation semisolid processing tensile properties
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常用航天铝合金热渐进成形极限的研究进展
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作者 李治兵 安治国 +7 位作者 孙鹏飞 林翰 乔正阳 任重 李江 邹政 高正源 李正芳 《航天制造技术》 2024年第5期1-8,23,共9页
铝合金因其轻质、高强、良好的加工性能以及优异的耐腐蚀性,在航天领域得到了广泛的应用。随着科技的进步和航天技术的发展,对铝合金材料的性能要求越来越高,促使铝合金材料不断向高性能、轻量化的方向发展。热渐进成形作为一种先进的... 铝合金因其轻质、高强、良好的加工性能以及优异的耐腐蚀性,在航天领域得到了广泛的应用。随着科技的进步和航天技术的发展,对铝合金材料的性能要求越来越高,促使铝合金材料不断向高性能、轻量化的方向发展。热渐进成形作为一种先进的板料成形技术,为航天用铝合金零件的制造提供了新的解决方案,并获得了当今学者的广泛关注。根据渐进成形加热方式不同,总结了近年来典型的加热方法为电加热、激光加热、电磁感应加热。在此基础上,综述了铝合金热渐进成形极限方面的研究,并总结了多种工艺参数对材料成形极限的影响规律。 展开更多
关键词 热渐进成形 加热方法 铝合金 成形极限 工艺参数
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