Fe－5Ni合金奥氏体高温变形行为

在温度９７３～１３７３Ｋ、形变速率２×１０－５～１．５×１０－１ｓ－１的试验条件下，研究了Ｆｅ－５Ｎ合金奥氏体的高温拉伸变形行为．结果表明：高温变形时峰值应力σｐ与温度Ｔ和形变速ε之间符合下式关系：Ｚ＝εｅｘｐ（Ｑ／ＲＴ）＝Ａ（ｓｉｎｈ（ａσｐ））ｍ。高应变速率区的表观激活能Ｑ为３１４ｋＪ／ｍｏｌ，与Ｆｅ的自扩散激活能Ｑｓｄ相当，变形由空位扩散所控制；而低应变速率区的Ｑ为２０２ｋＪ／ｍｏｌ，约为Ｑｓｄ的２／３，变形由晶界滑移所控制．     

Fe—5Ni合金奥氏体高温变形行为

在温度９７３－１３７３Ｋ，形变速率２×１０＾－５－１．５×１０＾－２ｓ＾－１的试验条件下，研究了Ｆｅ－５Ｎｉ合金奥氏体的高温拉伸变形行为。结果表明：高温变形时峰值应力σｐ与温度Ｔ和形变ε之间符合五式关系：Ｚ＝εｅｘｐ（Ｑ／ＲＴ）＝Ａ（ｓｉｎｈ（ασｐ））＾ｍ。高应变速率区的激活能Ｑ为３１４ｋＪ／ｍｏｌ，与Ｆｅ的自扩散激活能Ｑｓｄ相当，变形由空位扩散所控制；而低应变速率区的Ｑ为２０２ｋＪ／ｍｏｌ，约     

45V钢热变形条件下的动态回复行为

用Ｇｌｅｅｂｌｅ－１５００模拟试验机研究了４５Ｖ钢热变形条件下的动态回复行为。４５Ｖ钢动态回复过程的流变应力σ对应变ε的变化为σ＝〔σ＾２ｓ＋（σ＾２０－σ＾２３）ｅ＾－２Ｂｅ〕＾１／２，位错密度变化率ｄｐ／ｄε＝２Ａ／（αμｂ）＾２－２ＢＰｏ。分析了变形温度和应变速率对动态回复行为的影响。     

纳米晶Fe_(74.7-x)Cu_1Nb_xV_(1.8)Si_(13.5)B_9合金的磁性

本文报道Ｆｅ７４．７－ｘＣｕ１ＮｂｘＶ１．８Ｓｉ１３．５Ｂ９（ｘ＝１，１．５，２）纳米晶软磁合金的综合磁性。ｘ＝２的合金的高频铁损水平为：ｐ３／１００ｋ＝４６８ｋｗ／ｍ３：Ｐ２／２００ｋ＝７０６ｋＷ／ｍ３；Ｐ２／５００Ｋ＝３６２０ｋｗ／ｍ３和Ｐ０．５／１０００ｋ＝８１０ｋｗ／ｍ３优于Ｆｅ－Ｃｕ－Ｎｂ－Ｓｉ－Ｂ类纳米晶合金的水平所考察的三种合金铁损水平都大大优于功率优良的Ｍｎ－Ｚｎ铁氧体Ｈ７Ｃ４考察了起始磁化率的温度关系，观察到原始非晶样品出现两个尖锐的Ｈｏｐｋｉｎｓｏｎ峰，与此不同的是，在具有最佳磁性的样品中只出现第二Ｈｏｐｋｉｎｓｏｎ峰，用Ｔｈｏｍａｓ理论解释了这一现象。观察到高温下纳米α－Ｆｅ（Ｓｉ）晶粒系统的超顺磁行为，起始磁化率的温度关系符合Ｃｕｒｌｅ－Ｗｅｉｓｓ定律。     

NiAl和Ni3Al双相合金的超塑性变形

研究了ＮｉＡｌ和Ｎｉ３Ａｌ双相合金在高温超塑性变形行为．结果表明：该合金在９７５至１０２５℃的温度范围及应变速率为１５２×１０（－４）ｓ（－１）时，表现出超塑性变形行为；１０００℃时最大拉伸延伸率为１４９％，此时对应的应力敏感指数为０．３７５．该合金的超塑性形变可用经验公式ε＝Ａσ（２．６７）ｅｘｐ（－３０３０００／ＲＴ）来表示。对拉伸后试样的金相和ＴＥＭ研究表明，合金中ＮｉＡｌ和Ｎｉ３Ａｌ两相在高温能够较好地协同形变，超塑性是由变形过程中发生的连续回复与再结晶过程来实现的．     

快速凝固（Sm1—xBx）Fe2合金的结构和磁性

采用真空单辊快淬法（铜辊,线速度达２０～２３ｍ／ｓ）将成分为（Ｓｍ１－ｘＢｘ）Ｆｅ２（ｘ＝０,０．０１５,０．０３,０．０４５,０．０６）合金锭,制成快速凝固的鳞片状合金,再经粉碎在３０ＭＰａ压力下,模压成φ１０ｍｍ圆片,然后进行ＸＲＤ分析,比磁化强度和磁致伸缩（λ″－λ┴）的测量。实验结果表明各样品只有少量非晶相,主要是ＳｍＦｅ２及少量的ＳｍＦｅ５和ＳｍＦｅ７化合物。样品（Ｓｍ０．９８５Ｂ０．０１５）Ｆｅ２和（Ｓｍ０．９４Ｂ０．０６）Ｆｅ２,在７２０ｋＡ／ｍ磁场下,比磁化强度分别为：５９．５,５２．３Ａｍ２ｋｇ－１,在８８５ｋＡ／ｍ磁场下（λ″－λ┴）分别为：－５１０×１０－６和－３１０×１０－６。     

氯化物熔体中镱铜中间合金的形成和电解制备

利用线性扫描伏安法研究了Ｙｂ（Ⅲ）在等摩尔ＮａＣｌＫＣｌ熔体中Ｃｕ电极上还原的电化学行为及扩散系数。结果表明：Ｙｂ（Ⅲ）第一步可逆还原为Ｙｂ（Ⅱ）,Ｙｂ（Ⅱ）进一步还原并与Ｃｕ形成合金：Ｙｂ３＋＋ｅ＝Ｙｂ２＋,Ｙｂ２＋＋２ｅ＋ｎＣｕ＝ＹｂＣｕｎ。测定了Ｙｂ（Ⅲ）和Ｙｂ（Ⅱ）在９７３ＫＮａＣｌＫＣｌ熔体中的扩散系数分别为１．５×１０－５和１．０×１０－５ｃｍ２·ｓ－１。用自耗阴极法在１１２３Ｋ,阴极电流密度２０Ａ·ｃｍ－２,ＫＣｌＹｂＣｌ３（３０％）熔体中制取了ＹｂＣｕ合金     

Fe—28Al—5Cr与Fe—28Al—5Cr—0.5Nb—0.1C合金的超塑性变形能力与特征

研究了 Ｆｅ－２８Ａｌ－５Ｃｒ（原子分数）与 Ｆｅ－２８Ａｌ－５Ｃｒ－０．５Ｎｂ－０．１Ｃ合金的高温变形行为,结果表明,在 ８５０ ℃左右,应变速率为 ８．３×１０－４ ｓ－１时,呈现一定的超塑性变形能力,延伸率分别达到 １４５％和 ２５４％;应变速率敏感指数 ｍ分别为 ０．４与 ０．３５;激活能分别为： ２４３ ｋＪ／ｍｏｌ与 ２１８ ｋＪ／ｍｏｌ．在变形过程中,位错堆积形成小角度晶界,并逐渐转变成大角度晶界,使粗大的原始晶粒细化．     

大晶粒Fe_3Al基合金的超塑性

本文研究了大晶粒Ｆｅ_３Ａｌ基合金Ｆｅ—２８Ａｌ—２Ｔｉ合金的高温变形行为。发现该合金在７５０℃到９００℃应变速率为１×１０~（－３）／ｓ时以及在８５０℃一个较宽的应变速率范围内具有超塑性，最佳延伸率可超过５００％。８５０℃不同应变速率下，ｍ值可以从０．２２变化到０．４１金相及ＴＥＭ观察表明变形过程中发生了明显的动态再结晶，并由此导致了大晶粒Ｆｅ_３Ａｌ合金中的超塑性。     

Fe73.5Cu1Nb3Si13.5B9非晶合金的晶化动力学

用差热分析（ＤＴＡ）结合Ｘ射线衍射（ＸＲＤ）,研究了Ｆｅ７３．５Ｃｕ１Ｎｂ３Ｓｉ１３．５Ｂ９非晶合金的晶化动力学。结果表明：温度在０～７００℃范围内,该合金的晶化相为α－Ｆｅ和Ｆｅ２Ｂ;α－Ｆｅ相晶化表观激活能为４５２．３９ＫＪ／ｍｏｌ,Ｆｅ２Ｂ相的晶化表观激活能３９５．２３ＫＪ／ｍｏｌ;两相在晶化初期激活能最小,随晶化量Ｘｃ的增加而迅速境大,在α－Ｆｅ的体积分类为３０％～８０％,Ｆｅ２Ｂ的体积分     

TiC/AZ91D镁基复合材料高温压缩变形行为

利用自发渗透原位合成法制备了不同体积分数的TiC增强AZ91D镁基复合材料,研究了不同压缩应变速率以及不同变形温度下复合材料的热变形行为,计算分析了不同温度下应变速率敏感指数(m)和表观激活能(Q)与TiC含量的关系．结果表明：TiC／AZ91D复合材料压缩流变应力随TiC含量的增加而升高;TiC含量相同时,流变应力随温度升高或初始应变速率减小而降低．m值随变形温度升高而增大;变形温度以及压缩应变速率相同时,m值随TiC含量升高而增大．Q值依赖于温度、应变速率和TiC含量及其分布,不同条件下其高温变形机制有所差异．     

120°模具室温ECAP制备工业纯钛的压缩变形本构关系

在Gleeble-1500热模拟机上对120°模具室温Bc方式ECAP变形8道次制备的平均晶粒尺寸约为200 nm的工业纯钛进行等温变速压缩实验,研究超细晶工业纯钛在变形温度为298~673 K和应变速率为1×10-4~1×100s-1条件下的流变应力行为。结果表明:变形温度和应变速率均对流变应力具有显著影响,峰值应力随变形温度的升高和应变速率的降低而降低;流变应力在变形初期随应变的增加而增大,出现峰值后逐渐趋于平稳,呈现稳态流变特征。采用双曲正弦模型确定了超细晶工业纯钛的变形激活能Q=104.46 kJ/mol和应力指数n=23,建立了相应的变形本构关系。     

SUPERPLASTICITY IN SiCw／ZK60 COMPOSITE

The superplastic deformation behavior of SiCw/ZK60 composite was investigated at temperatures ranging from 573K to 723K and at initial strain rates ranging from 8.3x10-4s-1 to 8.3x10-2s-1. A maximum elongation of 200% with a m-value of 0.35 was obtained at 613K and a initial strain rate of 1.67x 10-2s-1. The apparent activation energy (98kJ/mol) approximates that for grain boundary diffusion (92kJ/mol) in magnesium. It is proposed that the dominant mechanism of superplastic deformation in the present composite is grain boundary sliding accommodated by diffusional transport, besides, interfacial sliding plays an important role in the superplastic deformation.     

汽车用5182铝合金温变形行为及组织

通过单向温拉伸试验以及扫描电镜和透射电镜观察,研究了汽车用5182铝合金板在变形温度为323~573 K,应变速率为0.001~0.1 s-1条件下的流变行为及微观组织。结果表明,在变形温度≥448 K、应变速率.ε=0.001 s-1条件下,5182合金出现明显的峰值应力,而当应变速率0.01~0.1 s-1时,合金的流变应力呈现稳态;当应变速率.ε=0.001 s-1时,随着变形温度的升高,合金单向温拉伸断口由典型的混合型断裂特征演变成典型的韧性断裂特征,合金产生了动态再结晶。     

热力参数对0Cr11Ni2MoV钢高温流变应力的影响

在Gleeble1500热模拟试验机上进行等温热模拟压缩试验,研究了热力参数(变形温度、变形速度和变形程度)对0Cr11Ni2MoVNb钢在变形温度950℃~1100℃、应变速率0.01~10s-1时的高温变形行为的影响。基于数理统计原理,科学分析并回归确定了合金在该温度范围下的变形激活能Q为429.48kJ/mol,应变速率敏感指数m为0.11059,得出了能综合反映热力参数对材料性能影响的本构方程。通过计算相关系数(R)和绝对误差的平均值(AARE)表明该本构有较好的精度,可对0Cr11Ni2MoVNb钢的流变应力进行很好的预测。     

AZ80镁合金热变形流变应力研究

在应变速率为0.001s-1～10s-1,变形温度为200℃～400℃条件下,在Gleeble-3800热模拟机上对AZ80合金的流变应力进行了研究。结果表明,AZ80合金的流变应力强烈地受变形温度的影响,当变形温度低于300℃时,其峰值流变应力呈现幂指数关系;当变形温度高于300℃时,其峰值流变应力呈现指数关系。在该文实验条件下,AZ80合金热变形应力指数n=8.43,热变形激活能Q=165.83kJ/mol。     

High strain rate superplasticity of rolled AZ91 magnesium alloy

The high strain rate superplastic deformation properties and characteristics of a rolled AZ91 magnesium alloy at temperatures ranging from 623 to 698 K（0.67Tm-0.76Tm） and high strain rates ranging from 10^-3 to 1 s^-1 were investigated.The rolled AZ91 magnesium alloy possesses excellent superplasticity with the maximum elongation of 455% at 623 K and a strain rate of 10-3 s-1,and its strain rate sensitivity m is high up to 0.64.The dominant deformation mechanism responsible for the high strain rate superplasticity is still grain boundary sliding（GBS）,and the dislocation creep mechanism is considered as the main accommodation mechanism.     

热力参数对0CrllNi2MOV钢高温流变应力的影响

在G1eeblel1500热模拟试验机上进行等温热模拟压缩试验,研究了热力参数（变形温度、变形速度和变形程度）对0CrllNi2MoVNb钢在变形温度950％～1100℃、应变速率0．01～10s-1时的高温变形行为的影响。基于数理统计原理,科学分析并回归确定了合金在该温度范围下的变形激活能Q为429．48kJ／mol,应变速率敏感指数。为0．11059,得出了能综合反映热力参数对材料性能影响的本构方程。通过计算相关系数（R）和绝对误差的平均（~（AARE）表明该本构有较好的精度,可对0CrllNi2MoVNb钢的流变应力进行很好的预测。     

Influence of thermo hydrogen treatment on hot deformation behavior of Ti600 alloy

Hot compressive deformation of Ti600 alloy after thermo hydrogen treatment (THT) was carried out within hydrogen content range of 0-0.5%, temperature range of 760-920 ℃ and strain rate range of 0.01-10 s-1. The flow stress of Ti600 alloy after THT was obtained under hot deformation condition, and the influence of hydrogen on work-hardening rate (S*), strain energy density (U*), and deformation activation energy (Q) was analysed. The results show that the flow stress of Ti600 alloy decreases remarkably with the increase of hydrogen when the hydrogen content is less than 0.3%. Both S* and U* decrease with the increase of hydrogen when the hydrogen content is less than 0.3%, and when the hydrogen content is more than 0.3%, S* and U* increase with hydrogen addition. The value of Q decreases with the increase of strain at the same hydrogen content. The addition of small quantity of hydrogen leads to an increase of Q at small strain values, and when the strain reaches 0.6, the value of Q decreases gradually with the increase of hydrogen. When the hydrogen content is within the range of 0.1%-0.3%, the flow stress of Ti600 alloy is decreased when being deformed at the temperature range of 760-920 ℃.     

Characteristics of hot tensile deformation and microstructure evolution of twin-roll cast AZ31B magnesium alloys

High temperature tensile properties and microstructure evolutions of twin-roll-cast AZ31B magnesium alloy were investigated over a strain rate range from 10-3 to 1 s-1.It is suggested that the dominant deformation mechanism in the lower strain rate regimes is dislocation creep controlled by grain boundary diffusion at lower temperature and by lattice diffusion at higher temperatures,respectively.Furthermore,dislocation glide and twinning are dominant deformation mechanisms at higher strain-rate.The processing map,the effective diffusion coefficient and activation energy map of the alloy were established.The relations of microstructure evolutions to the transition temperature of dominant diffusion process,the activation energy platform and the occurrence of the full dynamic recrystallization with the maximum peak efficiency were analyzed.It is revealed that the optimum conditions for thermo-mechanical processing of the alloy are at a temperature range from 553 to 593 K,and a strain rate range from 7×10-3 to 2×10-3 s-1.