Cr/Mo比对FeCoMoCrZr非晶合金晶化过程及磁性能的影响

采用单辊急冷法制备了一系列不同Cr/Mo比的FeCoMoCrZr非晶薄带,并对该系非晶合金进行等温热处理。用XRD和VSM研究Cr/Mo比的变化对(Fe0.58Co0.42)73Mo17-xCrxZr10系非晶合金晶化过程和磁性能的影响。结果表明,x在9~17之间变化时,所制备的合金薄带为非晶结构;(Fe0.58Co0.42)73Mo5Cr12Zr10非晶合金的晶化过程为:Am→α-Fe(Co)+CrFe4+Fe23Zr6+Cr2Mo,(Fe0.58Co0.42)73Cr17Zr10非晶合金的晶化过程为:Am→α-Fe(Co)+Am′→α-Fe(Co)+CrFe4+Fe3Ni2+未知相;Cr/Mo比例的增加降低了合金的热稳定性,促进了退火后α-Fe(Co)相的析出。两种合金的饱和磁化强度Ms随退火温度的变化趋势相同但幅度不同,在低于晶化峰值温度Tp退火,(Fe0.58Co0.42)73Mo5Cr12Zr10合金的Ms随退火温度的升高缓慢上升;而(Fe0.58Co0.42)73Cr17Zr10合金的Ms随退火温度的升高快速大幅上升。     

全金属组元铁基块体非晶的制备与性能研究

为了获得良好的玻璃形成能力,通常在铁基非晶合金中添加类金属元素(P、C、B、Si等),但这些铁基非晶合金大多室温塑性很差,且其脆性与其类金属元素的种类、含量以及分布有密切关系,因而本文选取全金属组元铁基非晶合金(Fe_(0.52)Co_(0.3)Ni_(0.18))_(73)Cr_(17)Zr_(10),通过旋淬甩带与铜模喷铸的方法分别制备了条带与块体试样,并采用X射线衍射仪(XRD)、差示扫描量热仪(DSC)、万能试验机等进行了相关性能研究.研究表明:(Fe_(0.52)Co_(0.3)Ni_(0.18))_(73)Cr_(17)Zr_(10)的临界尺寸在1～2 mm,玻璃转变温度为482℃,过冷液相区达到70℃;直径为1 mm的非晶棒材的屈服强度为2 190 MPa,断裂强度达到2 800 MPa,塑性应变量为3.6%.全金属成分中更多的金属-金属键合方式可能是其拥有较好塑性的原因.     

Fe78Co2Zr8Nb2B10-xGex（x=1,2,3）合金的晶化过程和磁性能研究

采用单辊快淬法制备Fe78Co2Zr8Nb2B10-xGex(x=1,2,3)系非晶合金,在不同热处理条件下对两种合金进行热处理。利用X射线衍射仪(XRD)、透射电镜(TEM)和振动样品磁强计(VSM)等测试手段对合金的微观结构和磁性能进行研究。研究结果表明,3种合金的晶化过程相似:非晶→非晶+α-Fe(Co)→α-Fe(Co)+Fe3Zr+Fe2B。3种合金的比饱和磁化强度(Ms)大体上随退火温度的升高而增大;3种合金的矫顽力(Hc)随退火温度的升高均呈现先增加、后降低、再增加的复杂变化趋势。     

Co基非晶态Fe_(5.3)Co_(61.3)Ni_(7.4)Si_(10)B_(16)及Fe_5Co_(58)Ni_(11)Si_(10)B_(16)合金的磁场热处理效应

本文对Co基非晶Fe_(5.3)Co_(61.3)Ni_(7.4)Si_(10)B_(16)及Fe_(5)Co_(58)Ni_(11)Si_(10)B_(16)合金用不同方法进行了热处理后得出:退火使合金磁性恶化,纵向磁退火有效地消除了应力,局部感生各向异性和畴壁钉扎,形成感生单轴各向异性,静态磁性获得显著提高。Fe_(5.3)Co_(61.3)Ni_(7.4)Si_(10)B_(16)合金最好静态磁性μ_m高达169×10~4Gs/Oe,Hc为4.3mOe,μ_(0.002)为94000G/0e,Br/Bs=0.895,磁滞损耗减小。但由于形成粗大180°畴使反常涡流损耗增加。倾斜磁场退火使180°畴数目增多,在一定频段内有效的降低反常涡流损耗。对提高初始导磁率有一定作用。     

Y元素的添加对Zr_(56)Co_(28)Al_(16)非晶合金在模拟体液中耐蚀性能的影响

采用铜模吸铸法制备了(Zr_(56)Co_(28)Al_(16))_(100-x_Y_x(x=0,1,2,4)非晶合金,研究了(Zr_(56)Co_(28)Al_(16))_(100-x)Y_x(x=0,1,2,4)非晶合金在模拟体液(PBS溶液)中的耐蚀性。运用X射线衍射(XRD)表征试样的结构,运用电化学工作站、场发射扫描电镜(SEM)和X射线光电子能谱(XPS)研究Y元素的添加对Zr_(56)Co_(28)Al_(16)非晶合金耐蚀性的影响。结果表明,适量Y元素的添加显著提高了Zr_(56)Co_(28)Al_(16)非晶合金的耐蚀性,但过量Y元素的添加,在非晶基体上有晶体相的析出,降低了Zr_(56)Co_(28)Al_(16)的耐蚀性能。     

Fe_(63)Ni_1Al_5Ga_2P_(9.65)B_(4.6)Si_3C_(6.75)Co_5非晶合金的晶化行为研究

采用XRD、DSC检测技术,采用连续升温晶化和等温退火晶化方法,研究分析了Fe63Ni1Al5-Ga2P9.65B4.6Si3C6.75Co5非晶薄带的晶化动力学行为和晶化过程中晶化相的析出过程。结果表明,该非晶合金的玻璃转变和晶化行为均具有显著的动力学特征。Kissinger法计算得到的Eg、Ex、Ep1、Ep2分别为750、340、432、689kJ/mol,Eg Ex,表明合金具有较好的热稳定性。合金晶化过程为:非晶→非晶+α-Fe→非晶+α-Fe+Fe2P+Fe3P→α-Fe+Fe2P+Fe3P+Fe3C(Al,Si)+Fe5PB2+SiC。合金的晶化类型为初晶型和随后的共晶型反应。     

Ni_(68)B_(21)Si_(11)三维金属玻璃的热稳定性

采用 Perkin-Elmer DSC7型差示扫描量热仪对深过冷快淬法制取的 Ni_(68)B_(21)Si_(11)三维金属玻璃进行等温、变温热分析,从液态合金的净化,非晶合金的预退火处理及冷却速率三个方面考察了 Ni_(68)B_(21)Si_(11)非晶合金的热稳定性。研究发现:由于大幅度地消除了合金内的预存晶核,深过冷快淬法形成的非晶合金的热稳定性显著提高,此法获得的 Ni_(68)B_(21)Si_(11)非晶合金在400K 下预期寿命提高了一个数量级;非晶合金的预退火处理将导致初始晶化温度 T_λ 和晶化热ΔH 下降;冷却速率对热稳定性影响较小。     

Fe_(64.7)Co_6Cr_(2.3)Mo_(2.5)B_(5.5)C_7Si_(3.3)P_(8.7)块体非晶合金的磁致伸缩特性

采用铜模吸铸法制备了直径2mm的Fe_(64.7)Co_6Cr_(2.3)Mo_(2.5)B_(5.5)C_7Si_(3.3)P_(8.7)块体非晶合金,其玻璃转变温度T_g、超冷液相区间ΔTx(=T_(x1)-T_g)、约化玻璃转变温度T_(rg)(=T_g/Tl)和玻璃形成能力参数γ(=T_(x1)/(T_g+Tl))分别为754,25K、0.595和0.3855。利用真空热处理炉分别在733K(T_g)、768K(T_g和T_(x1)之间)和803K(T_(x1))温度对块体非晶合金进行了等温退火,采用自制的电容法磁致伸缩测量装置测试了不同退火状态下的磁致伸缩特性,显示该非晶合金淬态下饱和磁致伸缩系数λ_s为9×10~(-6),随着退火温度的升高λ_s出现了先增后减的变化,磁致伸缩曲线形状也发生先变窄后变宽的变化。在733K退火样品的软磁性能最好,饱和磁致伸缩系数λ_s(=12×10~(-6))最高。     

非晶软磁合金Co_(65)Fe_4Ni_2Si_(15)B_(14)的纳米晶化动力学研究

采用差示扫描量热分析(DSC)和X射线衍射技术(XRD)研究了非晶态合金Co_(65)Fe_4Ni_2Si_(15)B_(14)的非等温晶化动力学.结果表明,初始晶化的晶化峰值温度T_p与升温速率β呈线性关系:T_p=11.49lnβ+795.43.采用Kissinger和Doyle-Ozawa方法计算了表观晶化激活能E_a,分别为471.68kJ/mol和461.50kJ/mol.进一步研究发现,该非晶合金的晶化为多阶段的连续形核直至饱和的过程;当进入稳定晶化阶段时,剩余非晶的局域晶化激活能逐渐下降,非晶基体的热稳定性降低,这是由B原子的高温扩散导致的.同时,局域Avrami指数n(α)也反映了不同晶化阶段的形核长大机制.     

非晶合金的热稳定性与热加工窗口研究

采用铜模喷铸法制备了Mg_(68)Zn_(28)Ca_4、Cu_(47)Ti_(34)Zr_(11)Ni_8和Zr_(60)Nb_5Cu_(20)Fe_5Al_(10) 3种非晶合金,通过X射线衍射仪(XRD),差热分析仪(DSC)研究了非晶合金的热加工稳定性,并建立了三维热加工窗口。结果表明,Mg68Zn28Ca4的过冷液相区没有明显随着加热速率的增大向高温区移动,Cu_(47)Ti_(34)Zr_(11)Ni_8和Zr_(60)Nb_5Cu_(20)Fe_5Al_(10)非晶合金的过冷液相区随着加热速率的增大向高温区移动。用Kissinger方法计算出3种非晶的晶化激活能分别为177.26,288.98和288.75kJ/mol。根据建立的三维热加工窗口中可以直接制定非晶合金的加工工艺,确定加工温度及最大加热时间。     

Fe77Co2Zr9B10Cu2合金的制备及其磁性能

采用单辊快淬法制备了Fe77Co2Zr9B10Cu2合金,在530～750℃等温退火40 min,利用X射线衍射和振动样品磁强计研究了Fe77 Co2 Zr9 B10 Cu2合金的微观结构和磁性能。结果表明:淬态Fe77Co2Zr9B10Cu2合金为非晶、纳米晶双相结构。随着退火温度的升高,α-Fe晶体相从非晶、基体中析出,晶粒尺寸长大,晶化体积分数增加,矫顽力先减小后增大,比饱和磁化强度逐渐增大。实验结果表明,530℃退火后合金的矫顽力最小,在670℃时迅速增大。样品的磁性与其微观结构、晶粒尺寸、晶化体积分数等因素有关.     

Effect of the current annealing (without and with tensile stress) on the soft magnetic behaviour of Fe73.5-x(Co0.5Ni0.5)xSi13.5B9Nb3Cu1 alloy ribbons (x = 2.5, 5 and 10)

Experimental data on microstructural (crystalline volume fraction, grain size) and magnetic (coercive field) properties in amorphous and nanocrystalline Fe73.5-x(Co0.5Ni0.5)xSi13.5B9Nb3Cu1 alloy ribbons (x = 2.5, 5 and 10) are presented. Nanocrystalline structure was developed by annealing the precursor amorphous ribbons by current annealing (CA) and stress-current-annealing (SA). Microstructural analysis of the treated ribbons using X-ray Diffraction showed a high content of amorphous phase in the bulk. In addition, substantial changes in the crystalline state such as grain size of the samples annealed at different conditions were observed. The alloy composition also affects greatly the grain size,: increasing the (Co,Ni) content leads to higher values of the average grain size. The evolutions of the coercive field with the two kinds of thermal treatment were analysed, allowing us to conclude that the addition of (Co,Ni) tends to reduce the magnetic softness character of the original material, while the treated SA samples show higher coercivities higher than those treated without by CA.     

Ni含量对激冷贫镍TiNi形状记忆合金薄带相变行为的影

用激冷甩带法制备了Til-xNix(x=45％～49.8％)(原子分数)形状记忆合金(SMA)薄带,用示差扫描量热仪研究了Ni含量对铸态及450℃、500℃退火态TiNi SMA薄带相变行为的影响.结果表明,冷却/加热时,铸态和退火态Ti1-xNix(x=45％～49％)SMA薄带发生A→M/M→A一阶马氏体相变;当Ni含量为49.8％时,铸态和退火态TiNi SMA薄带冷却时发生A→ R→M两阶段相变,加热时发生M→A一阶段相变.随Ni含量增加,TiNi SMA薄带马氏体正、逆相变温度范围先增大后减小,Ni含量为48％时相变温度范围最宽.退火态比铸态TiNi SMA薄带相变温度范围窄.随Ni含量增加,TiNi SMA薄带马氏体正、逆相变温度升高,相变热滞增大.当Ni含量为49％时,SMA薄带的马氏体相变温度达最大值,当Ni含量为49.8％时马氏体相变温度迅速下降.     

Corrosion behaviour and magnetic properties of melt-spun Nd-(Fe·Co·Ni)-B-(Al·Ti) ribbons

The corrosion behaviour of melt-spun Nd-Fe-B alloy ribbons in which Fe was replaced with Co and Ni and small quantities of Al and Ti added was investigated from the viewpoint of anodic corrosion, Although the addition of Ni degraded the magnetic properties of melt-spun ribbons, it improved corrosion resistance. According to EDXS and AES analyses, the corrosion products on the surface of Ni-free ribbons consisted of Nd and Fe oxides, but the Nd oxide corrosion product almost disappeared in the Ni-added samples. Also, the degradation of magnetic properties after the corrosion test was suppressed by the addition of Ni.From these results, it was thought that the improvement of corrosion resistance and the smaller degradation of magnetic properties of Nd-(Fe·Co·Ni)-B-(Al·Ti) ribbons after the corrosion test were associated with the suppressed dissolution of the Nd-rich phase at the grain boundaries.The oxidation of Ni-added melt-spun ribbons also showed similar characteristics and behaviour to the corrosion test in the morphologies of the ribbon surface and magnetic properties after the oxidation test.     

FeCoZrNbB合金的晶化过程及磁性能

采用单辊快淬法制备Fe_81-xCo_xZr₇Nb₂B₁₀(x = 2, 4, 6) 系非晶合金,并对该系非晶合金进行热处理。利用X射线衍射和振动样品磁强计研究FeCoZrNbB 合金系的晶化过程和磁性能。结果表明,Fe_81-xCo_xZr₇Nb₂B₁₀(x = 2, 4, 6) 系合金在快淬速率为30 m/s时完全形成非晶。Fe₇₉Co₂Zr₇Nb₂B₁₀合金的晶化过程为非晶→非晶+α-Fe→α-Fe + Fe₃Zr + Fe₂Nb_0.4Zr_0.6;Fe₇₇Co₄Zr₇Nb₂B₁₀与Fe₇₅Co₆Zr₇Nb₂B₁₀合金的晶化过程相同为非晶→非晶+α-Fe→ α-Fe + Fe₃Zr →α-Fe + Fe₃Zr + Fe₂Nb_0.4Zr_0.6。Co 含量的增加抑制了退火后α-Fe晶相的形核,并促使Fe 3Zr化合物更易析出。Fe_81-xCo_xZr₇Nb₂B₁₀(x = 2, 4, 6) 合金的比饱和磁化强度( M_s) 和矫顽力 ( H_c) 随退火温度的变化趋势相同。530℃ 之前退火,随退火温度的升高M s增加并不明显 ; 530℃之后退火,M_s迅速上升。530℃ 退火,H_c达到最小值;高于530℃ 退火,H_c随退火温度的升高而增加。      

Structures and Properties of Nanocrystalline Nd4.5Fe75Co1Si1B18.5Composite Magnets

1. IntroductionImprovement of hard magnetic properties, simplification of processing, and reduction of cost havebeen the principal motivating factors for much ofthe research on Nd-Fe-B permanent magnet materials since they were discovered. According to traditional Stoner-Wohlfarth model, the biggest Jr/Jsof hard magnetic materials with coarser microstructures is 0.sit]. When the grain size of Nd-Fe--B magnets is small enough, exchange coupled interactionwould be produced between soft and h…     

Phase evolution and magnetic metals co-substituted studies of La and refractory co-substituted alpha i-Fe/R2Fe14B-type nanocomposites

Phase evolution and magnetic properties of (Nd0.95La0.05)(9.5 similar to 11)Febal.M2B10.5, where M=Cr, Ti, Mb, V, Mo, Zr, Hf, Ta, Mn or W, melt spun ribbons have been investigated. Almost all the alloy ribbons, except for (Nd0.95La0.05)(9.5)Fe78M2B10.5 (M=Mo and Mn), consist merely two magnetic phases, namely alpha-Fe and R2Fe14B, which display a better combination of H-i(c) and magnetic energy product. Remanence (B-r) and coercivity (H-i(c)) values in the range of 8.0 to 9.1 kG and 9.5 to 18.9 kOe, respectively, can be achieved. Among compositions studied, the Ti and W-substitutions were found to be most effective in increasing the Br and H-i(c), respectively. For a fixed refractory metal substitution, namely, M=Cr, Ti or Mb, an increase in the total rare earth concentration resulted in nanocomposites of small grain sizes and a high volume fraction of the R2Fe14B phase, leading to an increase in the magnetic properties.     

Phase Evolution and Magnetic Studies of La and Refractory Metals Co-substituted α-Fe/R_2Fe_(14)B-type Nanocomposites

1. IntroductionIn last decade, two types of NdFeB nanocomposite powders, namely, or-Fe/Nd,Fe,.B['] andFe,B/Nd,Fe,.B['] t have drawn much attention of theresearcher for the bonded magnet application, because of their high remanence (B.) and high maximum energy product ((BH)...). The deficiency ofthese types of nanocomposites is their lower coercivity (tHe <8 hoe) arisen from the existence of certain amount of magnetically soft or-Fe or Fe3B phases,which might limit their application in h…     

Microstructure,Phase Composition,and Thermal Stability of Two Zirconium Alloys Subjected to High‐Pressure Torsion at Different Temperatures

The structure, phase composition, and thermal stability of the industrial zirconium alloys, namely, E110 (Zr–1% Nb) and E635 (Zr–1% Nb–0.3% Fe–1.2% Sn), which are subjected to high‐pressure torsion (HPT) at room temperature (RT), 200, and 400 °С have been studied. HPT of Zr‐alloys at RT (10 revolutions) leads to the formation of grain–subgrain nano‐sized structure and to increase the microhardness by 2.1…2.8 times. The increase in the HPT temperature to 200–400 °С leads to the increase in the structural‐element average size. The structural‐element size in the complexly alloyed E635 alloy in all cases is lower compared with the E110 alloy. The hardening of the alloys after HPT at RT and 200 °С is close, and at 400 °С is much less. HPT initiates the α‐Zr → (ω‐Zr + β‐Zr) transformation, which is the main factor for alloys hardening. The α‐Zr → (ω‐Zr + β‐Zr) transformation in the E635 alloy occurs less quickly. The maximum amount (ω‐Zr + β‐Zr) phase in the structure of the alloys is observed after HPT at RT and 200 °C, and the minimum ? at 400 °C. During heating, the alloys undergo the reverse (ω‐Zr + β‐Zr) → α transformation which depends on both the alloy composition and HPT temperature.

     

Fe(Co,Ni)ZrB非晶/纳米晶的制备及晶化过程研究

采用机械合金化法制备了Fe70Zr10B20、Fe63Co7Zr10B20和Fe63Ni7Zr10B20合金.利用X射线衍射仪(XRD)研究了3种合金的机械合金化过程及晶化过程.Fe70Zr10 B20球磨50h后的合金由大量非晶相和少量晶态相组成,Co的添加对FeZrB非晶合金的形成起到了抑制作用;Ni的添加对FeZrB非晶合金的形成起到了促进作用.Fe70-Zr10B20、Fe63Co7Zr10B20合金的晶化过程容易进行,而Fe63 Ni7Zr10 B20合金的晶化比较困难.