淬火温度对气瓶用Fe-Cr-Ni-Mo钢组织和力学性能的影响

为了优化一种气瓶用Fe-Cr-Ni-Mo钢的淬火工艺,采用SEM,TEM,EBSD和拉伸、冲击等观察和检测手段,研究了淬火温度对一种气瓶用Fe-Cr-Ni-Mo钢微观组织和力学性能的影响。结果表明,不同淬火温度处理后的合金钢,均呈现为板条马氏体组织,其碳化物析出和板条亚结构基本保持不变,而原始奥氏体晶粒则随淬火温度的提高而出现明显的粗化,由800℃的4.3µm长大到930,1200℃的29.6,371.1µm,同时有效晶粒尺寸(EGS)也逐渐增加,800,930,1200℃的EGS分别为0.60,1.20,3.22µm。淬火温度对合金钢的室温抗拉、屈服强度和断后伸长率影响较小,而随着淬火温度的提高,冲击吸收能量则出现了显著的下降,由800℃的119 J,下降到930,1200℃的68,38 J。EGS增大导致冲击断裂时出现解理断裂,是较高淬火温度合金钢冲击吸收能量下降的主要原因。淬火温度为800~860℃时,Fe-Cr-Ni-Mo钢具有良好的强韧性匹配,该研究结果对Fe-Cr-Ni-Mo钢制气瓶的工业化生产具有指导意义。

Electroplating process of amorphous Fe-Ni-Cr alloy

A novel process of electroplating amorphous Fe Cr Ni alloy in chloride aqueous solution with Fe(Ⅱ), Ni(Ⅱ) and Cr(Ⅲ) was reported. Couple plasma atomic emission spectrometry (ICP AES), X ray diffractometry(XRD), scanning electronic microscopy(SEM), microhardness test and rapid heating cooling method were adopted to detect the properties of the amorphous Fe Ni Cr deposit, such as composition, crystalline structure, micrograph, hardness, and adherence between deposit and substrate. The effects of the operating parameters on the electrodeposit of the amorphous Fe Ni Cr alloy were discussed in detail. The results show that a 8.7?μm thick mirror like amorphous Fe Ni Cr alloy deposit, with Vicker’s hardness of 530 and composition of 45%～55% Fe, 33%～37% Ni, 9%～23% Cr was obtained by electroplating for 20?min at room temperature(10～30?℃), cathode current 10～16?A/dm 2, pH=1.0～3.0. The XRD patterns show that there only appears a broad hump around 2 θ of 41?°～47?°for the amorphous Fe Ni Cr alloy deposit, while the SEM micrographs show that the deposit contains only a few fine cracks but no pinholes.

Factors Affecting Transformation Temperatures in Fe-Mn-Si-Cr-Ni Shape Memory Alloy

The effects of prestrain and annealing temperature on phase transformation temperatures in Fel4Mn5Si8Cr4Ni shape memory alloy have been studied. The results showed that when the annealing temperature was 673 K, both the At and the Ms temperatures increased appreciably as the prestrain increased, the As temperature increased slightly with increasing prestrain; the resistivity difference at 303 K between the heating and cooling curve also increased with increasing prestrain, which agreed with the recovery strain. The shape memory effect in Fe-Mn-Si-Cr-Ni shape memory alloy is caused by the stress-induced γ→ε martensite transformation and its reverse transformation. When the prestrain was 10%, the Ms temperature decreased remarkably as the annealing temperature increased.

Shape Memory Effect of As-aged Fe-14Mn-5Si-8Cr-4Ni-0.2C Alloy

The effects of aging temperature on shape memory effect, mechanical properties and microstruc-ture of Fe-14Mn-5Si-8Cr-4Ni-0.2C shape memory alloy have been studied. The results showed that the second phase particles rich in chromium, manganese and silicon precipitate during aging, and thereby increase the hardness and strength of the alloy. The shape recovery ratio can be remarkably improved by aging and a maximum value can be obtained at 1223 K, which is 68% higher than that of the specimen in solid solution state. When the aging temperature is below 1223 K, the amount of second phase particles increases as the aging temperature increases. The size of austenite grain increases with increasing aging temperature. When the temperature is over 1223 K, the second phase particles can not precipitate. The lack of second phase particles and the increase of grain size make the hardness and shape recovery ratio drastically decrease, when the temperature is over 1223 K.

Effects of cryogenic treatment on mechanical properties and microstructure of Fe-Cr-Mo-Ni-C-Co alloy

Fe-Cr-Mo-Ni-C-Co alloy was quenched in liquid nitrogen and held for 24 h.Hardness tester,OM,XRD,SEM were used to investigate the mechanical properties and microstructures of the alloy.The results show that the hardness increases by 1-2(HRC)and the compressive strength decreases slightly after cryogenic treatment.The increase in hardness is attributed to the transformation from austenite to martensite and the precipitation of the very tiny carbideη-Fe2C.The decrease in compressive strength is caused by residual stress.The great amount of carbides,such as Cr7C3 and Fe2MoC,in the alloy and the obvious difference in thermal expansion coefficient between these carbides and the matrix at the cryogenic temperatures lead to this residual stress.The microscopy of cryogenic martensite is different from that of the non-cryogenic martensite.The cryogenic martensite is long and fine;while the non-cryogenic martensite is short and coarse.There is obvious surface relief of the cryogenic martensite transformation.It is not orientational of this kind surface relief and the boundary of this surface relief is smooth and in a shape of butterfly.The surface relief in the non-cryogenic martensite is wide and arranged in parallel,and the boundary of surface relief is not smooth.These characteristics may imply different growth ways of the two kinds of martensite.

电感耦合等离子体原子发射光谱法测定哈氏合金中Cr、Fe、Mn、Mo、Ni的含量

哈氏合金（Hastelloy alloy）由Ni、Cr、Mo、Fe等元素组成,属于高等镍基合金,镍为面心立方结构,晶体学上的稳定性使得它能够比铁基合金容纳更多的合金元素[1]。哈氏合金作为高级镍基合金,在湿氧、亚硫酸、强氧化盐介质中都有优异的抗腐蚀性能[1],同时具有优良的强度、塑性、韧性、冶金稳定性、可加工性及可焊接性,已广泛应用于航空航天、核电及船舶等领域[2]。

Thermal stability,crystallization behavior,Vickers hardness and magnetic properties of Fe-Co-Ni-Cr-Mo-C-B-Y bulk metallic glasses

Thermal stability,crystallization behavior,Vickers hardness and magnetic properties of the Fe41Co7-xNixCr15Mo14C15B6Y2（x=0,1,3,5） bulk metallic glasses were investigated.The Fe41Co7-xNixCr15Mo14C15B6Y2（x=0,1,3,5） metallic glasses were fabricated by copper mold casting method.The thermal stability and crystallization behavior of the metallic glass rods were investigated by differential scanning calorimetry and isothermal experiments.Hardness measurements for samples annealed at different temperatures for different time were carried out at room temperature by the Vickers hardness tester,and magnetic measurements were performed at different temperatures by the vibrating sample magnetometer.It is shown that the addition of Ni does not play a positive role for enlarging ΔTx and GFA from parameter γ（=Tx/（Tg＋Tl））,and it can,however,increase the activation energy in the initial stage of crystallization by changing the initial crystallization behavior.The minor addition of Ni can refine the crystal grain obtained from the full crystallization experiment.The primary crystallization causes the decrease of hardness in these alloys,and as the crystallization continues,the hardness in all samples increases instead due to the precipitation of carbide and boride.The annealing temperature has an obvious effect on magnetic properties of these alloys,and the minor addition of Ni can effectively prevent the alloy annealed at high temperature to transform from paramagnetic to ferromagnetic state.

Studies on induction hardening of powder-metallurgy-processed Fe–Cr/Mo alloys

Induction hardening of dense Fe–Cr/Mo alloys processed via the powder-metallurgy route was studied. The Fe-3Cr-0.5Mo, Fe-1.5Cr-0.2Mo, and Fe-0.85 Mo pre-alloyed powders were mixed with 0.4wt%, 0.6wt%, and 0.8wt% C and compacted at 500, 600, and 700 MPa, respectively. The compacts were sintered at 1473 K for 1 h and then cooled at 6 K/min. Ferrite with pearlite was mostly observed in the sintered alloys with 0.4wt% C, whereas a carbide network was also present in the alloys with 0.8wt% C. Graphite at prior particle boundaries led to deterioration of the mechanical properties of alloys with 0.8wt% C, whereas no significant induction hardening was achieved in alloys with 0.4wt% C. Among the investigated samples, alloys with 0.6wt% C exhibited the highest strength and ductility and were found to be suitable for induction hardening. The hardening was carried out at a frequency of 2.0 kHz for 2–3 s. A case depth of 2.5 mm was achieved while maintaining the bulk(interior) hardness of approximately HV 230. A martensitic structure was observed on the outer periphery of the samples. The hardness varied from HV 600 to HV 375 from the sample surface to the interior of the case hardened region. The best combination of properties and hardening depth was achieved in case of the Fe-1.5Cr-0.2Mo alloy with 0.6wt% C.

粉末锻造Al_(2)O_(3)颗粒增强Fe–Ni–Mo–C–Cu复合材料的组织与性能

通过粉末锻造技术制备了不同含量微米级Al_(2)O_(3)颗粒强化的Fe–Ni–Mo–C–Cu(Q61)复合材料,并对调质态和淬火态复合材料的组织和性能进行了研究。结果表明:当Al_(2)O_(3)质量分数为0.15%时,增强颗粒在基体内分布均匀;相较于同种状态下不添加增强颗粒的单一Q61,调质态复合材料的硬度从HRC 38增至HRC 39.8,屈服强度从1106 MPa增至1121 MPa,延伸率从12%降至6.5%;淬火态复合材料的硬度从HRC 61.5增至HRC 63.2,磨损率从5.27×10^(-6)mm^(3)·m^(-1)·N^(-1)降至3.08×10^(-6)mm^(3)·m^(-1)·N^(-1),低于对比试验用的典型齿轮材料40Cr的磨损率(3.34×10^(-6)mm^(3)·m^(-1)·N^(-1))。当Al_(2)O_(3)质量分数大于0.15%时,Al_(2)O_(3)颗粒逐渐偏聚,虽然调质态下复合材料屈服强度仍继续小幅增加,但塑性严重退化,且淬火态复合材料磨损率增加,耐磨性变差。综合来看,添加0.15%Al_(2)O_(3)颗粒强化Q61复合材料在调质态下具有较高的综合力学性能,而在淬火态下表现出良好的抗摩擦磨损能力。

Al-Cr-Fe-Mn-Ni高熵合金中的L2_(1)相的相稳定性及其性能研究

为开发兼具良好强度与塑性的BCC基高熵合金,可引入与基体共格的B2或L2_(1)相。L2_(1)相具有更好的抗蠕变性能,有望在高温环境中得到应用。但是,目前对BCC型高熵合金中L2_(1)相的存在规律、相稳定性及其对合金性能的影响还缺乏深入的研究。为此,本工作研究了电弧熔炼制备的铸态Al_(0.5)Cr_(2.5-x)FeMn_(x)Ni(x=0.5~1.75)、Al_(0.75)Cr_(2.25-y)FeMn_(y)Ni(y=0.25~1.5)、AlCr_(2-z)FeMn_(z)Ni(z=0.5~1.5)高熵合金的相组成,及800℃或1000℃真空退火120 h对合金组织和相组成的影响。研究表明,这些合金中L2_(1)相的成分特征由40%~50%(原子分数)Ni和15%~20%(原子分数)Al、Mn组成。L2_(1)相只存在于Al含量为10%~15%(原子分数)的合金中,且多以BCC+L2_(1)两相共存,获得的组织为编织网状的调幅分解组织。当Al含量达到20%(原子分数)后,合金则由BCC+B2两相构成。L2_(1)相的存在会使BCC型XRD特征峰出现明显的峰分裂。经过800℃或1000℃退火后,合金中L2_(1)相仍能稳定存在,合金显微组织发生粗化并会形成σ或FCC相。铸态合金的硬度随Mn含量的增加而降低,含L2_(1)相的合金的硬度在463HV~558HV范围内。800℃退火会使含5%~15%(原子分数)Mn的合金硬度降低70HV~100HV,但由于硬质σ相的析出,含20%~30%(原子分数)Mn的合金硬度提高200HV以上;1000℃退火后,由于软质FCC相的形成,合金的硬度略有降低,这些结果将为BCC型高熵合金的设计奠定基础。

Fe-Cr-Ni-Mo合金27-7Mo的抗CO_2腐蚀性能

模拟大庆油田井下的腐蚀环境,使用高温高压釜进行了27-7Mo合金钢的腐蚀试验,并采用SEM、EDS和XPS测试手段对该钢的腐蚀产物膜进行了分析。结果表明:27-7Mo合金钢CO2腐蚀速率在温度120℃,压力10MPa条件下出现极大值,在其余试验条件下均属于轻度腐蚀。27-7Mo钢腐蚀产物膜较薄,有浅的沟渠,整体属于均匀腐蚀。其腐蚀产物膜主要由Cr、Ni、Mo、Fe的氧化物和氢氧化物构成。

Ni-Cr-Fe-Mo-Co-W合金中宏观“黑斑”缺陷的特征分析

将晶界萃取碳复型技术同其它实验技术相配合 ,研究了Ni-Cr-Fe-Mo-Co -W合金宏观“黑斑”缺陷特征的形成原因 ,认为“黑斑”缺陷主要是由晶界易腐蚀引起的。在“黑斑”区不均匀富集的钨、钼元素主要以数量较多、尺寸较大的富含钼、钨的M6C形式存在于晶界上 ,使“黑斑”区的晶界易受腐蚀。该合金中的“黑斑”缺陷具有元素的宏观偏聚和微观偏聚相结合的特点。

Temperature Dependent Work-hardening Behaviour in an Fe-Mn-Si-Cr-Ni Shape Memory Alloy

The work-hardening behaviour in an Fe-Mn-Si-Cr-Ni alloy has been investigated using tensile test at different temperatures and TEM observation. It was found that besides the intersection of εmartensite, the intersections of ε martensite with stacking fault and the cross-slip of dislocation which is difficult to occur in the alloy with low stacking fault energy are also important factors to the temperature dependent work-hardening behaviour.

FRECKLE FORMATION AND CHARACTERIZATION OF A Ni-Cr-Mo-Fe-W ALLOY

The freckle formation and their phase characterization in freckle areas were investigated by means of microstructure analysis approaches and a thermodynamic equilibrium phase calculation method in a Ni-Cr-Mo-Fe-W alloy. These results show that in freckle areas a large number of M6C, μ and P phases precipitate in grain boundaries even within grain due to the enrichment and segregation of Mo and C during solidification, which results in small grains in freckle areas. Equilibrium phase and liquid segregation calculation can give an reasonable interpretation of the freckle feature for this alloy.

Hydrogen Permeation and Diffusion in Amorphous Alloy Ni_(68)Cr7_Si_8B_(14)Fe_3 at Elevated Temperature

The behaviour of hydrogen permeation and diffusion in amorphous alloy Ni68Cr7Si8B14Fe3 hasbeen investigated by an ultrahigh vacuum gas permeation technique. A comparison experimentwas carried out between the as-quenched and annealed States (400℃/2h) of the amorphousalloy. The results show that, for both states of the amorphous alloy in the temperature rangeof 200～350℃, the diffusivity and permeability of hydrogen are in agreement with Arrheniusrelationship, there does not exist H-trapping effect, and the activation energies of diffusion andpermeation almost keep the same.

THERMODYNAMIC PROPERTIES OF NITROGEN IN Fe-Cr-Ni ALLOYS AT 1873K

The dependence of first interaction parameter (chromium on nitrogen) upon the content of Cr in Fe-Cr-Ni-N melt was expressed. The formalism developed for describing thermodynamics of metallic multicomponent systems was applied to the Fe-Cr-Ni-N quaternary system. (Edited author abstract) 17 Refs.

利用褐铁矿型红土镍矿烧结矿制备Fe-Cr-Ni合金

我国是不锈钢第一生产大国,但作为冶炼不锈钢主要原料的镍矿及铬铁矿资源贫乏,占红土镍矿资源总量60%以上的褐铁矿型红土镍矿与低品位铬铁矿愈发受到关注。同时,不锈钢冶炼通常需先分别生产铬铁和镍铁,工艺流程长,生产成本高。因此,本文基于烧结—高炉工艺,利用褐铁矿型红土镍矿烧结矿低成本地一步制备出了Fe-Cr-Ni合金。通过热力学分析及熔炼参数的优化,重点研究了不同Cr_(2)O_(3)含量的含镍烧结矿(S1:4.84 wt%;S3:7.72 wt%)的熔炼特性。在熔炼时间60 min(S1)/90 min (S3)、熔炼温度1600℃、焦粉用量20 wt%、炉渣碱度1.0的最佳条件下,成功制备出了铬品位5.6 wt%~9.3 wt%、镍品位1.55 wt%~1.70 wt%、铁品位84 wt%~88 wt%的Fe-Cr-Ni合金,其铬、镍和铁的回收率分别在90%、98%和96%以上。研究表明,含镍烧结矿Cr_(2)O_(3)含量的提高会造成熔炼时间的延长,这不利于焦比的降低与不锈钢产量的提高。在后续研究中,将开发出由含镍烧结矿与含铬球团矿构成的综合炉料结构,以更有效地实现高铬镍铁的冶炼。

Ni-Cr-Mo-Cu合金Fe掺杂的合金组织分析

应用扫描电镜和X-射线衍射测试,对在Ni-Cr-Mo-Cu合金中进行Fe掺杂的合金进行了微观组织观察和量化分析,表明该合金形成了基体和弥散相两种组织。使用Materials studio7.0材料计算软件对主要组织的超晶胞进行了结合能的计算,最终确定出了基体和弥散相的成分组成。

Fe-Mo-Cr-Ni耐磨合金成分和热处理工艺对组织及性能的影响

采用扫描电镜、能谱仪和X射线衍射仪等分析手段,结合硬度测定和摩擦磨损实验,研究了一类基于Laves相强化的FeMo-Cr-Ni耐磨合金的成分及热处理工艺与组织性能之间的关系。结果表明,铸态合金为Laves+α-Fe(Mo,Cr,Ni)两相组织,主要呈魏氏体组织和枝晶组织两种类型,均匀化退火处理后魏氏体组织特征完全消失,随着Mo和Ni元素含量增加,沿Laves相边界逐渐析出χ相,淬火处理后,χ相析出量增加;铸态合金磨损机制为粘着磨损,退火态合金磨损机制为磨粒磨损;实验中Fe Mo25Cr14Ni10合金具有优异的组织与性能。

Si对Fe-Mo-Cr-Ni合金组织及耐熔体腐蚀性能的影响

采用扫描电镜(SEM)和X射线衍射仪(XRD),研究了Si元素对Fe-Mo-Cr-Ni合金组织及耐Galvalume合金和铝熔体腐蚀性能的影响。结果表明,添加Si元素后,铸态组织由α-Fe+Laves逐渐转变为α-Fe+Laves+R,随Si含量的增加,组织形貌也依次呈现魏氏体、编织针状、枝晶状和花纹层状组织;Si元素的加入能有效提升Fe-Mo-Cr-Ni合金的耐蚀性,其中含Si量为1wt%的Fe-Mo-Cr-Ni合金耐腐蚀能力最佳,腐蚀速率最低。