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1.
采用累计流量法对供应态Ti-6Al-4V合金进行了固态置氢,运用OM、XRD、TEM分析等方法研究了Ti-6Al-4V合金固态置氢后的微观组织状态及演变过程。结果表明:供应态Ti-6Al-4V合金的置氢量低于0.30%(质量分数,下同)时,置氢使得Ti-6Al-4V合金中的α相减少、β相增加;置氢量达到0.30%时,置氢Ti-6Al-4V合金中有δ氢化物(TiH2相)形成;β-Ti(H)共析转变生成α-Ti和δ氢化物时主要以切变方式进行;置氢Ti-6Al-4V合金的相变温度最多下降了180°C,与Ti-6Al-4V合金在置氢过程中的相体积比变化和共析转变有密切关系。  相似文献   

2.
Ren  Ya-fei  Zhao  Jun  Xie  Hua-sheng  Liu  Shi-bing  Lou  Yan-chun  Yan  Ping 《中国铸造》2017,14(1):55-58
Thermo hydrogen treatment(THT) of titanium is a process in which hydrogen is used as a temporary alloying element in titanium alloys. It is an attractive approach for controlling the microstructure and thereby improving the final mechanical properties. In the present study, the microstructure of the original(non-hydrogenated) sample has only α phase and the grains is coarse with an average size of ~ 650 μm. While the grain size of thermo hydrogen treated Ti-5Al-2.5Sn ELI alloy became finer and the mechanical properties were improved significantly. When the hydrogen content of the hydrogenated Ti-5Al-2.5Sn ELI alloy is 0.321 wt.%, β phase and δ titanium hydride appear. Also the average grain size decreases to 450 μm. When the hydrogen content is 0.515 wt.%, the grain size decreases to 220 μm. The mechanical properties were tested after dehydrogenation, and the mechanical properties improved significantly compared to the unhydrogenated specimens. The tensile strength of the Ti-5Al-2.5Sn ELI alloy improved by 17.7% when the hydrogen content increased to 0.920 wt.%, at the same time the percentage reduction of area(Z) increased by 33% and the impact toughness increased by 37%.  相似文献   

3.
利用电磁成形实验研究氢含量对Ti-6Al-4V合金室温高速压缩性能的影响,通过微观组织观察揭示氢致压缩性能机理。结果表明,氢对Ti6Al4V合金的高速压缩性能存在有益的影响。在电磁成形实验放电能量相同的条件下,Ti-6Al-4V合金的变形率随氢含量的增加呈先增加后降低的趋势。当Ti-6Al-4V合金置氢0.2%(质量分数)时,合金的变形率增加了47.0%。确定了有利于Ti6Al4V合金室温电磁成形时的最佳氢含量。分析了氢致压缩性能的机理。  相似文献   

4.
应用光学显微镜研究氢对Ti-6Al-4V显微组织的影响,并在温度800℃~860℃和应变速率10-3s-1的变形条件下进行超塑拉伸实验。结果表明,随着氢含量的增加,β相的比例提高,且由等轴组织转变为双态组织,随着氢含量的进一步增加,在α相中形成了氢化物;同时,适量的氢可以显著降低Ti-6Al-4V合金峰值应力,置氢0.32wt%H,其峰值流动应力降低了约55%;此外,适量置氢可以显著降低Ti-6Al-4V合金的超塑性变形温度,较原始合金最佳超塑变形温度可降低60℃~100℃,置氢0.11wt%H,在840℃获得了1190%的延伸率,较相同条件下的原始合金延伸率提高75%。文章研究结果可为超塑成形、超塑成形/扩散连接工艺及生产提供优化参考。  相似文献   

5.
置氢Ti-6Al-4V钛合金的热压缩变形行为研究   总被引:1,自引:0,他引:1  
通过热模拟压缩实验,研究了氢对Ti-6Al-4V钛合金热变形行为的影响。结果表明,置氢可以显著降低Ti-6Al-4V钛合金高温压缩时的流动应力,提高Ti-6Al-4V钛合金的热加工变形速率一个数量级以上,并且明显降低了Ti-6Al-4V钛合金的变形温度。在变形温度760℃~800℃范围内,置氢量为0.4wt%的Ti-6Al-4V钛合金的流动应力最小;在变形温度840℃~920℃范围内,置氢量0.2wt%的Ti-6Al-4V钛合金的流动应力最小。同时,置氢前后Ti-6Al-4V钛合金的变形激活能计算结果表明,置氢量为0.4wt%的Ti-6Al-4V钛合金在α+β两相区的变形激活能为208.3kJ/mol,与未置氢Ti-6Al-4V钛合金相比降低了316kJ/mol。  相似文献   

6.
用气相充氢法研究了Ti-6Al-4V合金在初始氢气压力为0.012、0.04和0.07 MPa,温度为800、850和900℃条件下充氢过程中的氢扩散动力学。结果表明,在不同的初始氢气压力和充氢温度下,合金中的平均氢浓度随充氢时间的变化呈现指数关系,由此可见Ti-6Al-4V合金的充氢过程受氢原子的扩散所控制。通过求解扩散方程得到,氢在Ti-6Al-4V合金中的表观扩散激活能为32.80 kJ/mol,此激活能为氢在Ti-6Al-4V合金相中的扩散激活能。  相似文献   

7.
研究了Ti2Al Nb基合金Ti-22Al-(27-x)Nb-x Zr(x=0,1,6,at%)在650~800℃的氧化行为。采用XRD和SEM等测试技术对此温度区间形成的氧化层特征进行了分析。结果表明,相比Ti-22Al-27Nb,含锆合金具有较好的抗氧化性能。Ti-22Al-(27-x)Nb-x Zr合金在650℃氧化100 h,主要氧化产物为Ti O2,而在800℃氧化100 h,Ti O2,Al2O3和Al Nb O4为主要产物,但是在Ti-22Al-21Nb-6Zr合金中还有Zr O2生成。Ti-22Al-26Nb-1Zr合金具有优异抗氧化性能,归因于氧化产物细化形成了致密的氧化层,而Ti-22Al-21Nb-6Zr合金,虽然在800℃也形成了较多Al2O3,但是氧化层中的Zr O2为氧的快速扩散提供通道,进而导致该合金氧化增重明显。  相似文献   

8.
The true stress-true strain curves of Ti-6Al-2Zr-1Mo-1V alloy with hydrogen were obtained by hot compression test. The microstructures of the alloy before and after thermo-compression were observed. The apparent activation energies of deformation were calculated for the alloy with and without hydrogen. The behavior and mechanism of deformation for hydrogenated Ti-6Al-2Zr-1Mo-1V alloy at high temperature were analyzed. The relationship between hydrogenation time and hydrogen content at 800 ℃  can be expressed as the equation: CH(t)=1.2-1.2exp(-t/120). The true stress-true strain curves of hot compression for Ti-6Al-2Zr-1Mo-1V alloy with hydrogen first move down and then move up as hydrogen content increases. Appropriate hydrogen content can reduce the peak of flow stress to minimal value. The apparent activation energies of deformation of the alloy with 0.47% hydrogen content and without hydrogen were calculated as 140 kJ•mol-1 and 390,kJ•mol-1, respectively, at 800   ℃ and at strain rate 8.3×10-4 s-1. The apparent activation energy of deformation increases when the strain rate enhances from 8.3×10-4 s-1 to 8.31×0-2 s-1.  相似文献   

9.
细晶粒钛合金GTAW焊缝成形性能分析   总被引:2,自引:1,他引:1       下载免费PDF全文
通过常规及细晶粒Ti-6Al-4V钛合金的GTAW试验,对比了不同焊接工艺时两种钛合金的焊缝成形.结果表明,由于细晶钛合金晶粒细化,晶界增多,而使热导率降低,焊接过程中晶界对热量传导的阻碍作用变大,这就使得细晶粒钛合金的焊接参数范围变窄,在很大的电流参数范围内,细晶粒钛合金的焊缝成形性能均比常规钛合金差很多;但是在一个较窄的电流变化围内,细晶钛合金的焊缝成形性能优于常规钛合金,超出此范围,成形较差;并讨论了可能的影响因素;针对文中的试件规格推荐了一个最优的焊接电流参数为47~48 A.
Abstract:
Fine grain titanium alloy is used extensively in aerospace and ailrraft because of its excellent comprehensive properties and outstanding machinability. Fine grain Ti-6Al-4V alloy and common grain Ti-6Al-4V alloy were welded by tungsten iner-gas arc welding( GTAW) respectively. Welding parameters and appearance of two Ti-6Al-4V alloys welded were investigated. The results indicate that the heat conductivity impediment of grain boundary strengthened because of fine grain Ti-6Al-4V alloy grains refinement and grain boundary increasing. Thus, its coefficient of heat conductivity is decreasing . Camparing with appearance of common grain Ti-6Al-4V alloy, when the range of welding current parameter was wide, the appearance of fine grain Ti-6Al-4V alloy was bad. However, when the range of welding current parameters was narrow relatively, the appearance of fine grain Ti-6Al-4V alloy welded was better than the one of common grain Ti-6Al-4V alloy. The possible influencing factors were discussed. At last, according to the specimen size, an optimal welding current parameter(47 ~ 48) A was recommended.  相似文献   

10.
βγ-TiAl合金具有良好的高温变形能力,为TiAl合金的发展开辟了新的途径。成功制备了不同x=V/Nb(x=1,1.5,2,3.5)的βγ-TiAlTi-45Al-9(V,Nb,Y)合金,研究了上述合金在800℃静止空气中的氧化行为。结果表明:当x=1时,Ti-45Al-9(V,Nb,Y)合金中形成条带状、连续致密的Al2O3氧化层,显著提高了合金的抗氧化能力。随着x=V/Nb的增加,Al2O3氧化层厚度变薄,合金的抗氧化能力下降。  相似文献   

11.
<正> 1959年 Johnston 和 Gilman 提出位错运动速度 v 与有效应力 σ~*之间的经验公式为:V=B(σ~*)~(m*) (1)其中 B 是系数,m~*称为位错速度的应力指数。用应力弛豫法可以测定 m~*值,如下式所示:  相似文献   

12.
1.IntroductionContinuousfiberreinforcedtitaniummatrixcompositeshavepotentialapplicationatelevatedtemperature.Anewmethodhajsbeentriedbyoneofthepresentautho.s[1'21toalleviatethedeleteriousinterfacereactionbetweenthefiberandthematrix,whichislikelytooccurinthiscompositeduringfabrication.Previous.orb[llshowedthattitaniummatrixcompositecanachievefullconsolidationatrelativelylowtemperaturewiththeaidofhydrogenasatemporaryalloyingelement.Furtherstudyalongthisdirectionshouldbebasedonacomprehensiveunders…  相似文献   

13.
以HDH钛粉制备MIM Ti-6Al-4V合金的过程为参照,对使用氢化钛粉为原料制备P/M模压钛合金以及MIM钛合金的工艺过程进行了探索.使用HDH钛粉制备的MIM Ti-6Al-4V合金抗拉强度为819 MPa,拉伸样延伸率为7%;使用氢化钛粉制备的P/M模压Ti-6Al-4V合金拉伸样抗拉性能高于850 MPa;使用氢化钛粉为原料制备MIM Ti-6Al-4V合金,顺利实现了脱氢-脱脂过程.  相似文献   

14.
采用光学显微镜、透射电镜和拉伸试验等手段,研究了多道次两向轧制和单向轧制对不同原始状态(热轧态、水淬态和空冷态)Ti-6Al-4V合金显微组织和力学性能的影响。结果表明,热轧态Ti-6Al-4V合金的组织为片状α相+β相+少量等轴α相,水淬态Ti-6Al-4V合金形成了针状马氏体组织,空冷态Ti-6Al-4V合金形成了网状组织。Ti-6Al-4V合金适宜的两向轧制温度为700 ℃,此时合金中可见颗粒状β相弥散分布在α基体上。两向轧制Ti-6Al-4V合金的抗拉强度和屈服强度从高至低顺序为:水淬态>热轧态>空冷态,且轧向强度要高于横向;相较于单向轧制,两向轧制明显降低了Ti-6Al-4V合金板材拉伸性能的各向异性,且水淬态Ti-6Al-4V合金的轧向和横向强度差异最小,700 ℃轧制Ti-6Al-4V合金的主要细化机制为位错细化。  相似文献   

15.
研究了Ti811(Ti-8Al-1Mo-1V)和TC4(Ti-6Al-4V)两种钛合金对热盐应力腐蚀(HSSC)的敏感性.结果表明:Ti811合金对HSSC非常敏感,在相同条件下其热盐应力腐蚀临界应力(σHSSC)明显低于TC4合金,且低于同温度的蠕变强度,而TC4合金的σHSSC高于同温度的蠕变强度;两种合金在HSSC暴露过程中,明显遭受到盐腐蚀,腐蚀产生的氢扩散到基体中,致使合金发生脆化,从而降低合金的室温塑性.  相似文献   

16.
本研究采用取向分布函数(ODF)详细分析了具有等轴组织的Ti-6Al-4V热轧退火板在450、600和750℃下经过约45%的温轧压下量后沿层厚的宏观织构演变。结果表明采用多道次温轧的方法成功获得可改善Ti-6Al-4V合金力学性能各向异性的纤维织构ND//hkil和基面织构(0001)[2110]或(0001)[1210]。而且,轧板通体上均形成了ND//hkil纤维织构,中心层的横向织构(1210)[1010]随轧制温度而变化,表层的基面织构通过位错滑移累积剪切应变而产生,且基面织构的形成路径依赖于初始取向。  相似文献   

17.
采用真空感应凝壳熔炼工艺在石墨模中制备Ti-6Al-4V和Ti6Al4V0.5Si两种钛合金。将硅作为一种晶粒细化剂加入到Ti-6Al-4V合金中,考察添加硅对铸态和模锻态Ti-6Al-4V合金组织和性能的影响。铸态合金先在900°C下进行热模锻处理,然后分别进行两种不同的热处理。一种是将模锻样品在1050°C下保温30min,然后水淬以获得细小的层片状组织;另一种是将模锻件在1050°C下保温30min,然后再在800°C下保温30min,以获得粗大的层片状组织。Ti6-Al-4V合金中添加0.5%Si后,铸态合金的晶粒尺寸从627μm减小到337μm,其极限抗拉强度增加约25MPa。具有细小、层片状组织的Ti-6Al-4V0.5Si合金的最大极限抗拉强度为1380MPa,在Hank溶液和NaCl溶液中的腐蚀速度分别为1.35×106和5.78×104mm/a。Ti-6Al-4V合金中添加0.5%Si后,在低滑动速度下的磨损率降低50%,在高滑动速度下的磨损率降低约73%。  相似文献   

18.
The effects of oxygen on the mechanical properties and the lattice strain of commercial pure CP) Ti and Ti-6Al-4V alloys are discussed here in terms of the Vickers hardness, tensile strength and elongation. The Vickers hardness and tensile strength of the CP Ti and the Ti-6Al-4V alloys increased with an increase in the oxygen concentration. On the other hand, the elongation of the CP Ti decreased considerably as the oxygen concentration increased, while that of the Ti-6Al-4V alloys gradually decreased as the oxygen concentration increased. Thus, the oxygen concentration has a greater effect on the mechanical properties of CP Ti compared to its effects on the Ti-6Al-4V alloy. This can be explained in terms of the difference in the solid solution effect of oxygen between the CP Ti and the Ti-6Al-4V alloy. Where, the mechanical properties of Ti-6Al-4V alloy were previously affected by an earlier lattice expansion caused by an increment in the c/a ratio of the Ti-6Al-4V during the Al and V alloying process.  相似文献   

19.
针对Ti-6Al-4V合金汽轮机动叶片出现的组织异常,研究了两种热处理工艺对Ti-6Al-4V合金组织与性能的影响,并对锻造加热温度对该材料显微组织的影响进行了探讨。研究结果表明,Ti-6Al-4V合金汽轮机动叶片的组织异常是由于锻造加热温度过高或加热时间过长引起的,Ti-6Al-4V合金锻后采用固溶+时效或直接时效的热处理的方案都能满足产品毛坯性能要求,且锻后直接时效性能更优异。  相似文献   

20.
研究了置氢Ti-6AL-4V合金在800~860℃温度范围内气压扩散连接行为与机理。在840℃对置氢0.11%(质量分数,下同)的纯钛和Ti-6AL-4V合金进行了扩散连接。应用光学显微镜(OM)、扫描电子显微镜(SEM)和电子探针显微分析仪(EPMA)研究了氢对扩散连接接头焊合率及元素扩散行为的影响。结果表明:氢能够显著提高扩散连接接头的焊合率(置氢0.11%在840℃的焊合率大于98%);氢含量为0.11%的Ti-6Al-4V合金扩散连接后仍为等轴组织,而高氢含量(0.32%~0.48%H)Ti-6Al-4V合金扩散连接后组织转变为粗大的魏氏组织;氢对扩散连接行为的改善作用主要是由于氢的弱键效应及其对元素扩散系数的提高;相对于未置氢Ti-6Al-4V合金,0.11%的氢能够将Al和V元素的扩散系数提高一个数量级,并使扩散连接温度降低了40℃。  相似文献   

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