Ru对一种高W镍基单晶合金蠕变性能的影响

设计并制备了4%W/无Ru、6%W/无Ru以及6%W/2%Ru三种镍基单晶高温合金,通过蠕变性能测试、组织形貌观察、元素分布测定以及XRD谱线测定,研究Ru对一种高W镍基单晶合金蠕变性能的影响。结果表明,提高W含量会促进拓扑密堆相(TCP)析出,从而影响蠕变寿命,6%W/无Ru合金在1070℃/137 MPa条件下的蠕变寿命仅为58 h。元素Ru可改善元素W在γ/γ两相的浓度分布,高温蠕变期间元素Ru可抑制元素W由γ相向γ相扩散。6%W/2%Ru合金经高温蠕变无TCP相析出,其在1070℃/137 MPa条件下的蠕变寿命高达383 h。三种合金在高温蠕变期间,γ相均可形成垂直于应力轴方向的筏状结构,TCP相可破坏筏状结构的连续性,导致γ/γ两相扭折程度加剧,是6%W/无Ru合金蠕变寿命较低的主要原因。     

11.5CrNbTi和15Cr0.5MoNbTi超纯铁素体不锈钢的循环蠕变行为

对11.5CrNbTi和15Cr0.5MoNbTi超纯铁素体不锈钢进行650℃应力控制循环蠕变实验,研究了最大外加应力处引入的保持时间对铁素体不锈钢的循环蠕变变形和断裂行为的影响。结果表明:保持时间的延长使这两种不锈钢的最小循环蠕变速率增大,循环蠕变寿命和循环断裂周次减少。在相同的条件下,15Cr0.5MoNbTi不锈钢的循环蠕变抗力优于11.5CrNbTi不锈钢。这两种不锈钢的循环蠕变断裂模式均为穿晶断裂,随着保持时间的延长断口表面的蠕变孔洞增多,蠕变损伤作用增强。这两种不锈钢循环蠕变后的微观组织均为亚晶,位错的滑移和交滑移是循环蠕变的主要变形机制。     

GH3536合金的蠕变性能及蠕变行为

对GH3536合金在815～900℃不同应力水平下进行了高温蠕变试验,绘制了蠕变曲线并讨论了试验温度和试验应力水平对GH3536合金蠕变性能的影响规律,通过最小二乘法拟合得到了稳态蠕变速率的应力指数和Monkan-Grant关系式的参数,采用L-M参数法建立了外推公式,并对GH3536合金的蠕变断裂强度进行了外推。结果表明:在试验温度和试验应力水平下,GH3536合金的高温蠕变机制主要为位错的滑移和攀移,蠕变过程中有第二相析出,在晶界以及第二相颗粒处形成R型和W型裂纹;蠕变断裂由颈缩引起,为韧性断裂,断裂过程中发生了微孔的聚集和长大;根据外推公式GH3536合金在815℃下蠕变断裂时间2 000h所对应的蠕变断裂强度为58MPa。     

Ti65合金的初级蠕变和稳态蠕变

使用透射电镜(TEM)研究了Ti65合金在600~650℃、120~160 MPa条件下的蠕变变形行为及其微观变形机制。结果表明：初级蠕变变形机制主要由受攀移控制的位错越过α₂相的过程主导;稳态蠕变阶段蠕变机制主要由受界面处扩散控制的位错攀移的过程主导,且应力指数为5~7。在初级蠕变阶段α₂相与位错的相互作用是α₂相对合金高温强化的主要方式,在稳态蠕变阶段沿α/β相界分布的硅化物阻碍位错运动与限制晶界滑移是硅化物对合金强化的主要方式。     

化学气相渗透2D-SiCf/SiC复合材料的蠕变性能及损伤机理

研究了采用化学气相渗透工艺制备2D-SiC_f/SiC复合材料的真空蠕变性能, 蠕变温度为 1200、1300和1400 ℃, 应力水平范围为100~140 MPa。用扫描电子显微镜(SEM)和高分辨透射电子显微镜(TEM)分别观察分析了2D-SiC_f/SiC复合材料的蠕变断口形貌和微观结构。结果表明, 2D-SiC_f/SiC复合材料的主要蠕变损伤模式包括基体开裂、界面脱粘和纤维蠕变。桥接裂纹的纤维发生蠕变并促进了基体裂纹的张开、位移增大, 进一步导致复合材料蠕变断裂, 在复合材料蠕变过程中起决定性作用。2D-SiC_f/SiC复合材料的蠕变性能与SiC纤维微观结构的稳定性密切相关。在1200 ℃/100 MPa时, 纤维晶粒没有长大, 复合材料的蠕变断裂时间大于200 h; 蠕变温度为1400 ℃时, 纤维晶粒明显长大, 2D-SiC_f/SiC复合材料蠕变断裂时间缩短至8.6 h, 稳态蠕变速率增大了三个数量级。     

Cansas-Ⅱ SiCf/SiC复合材料的高温拉伸蠕变行为

连续碳化硅纤维增强碳化硅复合材料(SiC_f/SiC)是发展先进航空发动机的关键材料,航空发动机长时服役要求材料具有优异的高温蠕变性能。本工作研究了平纹编织Cansas-Ⅱ碳化硅纤维增强碳化硅复合材料(2D-SiC_f/SiC)在空气中的高温蠕变行为,蠕变温度为1200～1400℃,应力水平为80～140MPa。利用扫描电子显微镜(SEM)观察了2D-SiC_f/SiC复合材料的微观组织和断口形貌,使用能谱分析仪(EDS)进行了成分分析。结果表明:当蠕变应力低于比例极限应力(σ_PLS)时, 2D-SiC_f/SiC的蠕变断裂时间超过500h,稳态蠕变速率为1×10^–10～5×10^–10/s,蠕变行为由基体和纤维共同控制。当蠕变应力高于σ_PLS时,复合材料的基体、纤维和界面均发生氧化,蠕变断裂时间显著降低,稳态蠕变速率提高一个数量级,蠕变行为主要由纤维控制。     

固溶温度对亚稳β钛合金Ti-4Mo-6Cr-3Al-2Sn的组织和拉伸性能的影响

对自主设计的新型亚稳β钛合金Ti-4Mo-6Cr-3Al-2Sn(%,质量分数)在不同温度进行固溶和固溶时效处理,观察其显微组织和测试室温拉伸性能。结果表明：随着固溶温度的提高固溶态组织中的初生α相减少,当固溶温度高于相变点后初生α相完全消失,几乎全部为明显长大的粗大β晶粒。固溶温度为900℃的固溶态合金具有良好的强度和塑性匹配,屈服强度为898.7 MPa、抗拉强度为962.5 MPa、断裂伸长率为12.7%。在不同温度固溶处理的时效态合金,均析出了细小的次生α相。固溶温度低于相变点时,在初生α相间析出的细小次生α相呈60°或者平行交错排列;固溶温度高于相变点时初生α相几乎完全消失,随着固溶温度的提高析出的次生α相片层间距变大并粗化。在所有固溶温度下,时效态组织中沿原始β晶界处均析出了连续的晶界α相,合金的塑性均较差。经过750℃/0.5 h固溶和500℃/4 h时效的合金具有良好的强度和塑性匹配,其抗拉强度为1282 MPa,屈服强度为1210.6 MPa,断裂伸长率为5.3%。     

Mg-13Gd-1Zn合金的组织与力学性能

研究了铸态、退火态、挤压态和T5时效态Mg-13Gd-1Zn三元合金的显微组织和力学性能。结果表明,合金的铸态组织由α-Mg、(Mg,Zn)₃Gd和14H-LPSO长周期相组成。合金在均匀化退火和热挤压后的直接时效(T5)过程中都发生了晶内14H-LPSO相的沉淀析出,表明合金中14H-LPSO的沉淀相变发生在一个很宽的温度范围(200~510℃)。在挤压后合金的直接时效(T5)过程中发生了β'及β₁相的沉淀析出。在沉淀强化和LPSO强化的共同作用下,合金的屈服强度、抗拉强度和伸长率分别为197 MPa、397 MPa和2.56%。在200℃/80 MPa和200℃/120 MPa两种实验条件下,Mg-13Gd-1Zn合金的抗蠕变性能均优于WE54合金。     

热处理对真空压铸NZ30K镁合金微观组织及力学性能的影响

使用光学显微镜(OM)、扫描电镜(SEM)、能谱分析(EDS)、硬度测试和拉伸性能测试等方法,研究了热处理对真空压铸NZ30K镁合金微观组织及力学性能的影响。结果表明：铸态合金的宏观组织分为表层区和心部区,表层区组织由细小α-Mg等轴晶和分布在晶界的Mg₁₂Nd组成,心部区组织则由细小α-Mg等轴晶、粗大预结晶组织(ESCs)和分布在晶界的离异共晶Mg₁₂Nd组成。在固溶处理过程中心部区晶粒的长大比表层区更为显著,晶界迁移速率与晶粒尺寸不均匀呈正相关性,满足晶粒长大模型v=M₀ exp (-Q/RT) A (1/D₁-1/D₂)。合金的优化热处理工艺为540℃×6 h+200℃×8 h。与铸态合金(UTS=186.0±1.5 MPa,YS=131±2.5 MPa,EL=6.6±0.4%)相比,峰值时效态合金的抗拉强度和屈服强度分别提高到了223.6±4.1 MPa和172.8±2.9 MPa,但延伸率降低到了4.2±0.3%。其强度的提高主要得益于时效析出的片状纳米β"相能够有效地阻碍位错在基面上的滑移。铸态和热处理态合金的表层区断裂模式均为韧性断裂,而心部区的断裂模式在铸态下为准解理断裂、在固溶态下为解理断裂、在峰值时效态下为准解理断裂。     

Ti-Al-Zr-Mo-Nb-Sn-Si系铸造钛合金高温蠕变性能及显微组织研究

针对Ti-Al-Zr-Mo-Nb-Sn-Si铸造高温钛合金,研究了其在600℃、750℃下的蠕变性能与组织变化。结果显示,该铸造钛合金在750℃/180 MPa/0.5 h和600℃/400 MPa/0.5 h条件下的蠕变残余伸长率分别<3%和<0.4%,持久断裂时间分别为>2 h和14 h,具有良好的蠕变性能;高温蠕变断口存在细小颗粒;高温蠕变后塑性变形区的组织变化较小,呈魏氏组织,而集中变形区存在部分晶界消失、α片层宽化现象;高温蠕变后位错明显增多,与析出相相互纠缠。      

DD6单晶合金蠕变特性及断裂机理

在500MPa、900℃和300MPa、1000℃两种环境条件下,通过实验研究了[001]、[011]、[111]三种取向的镍基单晶合金DD6的蠕变特性及断裂机理。结果表明:DD6单晶高温合金蠕变性能具有明显的晶体取向相关性,在相同的温度和应力条件下,三种取向的单晶合金寿命差别很大,温度是影响[001]取向单晶合金蠕变寿命的主要因素,而应力则是影响[011]和[111]取向单晶合金蠕变寿命的主要原因。同时,晶体取向和实验条件的不同,都会使最小蠕变率发生变化,随着温度的升高,不同取向晶体的各向异性减弱,相同条件下,[111]取向最大蠕变量最大,[001]取向次之,[011]取向最小。而晶体取向对断裂机理有直接的影响,[001]、[111]取向DD6单晶合金的断裂是由微孔引起的断裂,[011]取向的DD6单晶合金在900℃、500MPa条件下的蠕变断裂为滑移断裂,1000℃、300MPa条件下的断裂为滑移面断裂和韧窝断裂二者兼有的混合型断裂。     

A parameter for power law creep

Experimental investigations on the creep rupture behaviour of type 304, 304£ and 316 stainless steels, a nickel-base superalloy SuperNi 600 and a turbine disc alloy (equivalent to MAR M 200) have been carried out. Stainless steels 304£ and 316 have been tested with and without weldment, and materials 304 SS and SuperNi 600 have been tested with and without corrosive coatings. MAR M 200 was tested in air. A parametric method is suggested for obtaining the master curves for these alloys under test conditions. The applicability of the parameter to 25-20 stainless steel and a modified nuclear grade 316 type stainless steel has been verified.     

LIFE PREDICTION OF 316 STAINLESS STEEL UNDER CREEP-FATIGUE LOADING

Life prediction for creep-fatigue loading conditions should be related to creep damage mechanisms. In order to examine the effect of the creep damage mode on rupture life under creep-fatigue loading, a “combined creep-fatigue loading test” was carried out on 316 stainless steel. In this method, creep loading and fatigue loading are repeated alternately. The fracture criteria under combined loading closely depend on the creep fracture modes of the static creep test. A new life prediction method which uses this new fracture criterion is proposed. The criteria are changed when the creep damage mode varies. In order to verify the adequacy of this method, fatigue tests with a tensile strain-hold wave form were carried out. It is clear that rupture life in such fatigue tests is dependent on the chosen fracture criteria.     

Creep behavior of nuclear grade 316LN austenitic stainless steel at 873 K and 923 K

Mechanics of Time-Dependent Materials - Creep deformation and rupture behavior of nitrogen-alloyed (0.14 wt.%) nuclear grade 316LN austenitic stainless steel were investigated for the varying...     

Zr-Cu-Ni非晶钎料真空钎焊TiAl合金/316L不锈钢接头的界面组织与剪切性能

采用自主设计制备的Zr-42.9Cu-21.4Ni非晶钎料对TiAl合金和316L不锈钢进行真空钎焊,研究钎焊温度和钎焊时间对TiAl合金/316L不锈钢异种金属接头微观组织和剪切性能的影响。结果表明：钎缝界面可以划分为6个不同的反应层。1040 ℃/10 min下制备的钎焊接头从TiAl合金到316L不锈钢侧界面组织依次为γ(TiAl)+AlCuTi/α₂(Ti₃Al)+AlCuTi/AlCu+ZrCuNi+FeZr/Cu₈Zr₃+ZrCuNi+TiFe+Fe₂Zr/FeZr+Fe₂Zr+TiFe₂+ZrCu/α-(Fe, Cr)。随着钎焊温度的升高,接头的抗剪强度先升高后降低。当钎焊温度为1040 ℃和钎焊时间25 min时,接头抗剪强度达到最大值162 MPa。断口分析表明,接头在FeZr+Fe₂Zr+TiFe₂+ZrCu界面处萌生,沿着Cu₈Zr₃+ZrCuNi+TiFe+Fe₂Zr和α-(Fe, Cr)扩展,呈解理断裂。     

Effect of NiCr and NiCrAl coatings on the creep resistance of a Ni alloy

The effect of plasma sprayed NiCr and NiCrAl coatings on the creep resistance of Nickel alloy 690 at temperature of 1033 K was investigated. Experimental results showed that the coatings had a beneficial effect on the improvement of the creep resistance of substrate. However, there was almost no difference in the creep lives between the NiCr and NiCrAl coated specimens at a given stress level. The relation between the applied stress and time to rupture of the coated specimens can be estimated by using Larson-Miller equation. For the coated specimens tested at low applied stress levels, the product of the minimum creep rate and the time to rupture was a constant value. The θ projection method can be used to accurately characterize the creep behavior of the coated specimens. The variation of the creep strain along with time predicted by using θ projection method agreed well with the experimental results.     

Small punch and uniaxial creep fracture behaviours of modified SUS304H steel at various temperatures

Commercial austenitic stainless steel SUS304H with small amount of vanadium addition was used in this study. Small punch (SP) creep and uniaxial tensile creep tests were conducted at 650, 700, and 750 °C to measure creep lives and the minimum displacement rates or the minimum creep strain rates. The measured parameters were compared between the two test methods, seeking empirical relationships among the parameters using Larson-Miller Parameter and Monkman-Grant relation. Magnitude of the applied stress (MPa) in the uniaxial tensile creep test was approximately equal to the applied load value (N) in the SP creep test at all test temperatures. It was shown that during the creep deformation of the SP creep specimen, crack initiation and accompanying crack growth occur simultaneously. Competing failure mechanisms of creep deformation and crack growth may affect the SP creep life and consequently determine the proportionality function, α, in the relation between the SP load and the tensile creep rupture stress in creep tests.     

Research on representative stress and fracture ductility of P92 steel under multiaxial creep

Creep experiments on both plain and notched specimens were conducted at 650 °C over a stress range of 120–185 MPa. The notch strengthening effect was found to exhibit in notched specimens. By using stress components at the skeletal point, several expressions of representative stress were compared to validate their effectiveness in predicting creep rupture lives of P92 steel under multiaxial stress states. The results showed that Hayhurst representative stress was more suitable for life predictions of P92 steel. In the mean time, the relationship between the fracture ductility and multiaxiality was presented to investigate the influence of the multiaxial stress states on creep rupture behavior of P92 steel. A more reasonable prediction model was proposed, and the validity of the model was verified by experimental data.     

Mechanistic approach for prediction of creep deformation,damage and rupture life of different Cr–Mo ferritic steels

Abstract

A mechanistic approach based on finite element analysis of continuum damage as proposed by Kachanov has been used to assess and compare creep deformation, damage and rupture behaviour of 2·25Cr–1Mo, 9Cr–1Mo and modified 9Cr–1Mo ferritic steels. Creep tests were carried out on the steels at 873 K over a stress range of 90–230 MPa. Modified 9Cr–1Mo steel was found to have highest creep deformation and rupture strength whereas 2·25Cr–1Mo steel showed the lowest among the three ferritic steels. Creep damage in the steels has been manifested as the microstructural degradation. 2·25Cr–1Mo steel was more prone to creep damage than 9Cr–steels. Finite element estimation of creep deformation and rupture lives were found to be in good agreement with the experimental results.     

HA-316L不锈钢纤维非对称功能梯度生物材料制备与显微组织

用低压热等静压方法在1100℃下制备了HA(ZrO₂)-316L不锈钢纤维非对称FGM,其中316L不锈钢纤维含量按体积比20%→15%→10%→5%呈非对称梯度变化.并通过金相显微镜、SEM、EDXA分析了材料的微观结构和微区元素含量.结果表明,HA(ZrO₂)-316L不锈钢纤维非对称FGM微观上表现为316L不锈钢纤维在FGM中呈无序、均匀分布状态,316L不锈钢纤维包裹于HA(ZrO₂)基体中,两者结合紧密,界面表现为部分凹凸不平,316L不锈钢纤维与HA(ZrO₂)基体紧紧的咬合在一起.在FGM基体中发生了微量的韧化相Fe元素扩散,韧化相316L不锈钢纤维不发生基体相Ca、P元素的扩散,基体与韧化相均相对独立,二者之间不发生任何化学反应.随着HA含量增加,HA(ZrO₂)-316L不锈钢纤维复合材料的断裂韧性和弹性模量逐渐减小,体现了FGM中各梯度层的力学性能缓和设计.HA(ZrO₂)-316L不锈钢纤维FGM中,分析认为,增韧机理主要为纤维拔出增韧和层间裂纹偏转增韧.