偏离<001>取向15°的三种镍基单晶高温合金试样的中温蠕变变形行为

研究了一种偏离001取向15°的镍基单晶高温合金的中温蠕变(760℃/793 MPa)性能和变形组织。结果表明:取向靠近001-101边界合金的蠕变寿命最长,而取向靠近001-111边界合金的蠕变寿命最短。虽然三种试样取向偏离001的夹角都约为15°,但是其微观变形组织明显不同。取向靠近001-101边界试样的变形主要受控于{111}110滑移系,而取向靠近001-111边界试样变形主要受控于{111}112滑移系。     

Anisotropy of Stress Rupture Properties of DD6 Single Crystal Superalloy at 980℃/250MPa Near [001] Orientation

通过不同取向DD6单晶高温合金980℃/250MPa持久测试,研究了取向对980℃持久性能的影响.结果表明:[001]取向偏离主应力轴15°以内,DD6单晶高温合金980℃/250MPa持久寿命相当,没有各向异性.这主要是由于近[001]取向DD6单晶高温合金多个<110>{111}滑移系共同作用的结果.同时,原子扩散造成的γ’筏排和γ/γ’相界面形成的位错网也降低持久性能各向异性.     

近[001]取向DD6单晶高温合金980℃/250MPa持久性能各向异性研究

通过不同取向DD6单晶高温合金980℃/250MPa持久测试,研究了取向对980℃持久性能的影响。结果表明:[001]取向偏离主应力轴15°以内,DD6单晶高温合金980℃/250MPa持久寿命相当,没有各向异性。这主要是由于近[001]取向DD6单晶高温合金多个〈110〉{111}滑移系共同作用的结果。同时,原子扩散造成的γ′筏排和γ/γ′相界面形成的位错网也降低持久性能各向异性。     

一种镍基单晶高温合金压缩变形的各向异性

将一种镍基单晶高温合金在室温沿不同晶体取向压缩变形,研究了在试样表面形成的滑移线和微观组织的变化。结果表明：这种合金〈111〉取向试样的屈服强度最高,〈001〉取向的强度最低,〈110〉取向的强度居中。〈001〉和〈110〉取向的试样在压缩变形过程中主要启动八面体滑移系,其中〈110〉取向明显观察到双滑移系的开动;而〈...     

DD6单晶高温合金980℃蠕变性能研究

研究了第二代单晶高温合金DD6的[001],[011]和[111]取向980℃不同应力条件的拉伸蠕变性能.结果表明,DD6合金的蠕变性能良好,并具有蠕变各向异性;与[011]和[111]取向相比,应力对[001]取向的合金蠕变寿命影响较小;蠕变过程中由于晶体转动[001]结晶取向与主应力轴方向偏离度逐渐减小,而[011]和[111]结晶取向与主应力轴方向偏离度有所增加;[001]取向的合金加工硬化倾向性较大,[011]和[111]取向的合金加工硬化倾向较小.     

初始凝固组织对Cr17表面皱折的影响机制

研究了Cr17铁素体不锈钢的初始凝同组织对与皱折特性相关的晶粒簇演变的影响和对冷轧退火板铍折的影响机制.结果表明:1.柱状晶和等轴晶铸坯在轧制和退火过程中其晶粒簇演变是不同的;2.等轴晶铸坯的冷轧退火试样比柱状晶铸坯的冷轧退火试样具有更少的{001}<110>晶粒簇和更多的{111}<112>晶粒簇;3.两种铸坯冷轧退火试佯皱折特性的差异归因于两者的{001}<110>、{111}<112>晶粒簇数量和分布的不同,而与{001}<010>、{111}<110>、{112}<110>晶粒簇无关.     

挤压态6013-T4铝合金在动态冲击载荷下的变形行为及其微观机理

使用霍普金森压杆试验装置进行挤压态6013-T4铝合金的室温动态压缩实验,应变速率为1×10³~3×10³ s^-1。结果表明,6013-T4铝合金在动态压缩过程中表现出明显的应变硬化和正应变速率敏感性;随着应变和应变速率的提高位错密度增大,在高应变速率和大应变量变形后试样的位错塞积显著。在相同的变形条件下0°方向试样的应力总是最高,而45°方向试样的应力最低。挤压态6013-T4合金的主要织构类型为{112}<111>和{110}<111>。对于{112}<111>织构,0°、45°和90°方向的最大施密特因子分别为0.27、0.49和0.41。对于{110}<111>织构,最大施密特因子分别为0.27、0.43和0.41。0°方向的施密特因子最小,使该方向的应力水平较高。在相同的应变速率和应变量条件下动态压缩变形时,0°方向试样的位错密度更高。在冲击件的材料选择和结构设计中有必要考虑材料的应变速率敏感性、力学性能各向异性以及微观组织的演变。     

一种4.5%Re镍基单晶合金在980℃蠕变期间的变形与损伤机制

通过蠕变性能测试和组织形貌观察,研究了一种Re含量为4.5%Re(质量分数,下同)的镍基单晶合金的高温蠕变行为、变形和损伤机制。结果表明,4.5%Re合金在980℃/300MPa的蠕变寿命为169h。蠕变初期,合金中立方γ′相转变为垂直于应力轴的N型筏状结构。稳态蠕变期间,合金的变形机制为位错在基体中滑移和攀移越过筏状γ′相。蠕变后期,合金的变形机制为位错在基体中滑移和剪切进入筏状γ′相。由于γ基体通道较窄,位错在基体通道中滑移所需的阻力较大。剪切进入γ′相的110超位错可由{111}面交滑移至{100}面,形成K-W锁,从而抑制位错的滑移和交滑移,这是合金具有较好蠕变抗力的主要原因。主/次滑移位错的交替开动,可致使筏状γ′相扭曲,并促使裂纹在筏状γ/γ′两相界面萌生;裂纹沿垂直于应力轴方向扩展,直至断裂,这是合金的蠕变断裂机制。     

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。     

一次枝晶间距对DD26单晶高温合金持久各向异性的影响

研究了取向对高速冷却法(DD26-HRS)和液态金属冷却法(DD26-LMC)制备的DD26单晶高温合金760℃/670 MPa条件下持久性能的影响。结果表明,DD26-HRS合金一次枝晶间距明显大于DD26-LMC合金,而且DD26-HRS合金持久各向异性更为严重。位错形貌显示靠近[001]-[012]边界试样变形以基体内多滑移为主。由于DD26-HRS合金γ′相尺寸较大,抑制了层错带剪切γ′相的变形机制,从而使得DD26-HRS合金持久寿命高于LMC合金。然而,靠近[001]-[112]边界试样变形以单方向层错剪切γ′相为主,基体内开动的位错较少,DD26-HRS合金枝晶间粗大的碳化物相周围易于位错的堆积,从而萌生裂纹并沿碳化物界面迅速开裂,造成DD26-HRS合金持久寿命低于DD26-LMC合金。     

EBSD Investigation on Oriented Nucleation in IF Steels

The mechanism responsible for the formation of recrystallization texture in cold-rolled Ti bearing interstitial free （IF） steel sheets was investigated using electron back-scatter diffraction （EBSD）. In addition, the origin of nuclei with specific orientations was studied. The formation of recrystallization texture was explained by oriented nucleation. Most nuclei have a high misorientation angle of 25-55° with the surrounding deformed matrices, but no specific orientation of misorientation axis between the nucleus and the surrounding deformed matrix is observed. The stored energy of deformed grains is in the decreasing order of the {111}〈112〉,{111}〈110〉, {112}〈110〉 and {001}〈110〉 orientations. New {111}〈110〉 grains are nucleated within deformed {111}〈112〉 grains and new {111}〈112〉 grains originate in the deformed {111}〈110〉 grains.     

The assisting and stabilizing role played by ω phase during the {112} <111>β twinning in Ti-Mo alloys:A first-principles insight

The ω phase is commonly observed in β-Ti alloys and plays a significant role on various properties of β-Ti alloys.Although many results about the role ofω phase on mechanical properties of β-Ti alloys have been derived from theoretical and experimental studies,the role ofω phase on deformation mechanism hitherto remains elusive and deserves to be further studied.In this work,the role played by ω phase during the {112 } <111>β twinning in Ti-Mo alloys were investigated by first-principles calculations at atomic scale.In the energy favorable interface of(112)β/(10(1)0)ω,we found that partial dislocations slipping on the successive (10(1)0)ω planes ofω phase can lead to the formation of { 112} <111>β twin nucleus.And the twin nucleus grows inwards ω grain interior through atomic shuffle.Thus,a new twinning mechanism of {112 } <111>β assisted by ω phase was proposed.Furthermore,our calculations indicated that the Pearance of ITB (interfacial twin boundary) ω phase can improve the stability of the symmetrical 12 } <111 >β twin boundary (TB),which can well explain the experimental phenomenon that the ITB ω phase always accompanies the formation of {112 } <111>β twin.Finally,a probable microstructure evolution sequence was suggested,namely β matrix → β matrix + athermal ω phase → (112)[11(1)]twin → (112)[11(1)]β twin + ITB ω phase.Our calculations provide new insights on the role played by ω phase during the twinning process of {112} <111>β,which can deepen the understanding on the deformation behaviors of β-Ti alloys.     

残余碳对取向硅钢初次和二次再结晶的影响

研究了脱碳退火样品中的残余碳对取向硅钢初次和二次再结晶的组织和磁性能的影响。结果表明：随着脱碳退火样品中残余碳含量的提高,初次再结晶的平均晶粒尺寸减小,表层和中心层的晶粒尺寸差增大;初次再结晶的强{111}<110>或{111}<112>织构向强{112}<110>织构转变,部分1/4层的Goss晶粒或{111}<112>晶粒转变为其他取向的晶粒;残余碳含量超过0.0200%后,高温退火样品二次再结晶不完善,磁性能较差。相变是导致上述现象的主要原因。     

薄规格取向硅钢中晶粒取向和尺寸对Goss晶粒异常长大的影响

利用EBSD技术统计了薄规格取向硅钢片中初次再结晶和二次再结晶前期组织中{411}〈148〉、{111}〈112〉、{100}〈025〉取向晶粒尺寸分布,分析了三种不同取向的晶粒对Goss晶粒异常长大的影响。结果表明:初次再结晶组织中不同的取向晶粒对应的平均晶粒尺寸(d)存在差异,{411}〈148〉取向晶粒的平均尺寸最大,其次为{100}〈025〉取向晶粒,{111}〈112〉取向晶粒的平均尺寸最小。Goss取向晶粒异常长大的过程中优先吞噬{111}〈112〉取向晶粒,其次是{411}〈148〉取向晶粒,最后是近{100}〈025〉取向晶粒和近黄铜取向晶粒。{111}〈112〉、{411}〈148〉取向晶粒对Goss取向晶粒异常长大的影响主要体现在二次再结晶的前期。因此,可以推断取向硅钢中最终残留的"岛晶"可能来源于近黄铜取向晶粒或近{100}〈025〉取向晶粒。     

High magnetic field effect on texture and grain growth of GNO silicon steel

Magnetic annealing at 800 °C for 3, 15 and 30 minutes was conducted to evaluate the effect of a 17T magnetic field on the microstructure formation of cold rolled Fe‐0.75 %Si samples. According to texture measurements magnetic field did not seem to significantly affect the development of grains with Goss orientation, however it showed to affect the nucleation and growth process of {001}, {110} and {111} grains by increasing the volume fraction of the η fiber and by decreasing the fraction of the alfa and gamma fibers. ESEM/OIM and optical microscope results indicate that although magnetic field may retard nucleation it also promotes grain boundary displacement and for longer annealing times the retardation effect is compensated by the magnetic filed driving force.     

Orientation Dependence of Stress Rupture Properties of a Ni-based Single Crystal Superalloy at 760℃

The orientation dependence of creep rupture lives of a single crystal superalloy at 760℃/760 MPa was investigated.The orientations of the specimens tested were about 30°away from [001].The results showed that specimens with orientations on the [001]-[011] boundary had the longest rupture life.The deformation of these specimen were controlled by a/2110 slip and a few stacking faults with two orientations were observed.On the other hand,specimens with orientations near the [001]-[011] boundary or on the [001]-[111] boundary showed short rupture lives,and stacking faults with single orientation were observed in these specimens.The rupture properties and the deformation mechanisms were discussed based on the dislocation pattern and the calculated Schmid factors for different specimens.     

Superplasticity and grain boundary sliding in rolled AZ91 magnesium alloy at high strain rates

The superplastic deformation characteristics and microstructure evolution of the rolled AZ91 magnesium alloys at temperatures ranging from 623 to 698 K (0.67–0.76 T_m) and at the high strain rates ranging from 10⁻³ to 1 s⁻¹ were investigated with the methods of OM, SEM and TEM. An excellent superplasticity with the maximum elongation to failure of 455% was obtained at 623 K and the strain rate of 10⁻³ s⁻¹ in the rolled AZ91 magnesium alloys and its strain rate sensitivity m is high, up to 0.64. The dominant deformation mechanism in high strain rate superplasticity is still grain boundary sliding (GBS), which was studied systematically in this study. The dislocation creep controlled by grain boundary diffusion was considered the main accommodation mechanism, which was observed in this study.     

锻态TB6钛合金β相区压缩变形行为和动态再结晶

使用圆柱形试样在Thermecmaster-Z型热模拟试验机上进行锻态TB6钛合金β相区的热压缩实验(变形温度950~1100℃,应变速率0.001~1 s^-1),研究了合金的高温压缩变形和动态再结晶行为。结果表明,这种合金在β相区的变形激活能为246.7 kJ/mol,其热变形机制是动态再结晶,动态再结晶新晶粒的主要形核机制是弓弯形核。当应变速率为0.01~0.1 s^-1、变形温度为<1000℃时动态再结晶的发展比较充分,变形组织明显细化;当变形温度高于1000℃、应变速率低于0.001 s^-1时,动态再结晶的晶粒明显粗化。在动态再结晶的晶粒尺寸D与Z参数之间存在着相关性,其函数关系为D=6.44×10²·Z^-0.1628。     

TiO2和O-Al2O3晶体的生长习性

通过水热法制备粉体的实验观察到金红石、锐钛矿和α-Al2O3晶体的生长习性．采用配位多面体生长习性法则合理地解释了Ti O2和α-Al2O3的生长习性．其主要结果为α-Al2O3晶体的生长习性为平板{0001}，其各晶面的生长速度为：V｛0001 }＜V｛1123}；锐钛矿的生长习性为四面体，其各晶面的生长速度为V<010>=V<001>>V<010>>V<111>．而PBC理论很难合理地解释α-Al2 O3晶体的生长习性．