丁智平王腾飞李明陈吉平
材料研究学报
在680和850℃下对DD3镍基单晶合金进行多轴非比例加载低周疲劳试验, 结果表明等效应变范围Δεe、试验温度、等效应力范围Δσe对单晶合金的低周疲劳寿命有显著影响。基于能量耗散理论, 引入参量k表征多轴非比例加载对疲劳寿命的影响, 构造循环塑性应变能作为损伤参量, 建立镍基单晶合金低周疲劳寿命预测模型。参量k与循环寿命之间呈幂函数关系。根据镍基单晶合金的微观尺度结构特征, 建立γ/γ'双相单胞有限元模型, 进行多轴非比例循环加载应力应变数值模拟。根据宏观有限元模型和γ/γ'双相单胞微观有限元模型的计算结果, 以及镍基单晶合金680和850℃低周疲劳试验数据, 对疲劳寿命模型进行多元线性回归分析, 结果表明微观单胞有限元模型的分析精度比宏观有限元模型显著提高,两种温度下的试验数据分别落在1.6倍和2.0倍偏差分布带内。
关键词:
金属材料
,
low cycle fatigue
,
single crystal superalloy
,
multiaxial non-proportional loading
,
unit cell model
,
life prediction
Chengbao Liu Jian Shen Jian Zhang Langhong Lou
材料科学技术（英文）
A nickel base single crystal (SC) superalloy was directionally solidified using liquid metal cooling (LMC) process at various withdrawal rates. The microstructure was refined as increasing the withdrawal rate from 3 to 12 mm/min. However, higher withdrawal rate of 15 mm/min induced the formation of stray grains. Size and volume fraction of the eutectics were found to decrease with the increasing in withdrawal rate. After solution heat treatment at 1250°C, un-dissolved eutectic was observed in specimens. High temperature creep rupture life was observed to be very sensitive to the fraction of these remaining eutectics. Creep rupture tests at 1000°C/235 MPa showed that refined microstructure and low fraction of the remaining eutectic lead to significant improvement of the rupture life.
关键词:
Eutectic
,
single crystal superalloy
,
liquid-metal-cooling
,
withdrawal rate
Y.S. Yang
,
X.H. Feng
,
G.F. Cheng
,
Y.J. Li
,
Z.Q. Hu
金属学报(英文版)
The crystal growth of a nickel-based single crystal superalloy DD3 was researched via controlled directional solidification under the action of a DC electric field. The cellular or dendrite spacing of the single crystal superalloy is refined and microsegregation of alloying elements Al, Ti, Mo and W, is reduced by the electric field. The electric field decreases the interface stability and reduces the critical growth rate of the cellular-dendritic translation because of Thomson effect and Joule heating. The precipitation of the γ' phase is more uniform and the size of the γ' phase is smaller with the electric field than that without the electric field.
关键词:
single crystal superalloy
,
null
D.H.Kim
金属学报(英文版)
Carbon and boron have been considered to strengthen grain boundaries that might form during single crystal casting. In this study the effect of boron on solidification behavior and creep properties of the carbon doped single crystal RR 2072 has been investigated. In order to understand solidification behavior with boron addition, the solid/liquid interface morphology and solidification microstructare were examined with solidification rate. The relationship between microstructaral evolution and creep properties of the carbon and boron modified single crystal has been also investigated.
关键词:
single crystal superalloy
,
null
,
null
Author C.D. Zhou1
,
2)
,
J.X. Yu1)
,
X.P. Dong1)
,
Y.H. Zhang1)
,
C.Q. Sun3) and T.F. Li4) 1) The State Education Commission Open Research Laboratory for High Temperature Materials and Testing
,
Shanghai Jiao Tong University
,
Shanghai 200030
,
China2) Shanghai Enhanced Lab of Ferrometallurgy
,
Shanghai University
,
Shanghai 200072
,
China3) Institute of Aeronautical Materials
,
Beijing 100095
,
China 4) Institute of Corrosion and Protection of Metals
,
The Chinese Academy of Sciences
,
Shenyang 110015
,
ChinaManuscript received 18 October 1998
金属学报(英文版)
An investigation has been made on the tensile fracture behavior of oriented single crystal DD100 superalloy at 850. The appearance of the fracture surface of DD100 reflects the glide plane decohension fracture mechanism, which is different from the fracture of oriented DD100. The tensile strength and elongation are lower than the oriented DD100. Oxygen in air has little effect on the strength of DD100 but reduces the tensile elongation obviously. Oxygen does not affect the fracture mode of DD100 but strongly accelerates the process of fracture.
关键词:
single crystal superalloy
,
null
,
null
熊继春李嘉荣赵金乾刘世忠董建新
金属学报
对单晶高温合金DD6进行表面吹砂处理, 然后进行固溶与时效真空热处理, 采用SEM, TEM, EPMA和Thermo-Calc的方法研究了单晶合金DD6再结晶晶界析出相的特征及其形成机制. 结果表明, 经过吹砂处理的DD6合金在固溶与时效热处理过程中发生再结晶. 再结晶晶界出现析出相, 分析表明析出相为M6C碳化物, 该碳化物呈粒状析出, 尺寸约为0.5 μm, 数量极少, 富含W, Re和 Mo, 且Cr, Nb和Co的含量与合金名义成分差别不大, 而Al, Ta和Ni含量较低. 由于再结晶晶界上C元素的聚集效应, C原子在晶界上达到一定浓度后即与一定数量的W, Mo等μ相形成元素发生相变反应, 抑制了合金析出μ相的倾向. 又因为DD6合金W含量较高, 而Cr含量较低, 抑制了M23C6碳化物, 有利于析出M6C碳化物.
关键词:
单晶高温合金
,
DD6
,
recrystallization
,
precipitate
史振学
,
刘世忠
,
李嘉荣
材料热处理学报
在真空定向凝固炉中采用螺旋选晶法制备了一种镍基单晶高温合金,固溶处理后分别采用1080、1120、1160和1200℃不同的温度进行一次时效,然后在相同工艺下进行二次时效,研究一次时效温度对合金组织和1100℃/140 MPa条件下持久性能的影响.研究表明,随一次时效温度升高,γ'相的尺寸增大,体积分数先增加后减少,在较高温度时效后γ基体通道中有细小的二次γ'相析出,立方化程度先增加后因在1200℃下时效后有部分γ '/γ相界面变为锯齿状而降低.随着一次时效温度提高,合金的持久寿命先增加后降低,在1200℃下时效后持久寿命最低.在1080、1120和1160℃时效后,γ'相在持久过程中形成了完善细密的筏排组织,而在1200℃时效后,γ '相在持久过程中形成了非常不规则的粗化组织.合金在1120℃进行一次时效,合金的组织和持久性能最佳.
关键词:
单晶高温合金
,
时效温度
,
组织
,
持久性能
谷怀鹏
,
刘丽君
,
曹腊梅
,
薛明
,
汤鑫
,
曹雪
航空材料学报
doi:10.3969/j.issn.1005-5053.2013.6.004
采用扫描电子显微镜(SEM)、电子探针(EPMA)和拉伸性能测试等手段,研究含Ru镍基单晶高温合金的显微组织、偏析行为和拉伸性能.结果表明:铸态下,Re,W强烈偏析于枝晶干而Ta,Al在枝晶间偏聚,Ru及其他元素分布趋于均匀.热处理后,Re,W偏析程度有所减轻;合金枝晶干和枝晶间处的γ’相均呈立方状,体积分数分别为63％和71％,平均尺寸分别为0.40 μm和0.54μm.拉伸性能结果表明,随着拉伸温度升高,合金抗拉强度和屈服强度先升高后降低,在760℃时达到最大值,但断后伸长率最小,为8.8％.合金在25℃,760℃和980℃下的断裂机制分别为类解理断裂、滑移分离剪切断裂和韧窝-类解理复合断裂.
关键词:
单晶高温合金
,
Ru
,
热处理
,
显微组织
,
拉伸性能
李晓红
,
叶雷
,
钟群鹏
,
曹春晓
,
毛唯
航空材料学报
doi:10.11868/j.issn.1005-5053.2015.1.001
对DD3单晶合金进行1250℃保温不同时间的TLP扩散连接研究.降温过程采取了随炉冷却和充氩快冷两种方式,随后对接头进行了870℃/32h/空冷的时效处理.分析了不同规范下的焊缝及母材的组织,同时测定了接头的980℃持久性能.结果发现:炉冷并时效处理试样的焊缝及母材中的γ’相的尺寸随着保温时间增加而增加,且形状趋于不规则.而充氩冷却并时效处理试样的焊缝及母材中的γ’相的尺寸和形状基本一致,随保温时间的增加没有明显变化,立方化较好.低的冷却速率使焊缝和母材中的γ’相粗化从而降低了接头和母材的性能,而高的冷却速率促使焊缝及母材中形成细小立方化的γ’相,不仅使接头性能明显提高,同时母材性能也没有降低.
关键词:
单晶高温合金
,
过渡液相扩散焊
,
冷却速率
,
高温持久性能
田素贵
,
李秋阳
,
郭忠革
,
薛永超
,
曾征
,
舒德龙
,
谢君
中国有色金属学报
通过对不同温度固溶处理合金枝晶干/间区域进行成分分析、蠕变性能测试及组织形貌观察,研究固溶温度对一种无Re单晶镍基合金成分偏析和蠕变行为的影响.结果表明:经不同温度固溶处理后,合金中枝晶干/间区域具有不同的偏析程度,随固溶温度提高,元素偏析程度降低,可明显提高合金的蠕变抗力和延长蠕变寿命.800℃蠕变期间,合金中γ'相仅形成串状结构,未形成完全筏状组织.合金在中温蠕变期间的变形机制是位错在基体中滑移和剪切γ '相,其中,在基体中发生大量位错的单取向、双取向滑移,可产生形变硬化作用,阻碍位错运动,加之γ/γ两相共格界面的应力场作用,可抑制位错剪切进入γ '相,是使合金在稳态蠕变期间保持较低应变速率的主要原因.
关键词:
单晶高温合金
,
成分偏析
,
固溶热处理
,
蠕变
,
变形机制
