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GH4169G高温合金车削切削力与切削温度有限元仿真研究 被引量:2
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作者 牛湛皓 史耀耀 +2 位作者 黄新春 宋艺辉 樊昱昌 《工具技术》 北大核心 2024年第1期95-100,共6页
为研究GH4169G高温合金车削用量及刀具几何特性对切削力和切削温度的影响规律,基于ABAQUS有限元仿真软件,通过依次改变切削深度、切削速度和刀具几何角度,获得不同参数组合下切削力和切削温度的变化规律,进一步揭示车削参数和刀具几何... 为研究GH4169G高温合金车削用量及刀具几何特性对切削力和切削温度的影响规律,基于ABAQUS有限元仿真软件,通过依次改变切削深度、切削速度和刀具几何角度,获得不同参数组合下切削力和切削温度的变化规律,进一步揭示车削参数和刀具几何角度对GH4169G高温合金切削过程中热—力耦合作用的影响机理,从而对切削工艺参数和刀具特性进行优选。 展开更多
关键词 gh4169g高温合金 车削 有限元仿真 切削力 切削温度
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Detection and analysis of basic variables during linear friction welding of GH4169 superalloy 被引量:2
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作者 马铁军 汤化伟 +1 位作者 李文亚 张勇 《China Welding》 EI CAS 2012年第2期13-16,共4页
By monitoring the line voltage and current of the driving motor during linear friction welding ( LFW) of GH4169 superalloy, the frictional power of the rubbing interface between two components to be joined was detec... By monitoring the line voltage and current of the driving motor during linear friction welding ( LFW) of GH4169 superalloy, the frictional power of the rubbing interface between two components to be joined was detected. The data was recorded by a data acquisition card and processed by the LabVIEW software. By analyzing the evolution of frictional power, the joint formation mechanism was discussed. The curves of the measured basic variables (frictional power, axial shortening, interfacial temperature and axial pressure) reflected the characteristics of the LFW process and offered an effective way for welding parameter optimization. 展开更多
关键词 linear friction welding frictional power gh4169 superalloy
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SUPERPLASTIC FORMING AND AP-PLICATION OF GH4169 SUPERALLOY 被引量:1
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作者 LuHongjun YaoCaogen 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2003年第1期62-63,67,共3页
The superplastic forming and application of GH4169 superalloy are studied. It is shown that for the typical superplastic forming strain rates of 10- 3 s 1 to 10- 4 s -1, the available engineering strains of the fine-g... The superplastic forming and application of GH4169 superalloy are studied. It is shown that for the typical superplastic forming strain rates of 10- 3 s 1 to 10- 4 s -1, the available engineering strains of the fine-grain GH4169 superalloy are always higher than 250% within wide temperature scopes (920 -980℃), and the maximum elongation to failure obtained is 513%. Dynamic grain growth is presented during superplastic deforming for the alloy, and the grain becomes larger with the increase of the strain. A GH4169 fuel manifold of an aerocraft is superplastically formed, and the superplastically formed GH4169 mainfold is tested by 30 MPa hydraulic pressure for 10 min. So some GH4169 alloy complex components can be superplastically formed in the aerospace industry to decrease the costs of fabricating these components. 展开更多
关键词 superalloy gh4169 Superplastic forming Application
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Stress Relaxation Behavior of GH4169 Superalloy
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作者 常鹏鹏 孔永华 +2 位作者 陈国胜 谢黎雄 朱世根 《Journal of Donghua University(English Edition)》 EI CAS 2015年第1期58-61,共4页
GH4169 superalloy stress relaxation test was investigated to study its characteristics of stress relaxation curves at various temperatures( 550,650,and 750 ℃). These curves presented jointly two distinct stages,the s... GH4169 superalloy stress relaxation test was investigated to study its characteristics of stress relaxation curves at various temperatures( 550,650,and 750 ℃). These curves presented jointly two distinct stages,the stage of inner stress relaxing quickly,and the stage of inner stress relaxing slowly and closing to the stress relaxation limit. And these curves obtained could be fitted by second order exponential decay function well. Based on the experimental stress relaxation curves,the relationship between stress relaxation rate and time were derived, which showed that the higher relaxation temperature and the greater initial rate of stress relaxation. The whole process presented two different stages,the stage of stress relaxation rate falling rapidly and the stage of stress relaxation rate slowing down and tending to be constant. The relation curve between creep strain rate and stress of GH4169 superalloy can be divided into three stages,low stress stage,transition stage,and high stress stage.Both the high stage and the low stage present linear correlation. 展开更多
关键词 gh4169 superalloy stress relaxation experiment second order exponential decay function
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热处理制度对GH4169G合金微观组织与蠕变性能的影响 被引量:9
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作者 田素贵 王欣 +1 位作者 刘臣 孙文儒 《中国有色金属学报》 EI CAS CSCD 北大核心 2013年第1期108-115,共8页
对等温锻造GH4169G合金进行不同条件热处理和蠕变性能测试,研究热处理制度对合金组织与蠕变性能的影响。结果表明:经直接时效和标准热处理后,ITF-GH4169G合金中的δ相具有粒状或针状形态,其中,标准热处理期间合金中元素Fe和Cr富集于近... 对等温锻造GH4169G合金进行不同条件热处理和蠕变性能测试,研究热处理制度对合金组织与蠕变性能的影响。结果表明:经直接时效和标准热处理后,ITF-GH4169G合金中的δ相具有粒状或针状形态,其中,标准热处理期间合金中元素Fe和Cr富集于近晶界区域。与标准热处理合金相比,直接时效态合金在蠕变期间晶内发生位错的单取向或双取向滑移,可减缓应力集中、延迟裂纹的萌生与扩展。而标准热处理态合金中形成的针状δ相可削弱晶界的结合强度,并促使晶界处发生裂纹的萌生与扩展。 展开更多
关键词 gh4169g合金 热处理制度 微观组织 针状δ相 蠕变
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一种GH4169G合金的组织与蠕变行为 被引量:5
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作者 刘姣 李振荣 +2 位作者 王欣 田素贵 孙文儒 《材料热处理学报》 EI CAS CSCD 北大核心 2013年第8期74-79,共6页
通过对等温锻造GH4169G合金进行直接时效处理、蠕变性能测试和组织形貌观察,研究了GH4169G合金的组织结构及蠕变行为。结果表明:经等温锻造和直接时效后,GH4169G合金晶粒具有不均匀特征,且在晶内存在孪晶,并有粒状δ相在晶内及沿晶界不... 通过对等温锻造GH4169G合金进行直接时效处理、蠕变性能测试和组织形貌观察,研究了GH4169G合金的组织结构及蠕变行为。结果表明:经等温锻造和直接时效后,GH4169G合金晶粒具有不均匀特征,且在晶内存在孪晶,并有粒状δ相在晶内及沿晶界不连续析出,可改善晶界的结合强度。经不同条件蠕变性能测试后,根据稳态蠕变期间的应变速率,测定出合金在稳态期间的蠕变激活能和应力指数分别为Q=532.7 kJ/mol和n=12.1。合金在蠕变期间的变形特征是不同取向的孪晶变形和位错滑移,随蠕变进行,形变位错密度增加,且在晶界附近发生位错堆积,并产生应力集中,致使微裂纹在晶界处萌生及扩展,直至蠕变后期发生沿晶断裂。 展开更多
关键词 gh4169g合金 组织结构 蠕变 变形机制
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热处理工艺对GH4169G合金组织与性能的影响
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作者 刘臣 田素贵 +2 位作者 曾征 张超 孙文儒 《材料科学》 2012年第2期72-76,共5页
通过对等温锻造GH4169G进行不同工艺的热处理和组织形貌观察,研究了热处理工艺对合金组织与蠕变性能的影响。结果表明,GH4169G合金经直接时效处理后的组织结构由γ基体、γ'、γ''?及δ相组成,且晶粒尺寸约为10 μm^15 μm... 通过对等温锻造GH4169G进行不同工艺的热处理和组织形貌观察,研究了热处理工艺对合金组织与蠕变性能的影响。结果表明,GH4169G合金经直接时效处理后的组织结构由γ基体、γ'、γ''?及δ相组成,且晶粒尺寸约为10 μm^15 μm,并存在较多孪晶组织,其中,粒状δ相分布于晶内,而大量细小γ'和γ''强化相在晶内弥散析出,是使合金具有较好蠕变性能的主要原因。与直接时效处理合金相比,经标准热处理后,合金的晶粒尺寸无明显变化,组织结构仍由γ基体、γ'、γ''及δ相组成,但孪晶数量明显减少,且有块状和针状δ相沿晶界不连续析出,其中,元素Fe、Cr富集于近晶界区域,是使其δ相具有针状形态的主要原因。 展开更多
关键词 gh4169g合金 直接时效 标准热处理 组织结构
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晶粒组织对GH4169G合金持久性能的影响 被引量:4
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作者 朱丽娜 李文 +1 位作者 祁峰 孙文儒 《热加工工艺》 CSCD 北大核心 2011年第16期47-49,共3页
研究了GH4169G合金锻造饼坯表层不完全再结晶组织和中间层完全再结晶组织对持久性能的影响。研究结果表明,在标准热处理状态下,具有混晶组织的表层合金比具有等轴晶组织的中间层合金持久性能差,δ相的析出数量、分布情况及晶粒组织变形... 研究了GH4169G合金锻造饼坯表层不完全再结晶组织和中间层完全再结晶组织对持久性能的影响。研究结果表明,在标准热处理状态下,具有混晶组织的表层合金比具有等轴晶组织的中间层合金持久性能差,δ相的析出数量、分布情况及晶粒组织变形协调能力是影响持久性能的主要原因。 展开更多
关键词 gh4169g合金 晶粒组织 Δ相 持久性能
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航空涡轮盘用GH4169G合金研制 被引量:7
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作者 王庆增 陈国胜 孙文儒 《宝钢技术》 CAS 2013年第2期37-42,共6页
目前应用最广泛的航空涡轮盘材料是IN718合金,提高IN718合金的组织稳定性和持久寿命对航空发动机的使用尤为重要。试验研究发现,添加适量的P、B可有效提高IN718合金的持久寿命,但添加P、B的IN718合金材料工业化生产和应用方面的报道很... 目前应用最广泛的航空涡轮盘材料是IN718合金,提高IN718合金的组织稳定性和持久寿命对航空发动机的使用尤为重要。试验研究发现,添加适量的P、B可有效提高IN718合金的持久寿命,但添加P、B的IN718合金材料工业化生产和应用方面的报道很少。采用金相观察、力学性能测试等手段,研究了GH4169G合金的组织与性能。对比分析了P、B微量元素不同添加量对GH4169G合金力学性能的影响。试验结果表明,GH4169G合金的热加工工艺性能良好;与普通IN718合金相比,GH4169G合金的持久寿命提高3倍以上。 展开更多
关键词 gh4169g IN718 涡轮盘 微合金化
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GH4169G合金均匀化过程δ相的析出变化 被引量:3
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作者 杨国良 李晓桥 《热加工工艺》 CSCD 北大核心 2011年第14期170-172,188,共4页
在研究GH4169G合金准120mm铸锭均匀化制度基础上,介绍了验证合金均匀化效果的三种方法。分析铸态组织后,将试样进行不同程度的均匀化处理。通过文献结合实验确定δ相验证制度为910℃×14 h,AC。合金偏析严重时,δ相呈长针状分布... 在研究GH4169G合金准120mm铸锭均匀化制度基础上,介绍了验证合金均匀化效果的三种方法。分析铸态组织后,将试样进行不同程度的均匀化处理。通过文献结合实验确定δ相验证制度为910℃×14 h,AC。合金偏析严重时,δ相呈长针状分布在枝晶间,枝晶轴未析出区比例较大;合金均匀化改善时,枝晶间δ相析出面积增大,聚集程度降低,且针状相的长度减少过渡到棒状。均匀化程度更高时,枝晶轴基本上都有δ相析出,析出相呈棒状与粒状分布,主要差别在于枝晶轴/枝晶间析出量多少及部分区域聚集析出。完全均匀化,δ相呈粒状在晶粒内均匀析出,晶界仍有针状δ相析出。 展开更多
关键词 gh4169g合金 均匀化 δ相变化
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GH4169G合金高强涡轮盘锻件的试制 被引量:4
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作者 罗恒军 谢静 +3 位作者 廖佳 孙文儒 张伟红 信昕 《大型铸锻件》 2013年第3期47-48,共2页
以GH4169G高强涡轮盘为研究对象,在工业条件下成功试制出组织和性能满足技术标准要求的锻件。
关键词 gh4169g合金 高强涡轮盘 金相组织 力学性能
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Microstructure and homogenization process of as-cast GH4169D alloy for novel turbine disk 被引量:9
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作者 Kai Chen Shu-yuan Rui +2 位作者 Fa Wang Jian-xin Dong Zhi-hao Yao 《International Journal of Minerals,Metallurgy and Materials》 SCIE EI CAS CSCD 2019年第7期889-900,共12页
To investigate the microstructure, segregation, and suitable homogenization process of as-cast GH4169D alloy, the microstructure, elements segregation, and precipitates of cast GH4169D ingots prepared by vacuum induct... To investigate the microstructure, segregation, and suitable homogenization process of as-cast GH4169D alloy, the microstructure, elements segregation, and precipitates of cast GH4169D ingots prepared by vacuum induction melting (VIM) and vacuum arc remelting (VAR) were observed by optical microscopy (OM), scanning electron microscopy, and energy-dispersive X-ray spectroscopy (EDS). According to the residual segregation model and simulation results of DICTRA thermodynamic software, the homogenization temperature and time range were set as 1120–1170°C and 5–20 h, respectively. The experimental results showed that microscopic dendrite and element segregation occurred in the interior of ingots and the main segregation elements were Nb and Ti. In addition, the precipitates were mainly distributed in interdendritic regions and were composed of NbC, Laves,γ′, and δ phases. The homogenization process suggested that the interdendritic detrimental precipitated Laves phase can be eliminated or redissolved after homogenization at 1150°C for 20 h, suggesting it was the most suitable homogenization treatment. Thermal compression test results showed that the GH4169D alloys after homogenization treatment had no cracks and dynamic recrystallization occurred, with recrystallization volume fraction increasing with temperature, indicating a good working plasticity at temperatures from 1050 to 1200°C. 展开更多
关键词 gh4169D superalloy AS-CAST MICROSTRUCTURE SEgREgATION HOMOgENIZATION thermal DEFORMATION
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Creep rupture properties and microstructure stability of the GH984G alloy tube
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作者 WANG Tingting XU Songqian 《Baosteel Technical Research》 CAS 2024年第1期43-48,共6页
GH984G alloy is a significant candidate material for 650-700℃ ultra-supercritical coal-fired generating units.In this paper,creep rupture properties and microstructure stability of the GH984G alloy tube were studied,... GH984G alloy is a significant candidate material for 650-700℃ ultra-supercritical coal-fired generating units.In this paper,creep rupture properties and microstructure stability of the GH984G alloy tube were studied,and the findings indicated excellent creep rupture properties at 700℃.Furthermore,the extrapolated strength for 100000 h was found to be 153.8 MPa,which satisfies the requirements for the long-term performance of high-temperature materials in power stations.Aging at 700℃ with the extension of time,the grain boundary carbides and the particle size of the γ′phase on the matrix gradually coarsen,but its spherical morphology remains uniformly distributed.However,no harmful phase precipitates were found even after aging at 700℃ for up to 19144 h.Excellent microstructure stability guarantees the 700℃ creep rupture properties of the GH984G alloy tube. 展开更多
关键词 gh984g alloy tube nickel-iron-based superalloy stress-rupture properties microstructure stability
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GH4169G合金高压后挡板锻件组织性能研究 被引量:2
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作者 赵刚 邓娟 +1 位作者 全琼蕊 王艳 《热加工工艺》 北大核心 2022年第11期52-54,59,共4页
某发动机用GH4169G变形高温合金高压后挡板锻件高温光滑持久性、缺口周期持久性及晶粒度未达到技术要求。为了探明锻件组织性能不合格的原因,对某批次后挡板缺口周期持久性不合格试样尺寸进行了检测和分析,对缺口周期持久性不合格试样... 某发动机用GH4169G变形高温合金高压后挡板锻件高温光滑持久性、缺口周期持久性及晶粒度未达到技术要求。为了探明锻件组织性能不合格的原因,对某批次后挡板缺口周期持久性不合格试样尺寸进行了检测和分析,对缺口周期持久性不合格试样断口附近高倍组织进行了检测,对锻件全截面高倍组织进行了检测分析。结果表明:GH4169G合金缺口周期持久性能对缺口非常敏感,缺口的半径大小对性能有很大影响,试样缺口半径小是该批锻件缺口周期持久性能不合格主要原因;高压后挡板锻件局部存在变形混晶组织并且大晶粒晶界处δ相贫化,这是高温持久性能不合格的原因。 展开更多
关键词 gh4169g高温合金 高压后挡板锻件 晶粒度 缺口周期持久性
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GH4169G合金零件异常腐蚀区缺陷分析 被引量:2
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作者 刘巧沐 黄顺洲 +2 位作者 陈玉龙 王春健 裴会平 《燃气涡轮试验与研究》 北大核心 2019年第1期52-56,共5页
针对生产中GH4169G合金零件低倍全面腐蚀时出现的异常腐蚀区,采用光学显微镜、扫描电子显微镜及能量散射谱,对正常区域和异常腐蚀区的宏观、微观组织形貌及化学成分进行了对比分析。结果表明,异常腐蚀区为白斑缺陷;虽然该异常腐蚀区离... 针对生产中GH4169G合金零件低倍全面腐蚀时出现的异常腐蚀区,采用光学显微镜、扫描电子显微镜及能量散射谱,对正常区域和异常腐蚀区的宏观、微观组织形貌及化学成分进行了对比分析。结果表明,异常腐蚀区为白斑缺陷;虽然该异常腐蚀区离散分布着富Ca和富Mg的氧化物颗粒,但氧化物颗粒未见聚集,由此判断该缺陷为"干净"白斑。强度类比评估表明,带白斑缺陷零件可满足阶段性试验要求,且试验后分解检查未发现零件异常。 展开更多
关键词 航空发动机 gh4169g合金 异常腐蚀区 显微组织 白斑 氧化物颗粒
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GH4169G低压涡轮盘“脏白斑”水浸超声C扫检测分析 被引量:1
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作者 李玲 张运 +3 位作者 黄志新 张策 张倩兰 李欣 《中国新技术新产品》 2022年第24期1-4,共4页
在加工过程中对某低压涡轮盘进行腐蚀检查,在盘径向距圆周45 mm处发现1块长条亮腐蚀区(尺寸约为12 mm×3 mm),经外观检查、金相分析和能谱分析,最终判定该表面腐蚀可见的浅腐蚀区域为贫Nb偏析产生的白斑,宏观尺寸和微观晶粒度均不... 在加工过程中对某低压涡轮盘进行腐蚀检查,在盘径向距圆周45 mm处发现1块长条亮腐蚀区(尺寸约为12 mm×3 mm),经外观检查、金相分析和能谱分析,最终判定该表面腐蚀可见的浅腐蚀区域为贫Nb偏析产生的白斑,宏观尺寸和微观晶粒度均不符合标准要求。同时,白斑附近有碳化物聚集,其中夹杂少量Mg、Al氧化物。针对该情况,该文分析了腐蚀前该低压涡轮盘的超声检测结果,从理论上分析了“白斑”和“脏白斑”超声检测的可能性,并结合理论和实践探讨了GH4169/GH4169G水浸超声检测的主要工艺参数,对保证GH4169/GH4169G盘内部质量具有一定指导意义。 展开更多
关键词 gh4169/gh4169g 低压涡轮盘 水浸超声C扫检测 “白斑” 夹杂物
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Research on GH4169G alloy for aerospace turbine disk
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作者 WANG Qingzeng~(1)),CHEN Guosheng~(1)),SUN Wenru~(2)),LIU Fengjun~(1)), WANG Zixin~(1)) and LIU Fang~(2)) 1) Special Steel Business Unit,Baoshan Iron & Steel Co.,Ltd.,Shanghai 200940,China 2) Institute of Metal Research,Chinese Academy of Sciences,Shenyang 110016,China 《Baosteel Technical Research》 CAS 2010年第S1期90-,共1页
Using metallographic observation and mechanical measurement,the microstructure and mechanical properties of GH4169G alloy has been investigated.The effect of the phosphorus,boron trace elements on mechanical propertie... Using metallographic observation and mechanical measurement,the microstructure and mechanical properties of GH4169G alloy has been investigated.The effect of the phosphorus,boron trace elements on mechanical properties of the GH4169G alloy are compared and analyzed.The results showed that the hot-workability of the GH4169G alloy is very good.The stress ruptures properties of GH4169G alloy is over 3 times than the traditional GH4169 alloy. 展开更多
关键词 gh4169g Inconel 718 turbine disk PHOSPHORUS BORON Micro-alloying
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GH4169G合金叶盘叶尖裂纹失效分析
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作者 李祚军 白云瑞 +1 位作者 吴晨 田伟 《燃气涡轮试验与研究》 北大核心 2020年第5期54-58,共5页
针对GH4169G合金叶盘试验后1个叶片叶尖出现的裂纹,对裂纹叶片进行了断口和组织分析。得出裂纹的性质为高周疲劳,裂纹源区位于叶背侧亚表面,裂纹叶片叶尖处晶粒度为5.5级,不满足锻件检测要求,降低了高周疲劳性能。对与裂纹叶片邻近的多... 针对GH4169G合金叶盘试验后1个叶片叶尖出现的裂纹,对裂纹叶片进行了断口和组织分析。得出裂纹的性质为高周疲劳,裂纹源区位于叶背侧亚表面,裂纹叶片叶尖处晶粒度为5.5级,不满足锻件检测要求,降低了高周疲劳性能。对与裂纹叶片邻近的多个叶片各部位进行组织分析,叶尖处均未达到平均晶粒度8级或更细的要求,δ相较少,距离裂纹叶片越远晶粒越细,叶身纵向晶粒从叶尖至叶根逐渐变细。复查该叶盘锻件的等温锻造工艺,叶片部位欠压过多,外缘周向最小尺寸偏小,导致叶片叶尖附近部位变形量不足,晶粒粗大。对锻造工艺进行优化,将最大锻造压力由5 000 t调整为8 000 t,预留欠压量由≤15 mm调整至≤10 mm。优化后的锻件充满模具,外缘尺寸符合锻件图纸要求,晶粒度符合技术要求,后续各批次中该问题未复现。 展开更多
关键词 gh4169g合金 叶片裂纹 失效分析 高周疲劳 晶粒度 等温锻造
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Effect of linear friction welding process on microstructure evolution,mechanical properties and corrosion behavior of GH4169 superalloy
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作者 Yu SU Xiawei YANG +5 位作者 Tingxi MENG Dong WU Rui XU Haiyu XU Wenya LI Shuo YIN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第6期504-520,共17页
Linear Friction Welding(LFW)technology was used to realize the welding of GH4169 superalloy,and the effect of welding parameters on the microstructure,mechanical properties and corrosion behavior of the joint was anal... Linear Friction Welding(LFW)technology was used to realize the welding of GH4169 superalloy,and the effect of welding parameters on the microstructure,mechanical properties and corrosion behavior of the joint was analyzed.The results show that there is a positive correlation between the weld hardness and the tensile strength.With the gradual increase of heat input and welding pressure,the joint quality is gradually improved,but the heat affected zone is not significantly increased.The smaller the grain size of the weld,the higher the strength and plasticity of the joint.With the increase of the joint shortening amount,the corrosion resistance of the weld first gradually increases.However,when the shortening reaches a certain level,the corrosion resistance of the joint becomes little changed.With the increase of solution temperature,the corrosion current density increases and the polarization impedance decreases.The higher the corrosion temperature,the worse the corrosion resistance of the joint.There is no significant correlation between the joint strength and the corrosion resistance.The corrosion resistance of the joint can be enhanced without changing the joint mechanical properties by reducing the welding frequency and amplitude or increasing the welding pressure. 展开更多
关键词 Linear Friction Welding(LFW) gh4169 superalloy MICROSTRUCTURE Mechanical properties Corrosion behavior
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Formation mechanism of large grains inside annealed microstructure of GH4169 superalloy by cellular automation method 被引量:12
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作者 Ming-Song Chen Zong-Huai Zou +2 位作者 Y.C.Lin Hong-Bin Li Guan-Qiang Wang 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2019年第7期1403-1411,共9页
In authors’ previous work [Mater. Charact. 141 (2018) 212-222]. it was found that the heterogeneous deformed microstructures can be replaced by the relatively homogeneous recrystallized grains through an annealing tr... In authors’ previous work [Mater. Charact. 141 (2018) 212-222]. it was found that the heterogeneous deformed microstructures can be replaced by the relatively homogeneous recrystallized grains through an annealing treatment. However, there are still some relatively large recrystallized grains. To find the reasons for the formation of large grains, some new annealing treatment tests were done, and the cellular automation (CA) simulations were carried out in the present work. The experimental results showed that the microstructural evolution during annealing treatment is significantly affected by the content of S phase. So. the effects of δ phase on the nucleation and growth of grains are carefully considered in the CA model to accurately simulate the microstructural evolution behavior. By the CA simulation, it is found that the dislocation density rapidly decreases due to the nucleation of static recrystallization (SRX) and the growth of dynamc recrystallization (DRX) nuclei at the early stage of annealing. The high initial dislocation density provide the high velocity for the growth of DRX nuclei, which is responsible for the formation of coarse grains, However, the growth rate of SRX nuclei is relatively small due to the low dislocation density and pinning effects of δ phase. 展开更多
关键词 gh4169 superalloy Cellular automation model Coarse grains ANNEALINg treatment RECRYSTALLIZATION behavior
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