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定向凝固高温合金晶界形貌的分形描述

孙力玲 , 董连科 , 张静华 , 胡壮麒

金属学报

用分形分析的方法定量描述了定向凝固高温合金的树枝晶晶界形貌。结果表明,随着凝固速率的提高,晶界分形维数均增大。还讨论了凝固合金系统熵与晶界分形维数之间的关系。

关键词: 高温合金 , fractal , directional solidiflcation , superalloy

GH718合金氢渗透特性的研究

徐坚 , 孙秀魁 , 刘清泉 , 陈文绣

中国腐蚀与防护学报

GH718合金氢渗透特性的研究徐坚,孙秀魁,刘清泉,陈文绣(中国科学院金属研究所,快速凝固非平衡合金国家重点实验室沈阳110015)1前言GH718(INCONEL718)合金广泛用作为涡轮叶片、氢燃发动机、核反应堆器壁等部件的材料.由于使用环境中氢气氛的存在,选材时必须考虑氢的进入与传输对合金性能的影响.尽管此合金的氢渗透数据曾有报导山,但关于合金的组织结构对氢渗透和扩散特性的影响仍不十分?...

关键词: null , hydrogen diffusion , superalloy , precipitation-phase

拉晶速率对单晶高温合金凝固析出行为及显微组织的影响

程国华 , 赵京晨 , 孙家华 , 史正兴

金属学报

研究了拉晶速率对单晶高温合金凝固界面形态、一次臂间距、(γ+γ')共晶和γ'相析出行为的影响.结果表明,随拉晶速率的增加,凝固界面从平面向胞状、粗枝、细枝转变,一次臂间距先增加然后减小,(γ+γ')共晶增多,γ'尺寸减小,立方规则性增加.胞状、枝状凝固时,γ'尺寸出现“双峰”分布.

关键词: 拉晶速率 , superalloy , single crystal , liquid/solid interface morphology , microstructure

LDZ125微晶涂层抗循环氧化性能

张捷 , 楼翰一

腐蚀学报(英文)

研究了高温合金LDZ125及其溅射微晶涂层的抗循环氧化行为.微晶涂层仅由γ相组成,晶粒尺寸约为30nm.结果表明:微晶涂层在1000℃的抗循环氧化性能比铸态合金的有极大提高.微晶层氧化时只形成单一的Al2O3氧化膜,且在整个氧化过程中未见开裂剥落,有极好的粘附性.

关键词: 溅射 , coating , microcrystal , superalloy , cyclic oxidation

一种新型定向凝固镍基高温合金抗热腐蚀性能的研究

宁礼奎郑志谭毅刘恩泽佟健于永泗王华

金属学报

研究了新型定向凝固镍基高温合金DZ68的抗热腐蚀性能, 并与K438合金进行了比较. 结果表明: 热处理态DZ68合金组织中几乎没有(γ+γ') 共晶, 碳化物尺寸小,其整体组织比较均匀; 在热腐蚀过程中发生比较均匀的腐蚀, 其外腐蚀层的腐蚀产物主要是(Ni, Co)Cr2O4, 内腐蚀层的腐蚀产物主要是Al2O3. 热处理态K438合金组织中存在较多的 (γ+γ'共晶和数量较多、尺寸较大的长条状碳化物, 组织均 匀性较差; 在热腐蚀过程中发生不均匀腐蚀, 其外腐蚀层的腐蚀产物主要是NiO, 内腐蚀层的腐蚀产物主要是CrS.两种合金中Ti元素的偏析有促进其它元素偏析的倾向, 使合金组织的均匀性恶化,热腐蚀均匀性变差. 在本实验条件下, DZ68合金的抗热腐蚀性能略好于K438合金.

关键词: DZ68 , hot corrosion , superalloy

3种700℃级超超临界燃煤锅炉备选高温合金煤灰腐蚀行为

鲁金涛 , 谷月峰 , 杨珍

腐蚀学报(英文)

研究了3种700℃超超临界燃煤锅炉备选高温合金Inconel 740,CCA617,GH 2984在760℃现役机组煤灰腐蚀介质中的高温腐蚀行为.结果表明:镍基合金Inconel 740和CCA 617均能形成保护性的Cr2O3氧化膜,局部点蚀为其主要失效形式.点蚀区域氧化膜为多层结构,由外到内依次为Ni(Co)O、Cr2O3(TiO、Al2O3)以及少量内层硫化物:较高Cr、Al含量提高了Inconel 740合金的耐蚀性能;挥发性产物与氧化膜微区溶解降低了CCA 617合金氧化膜的致密性.GH 2984合金因含有较多的Fe未能形成保护性的氧化膜,氧化膜分层生长,且出现了严重的剥落现象.

关键词: 700℃超超临界 , 高温合金 , 煤灰腐蚀 , 腐蚀机理

CRACK GROWTH BEHAVIOR AND FRACTURE FEATURE OF GH2132 UNDER CREEP-FATIGUE CONDITIONS

M.F. Geng(Luoyang Ship Material Research Institute , Luoyang 471039 , China)

金属学报(英文版)

The crack growth behavior and fracture feature of superalloy GH2132 (equivalent to A286) under creep-fatigue conditions have been studied in the present paper. The tests were carried out at 550℃ under various cyclic freqencies (hold time) and load levels,and the fracture surfaces were examined by using a scanning electron microscope. It is shown that the fracture mode of creep-fatigue and the effect of cyclic loading on crack growth change with the growth of crack and the increase of net-section stress,and both are reversed when the net-section stress is up to the yield stress of material.When σn <σ0.2, cracking is predominantly cycle-dependent transgranular and cyclic loading accelerates creep crack growth, whereas when σm>σ0.2, the case is reversed.

关键词: creep-fatigue , null , null , null , null , null

HEAT TRANSFER BEHAVIOR OF SUPERALLOY DROPLETS DURING SPRAY FORMING

J.F. Sun , J. Shen , Z. Y. Li , J. Jia and Q.C. Li National Key Laboratory of Metal Precision Hot Processing , Harbin Institute of Technology , Harbin 150001 , China

金属学报(英文版)

Based on the Newtonian heat transfer formulation and classical heterogeneous nucleation theory, a mathematical model has been established to predict the profile of flight velocity, heat transfer coefficient, temperature, solid fraction and cooling rate of atomizing droplets for a superalloy. The results indicated that above parameters change with different droplet size and flight distance. The changing trend as well as the mechanism for the change are described and discussed.

关键词: spray forming , null , null , null

HIGH TEMPERATURE CRACK PROPAGATION AND FRACTUREOF SUPERALLOYS

Author X.S. Xie , Z.C. Xu and J.X. Dong High Temperature Materials Research Laboratory , University of Science and Technology Beijing , Beijing 100083 , ChinaManuscript received 18 October 1998

金属学报(英文版)

High temperature crack propagation and fracture behavior of disks produced by six superalloys have been studied. Crack propagation rates were determined at 650 creep, fatigue and creep/fatigue interaction conditions. The crack propagation rate is raised with increasing strength of superalloy and is also increased with the dwelling time at maximum stress level of cyclic creep test condition. Crack propagation behavior is closely related to high temperature ductility (such as creep strain and stress rupture elongation). Ductility improvement can increase crack propagation resistance by means of softening heat treatment, controlling grain boundary precipitate and microalloying treatment (such as Mg addition to superalloy). \=

关键词: crack propagation , null , null , null

SPRAY FORMED NICKEL-BASE SUPERALLOYS

Z. Li , S.F. Tian , X.G. Zhao , Z.K. Liang , L.P. Ren , G.F.Mi and M.G. Yan(Bejing Institute of Aeronautical Materials , Beijing 100095 , China Manuscript received 26 August 1996)

金属学报(英文版)

In this paper,part of the research and development work in the field of spray formed superalloys at BIAM of China is briefly summarized. With an experimental spray forming facility,whose melting capacity is suitable for making disk and columnar shaped integral-dense and clean Ni-base superalloy preforms with low oxygen content,fine grain, uniform chemistry and improved forgeability, a series of Ni-base superalloys have been spray atomized and deposited, among which three alloys have been chosen for microstructural and mechanical properties evaluation.

关键词: :spray forming , null , null

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