网站首页期刊简介编委会过刊目录投稿指南广告合作征订与发行联系我们English
铸态N3合金模具服役后的显微组织及力学性能
英文标题:Microstructure and machanical property of as-cast N3-alloy after service
作者:冯微 赵会彬 张华霞 孟宇 
单位:(北京航空材料研究院股份有限公司 高温合金熔铸事业部 北京 100095) 
关键词:等温锻造 服役损伤 高温合金 模具 裂纹 
分类号:TG132.3
出版年,卷(期):页码:2024,49(12):154-161
摘要:

 为了解等温锻造模具服役损伤的根本原因,以服役后表面开裂的等温锻造用模具为研究对象,通过宏观腐蚀、扫描电镜、能谱分析并结合力学性能测试方法,对其损伤形式和原因进行了研究。结果表明:模具表面及内部无疏松、冷隔等铸造缺陷,服役后未见磨损、变形。模具的损伤发生在上表面,主要表现为服役时高温氧化和冷热疲劳导致的裂纹,深度为10~30 mm。模具其余部位的高温拉伸性能和持久性能均高于服役前,分析原因为模具合金在服役过程中进一步析出的纳米级二次γ′相和颗粒状M6C起到强化作用。为了提高模具使用寿命,使用过程应避免急冷急热,铸造过程应控制工艺,避免生成初生大块状M6C。

 

 Abstract: In order to understand the fundamental causes of service damage in isothermal forging molds, for the isothermal forging molds with surface cracking after service, the damage forms and causes were studied by macroscopic corrosion, scanning electron microscopy, energy spectrum analysis and mechanical property testing methods. The results show that there are no casting defects such as porosities or cold insulation on the surface and inside of the mold, and wear or deformation was not observed after service. The damage to the mold occurs on the upper surface, mainly manifests as cracks caused by the high-temperature oxidation and the cold and hot fatigue during service, with the depth of 10-30 mm. The high-temperature tensile properties and durability properties for the remaining parts of the mold are higher than that before service, and the reason is that the mold alloy further precipitates nanoscale secondary γ′ phase and granular M6C during service, which plays a strengthening role. In order to improve the service life of the mold, rapid cooling and heating should be avoided during service, and the casting process should be controlled to avoid the generation of initial large block shaped M6C.

 
基金项目:
作者简介:
作者简介:冯微(1982-),女,硕士,工程师 E-mail:fengwei620@163.com
参考文献:

 
[1]王淑云,李惠曲,杨洪涛.粉末高温合金超塑性等温锻造技术研究
[J].航空材料学报, 2007, 27(5):30-33.


 

Wang S Y,Li H Q,Yang H T. Superplastic isothermal forging of technology of P/M superalloy
[J].Journal of Aeronautical Materials, 2007, 27(5):30-33.

 


[2]张利军,常辉,薛祥义.等温锻造技术及其在航空工业中的应用
[J].热加工工艺,2010,39(21):21-24.

 

Zhang L J,Chang H,Xue X Y,et al.Isothermal forging technology and its application in aviation industry
[J].Hot Working Technology,2010,39(21):21-24.

 


[3]张国庆,张义文,郑亮,等.航空发动机用粉末高温合金及制备技术研究进展
[J].金属学报, 2019, 55(9):1133-1144.

 

Zhang G Q,Zhang Y W,Zheng L,et al.Research progress in powder metallurgy superalloys and manufacturing technologies for aeroengines application
[J].Acta Metallurgica Sinica,2019,55(9):1133-1144.

 


[4]赵会彬,吴昌新,郭灵.1100℃等温锻造用模具材料的研制
[J].材料工程, 2009(S1):18-21.

 

Zhao H B,Wu C X,Guo L.Development of a die material for isothermal forging at 1100℃
[J].Journal of Materials Engineering,2009(S1):18-21.

 


[5]Zhou T J,Feng W,Zhao H B,et al. Coupling effects of tungsten and molybdenum on microstructure and stressrupture properties of a nickelbase cast superalloy
[J].Progress in Nature Science:Material International,2018,28(6):45-53.

 


[6]Tawancy H M,AlHadhrami L M. Degradation of turbine blades and vanes by overheating in a power station
[J].Engineering Failure Analysis,2009,16(1):273

 


[7]Tong J Y,Ding X F,Wang M L,et al.Assement of sercice indeced degradation of microstructure and properties in turbine blades made of GH4037 alloy
[J].Journal of Alloys and Compounds,2016,657:777-786.

 


[8]Miura N,Nakata K,Miyazaki M,et al. Morphology of γ′ precipitates in second stage high pressure turbin blade of single crystal nicklebased superally after service
[J].Materials Science Forum,2010,638-642:2291-2296.

 


[9]GB/T 228.2—2015,金属材料拉伸试验第2部分:高温试验方法
[S].

 

GB/T 228.2—2015, Metallic materials—Tensile testing—Part 2: Method of test at elevated temperature
[S].

 


[10]GB/T 2039—2024,金属材料单轴拉伸蠕变试验方法
[S].

 

GB/T 2039—2024,Metallic materials—Uniaxial creep testing method in tension
[S].

 


[11]郭建亭.高温合金材料学(下册):高温合金材料与工程应用
[M].北京:科学出版社,2010.

 

Guo J T.Materials Science and Engineering for Superalloys(Volume Ⅱ): High Temperature Alloy Materials and Engineering Applications
[M].Beijing:Science Press,2010.

 


[12]郭建亭.高温合金材料学(上册):应用基础理论
[M].北京:科学出版社,2010.

 

Guo J T.Materials Science and Engineering for Superalloys(Volume Ⅰ): Basic Theory
[M].Beijing:Science Press,2010.

 


[13]喻健,李嘉荣,史振学,等.DD6单晶高温合金二次γ′相的析出
[J].稀有金属材料与工程, 2013,42(8):1654-1658.

 

Yu J,Li J R,Shi Z X,et al. Precipitation of secondary γ′ phase of DD6 singal crystal superalloy
[J].Rear Metal Materials and Engineering, 2013,42(8):1654-1658.

 


[14]韦林,周思耕,盛乃成,等.γ′相对高钨镍基高温合金拉伸和持久变形行为的影响
[J].材料研究学报, 2023,37(1):29-38.

 

Wei L,Zhou S G,Sheng N C,et al. Effect of γ′-phase on tensile and stress rupture deformation behavior of high Wcontaining Nibased superalloys
[J].Chinese Journal of Materials Research,2023,37(1):29-38.

 


[15]杨刚.DZ417G合金化学成分对合金组织性能的影响
[D].哈尔滨:哈尔滨工业大学,2018.

 

Yang G.Effect of Chemical Compositions of DZ417G Superalloy on the Microstructure and Mechanical Properties
[D].Harbin: Harbin Institute of Technology,2018.

 


[16]杨金侠,郑启,孙晓峰,等.高温合金IN792组织与持久性能稳定性研究
[J].稀有金属材料与工程, 2012,41(6):1038-1040.

 

Yang J X,Zheng Q,Sun X F,et al. Stability of microstructure and stressrupture properties of IN792 superalloy
[J].Rear Metal Materials and Engineering,2012,41(6):1038-1040.

 


[17]穆岩,王树森,仉凤江,等.长期时效对高钨镍基高温合金碳化物演变的影响
[J].特种铸造及有色合金, 2021,41(9):1148-1152.

 

Mu Y,Wang S S,Zhang F J,et al.Effect of longterm thermal exposure on carbide evolution in high tungsten Nibased superalloy
[J].Special Casting & Nonferrous Alloys,2021,41(9):1148-1152.

 


[18]谭毅,廖娇,李佳艳,等.电子束熔炼Inconel 740合金不同热处理状态下的组织演变与显微硬度
[J].材料工程, 2015,43(4):19-24.

 

Tan Y,Liao J,Li J Y,et al.Microstructure evolution and microhardness of Inconel 740 alloy in different heattreatment conditions prepared by electron beam melting
[J].Journal of Materials Engineering,2015,43(4):19-24.

 


[19]朱玉平,盛乃成,谢君,等.高钨镍基高温合金K416B富W相的析出行为
[J].金属学报, 2021,57(2):215-223.

 

Zhu Y P,Sheng N C,Xie J,et al. Precipitation behavior of Wrich phases in a highW containing Nibased superalloys K416B
[J].Acta Metallurgica Sinica, 2021,57(2):215-223.

 


[20]周同金.铸造高钨镍基高温模具合金组织及力学性能研究
[D].哈尔滨:哈尔滨工业大学,2019.

 

Zhou T J.Microstructure and Mechanical Properies of Cast Nickelbased Superalloy with High Tungsten Content Using for High Temperature Dies
[D].Harbin: Harbin Institute of Technology,2019.

 


[21]Ai C,Liu L,Zhang J,et al. Influnce of substituting Mo for W on solidification characteristics of Recontaining Ni based single crystal superalloy
[J].Journal of Alloys and Compounds,2018,754:85-92.

 


[22]肖传民,舒德龙,谢君,等.Hf对一种高W镍基合金组织及拉伸性能的影响
[J].沈阳工业大学学报, 2021, 43(4):396-401.

 

Xiao C M,Shu D L,Xie J,et al. Influnce of Hf content on microstructure and tensile properties of a nickle based superalloys with high W content
[J].Journal of Shenyang University of Technology, 2021, 43(4):396-401.

 


[23]刘君.钛合金等温锻用K403模具材料特性及失效研究
[D].西安:西北工业大学,2015.

 

Liu J.Study on Material Characteristic of Failure of K403 Die Used for Isothermal Forging of Titanium Alloys
[D].Xi′an:Northwesten Polytechnical University,2015.

 

 


[24]刘艳霞.挤压模具材料用粉末冶金镍基合金研究
[D].赣州:江西理工大学,2015.

 

Liu Y X.Study on Powder Metallurgy Nickel Based Alloy for Extrusion Mold Materials
[D].Ganzhou:Jiangxi University of Science and Technology,2015.

 

服务与反馈:
文章下载】【加入收藏
《锻压技术》编辑部版权所有

中国机械工业联合会主管  中国机械总院集团北京机电研究所有限公司 中国机械工程学会主办
联系地址:北京市海淀区学清路18号 邮编:100083
电话:+86-010-82415085 传真:+86-010-62920652
E-mail: fst@263.net(稿件) dyjsjournal@163.com(广告)
京ICP备07007000号-9