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表面完整性对FGH95合金高温疲劳性能的影响
Effect of surface integrity evolution on high-temperature fatigue property of FGH95 alloy

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罗学昆 1 *   吴小燕 2   王科昌 2   王欣 1   汤智慧 1  
文摘 金属构件的加工表面完整性状态对其整体疲劳性能具有显著影响。本工作研究了磨削、磨削 +铸钢丸喷丸、磨削 +陶瓷丸喷丸和磨削 +复合喷丸4种表面加工集成方法对FGH95合金高周疲劳性能的影响规律。采用表面粗糙度仪、X射线残余应力测试仪和显微硬度计分别对不同复合加工方法试样的表面粗糙度、表面残余应力分布和硬度梯度等表面完整性参数进行了表征;采用旋转弯曲疲劳试验机测试了缺口(应力集中系数Kt = 1.7)试样的旋转弯曲疲劳,研究不同表面完整性状态对缺口试样高温疲劳寿命的影响规律。结果表明:相对磨削,磨削 +铸钢丸喷丸、磨削 +陶瓷丸喷丸和磨削 +复合喷丸三种方法均可显著提高试样的高温疲劳寿命;其中,磨削 +复合喷丸方法获得了最优的表面残余应力场、硬度梯度、表面粗糙度和高温疲劳寿命增益效果。
其他语种文摘 Surface integrity state after machining has an important effect on the service life of metal parts and components. The effects of four kinds of surface integration processing methods on the high-temperature fatigue properties of FGH95 alloy were investigated. These four surface processing methods were AR (grinding), GCSSP (grinding and cast steel shot peening), GCSP (grinding and ceramic shot peening) and GDSP (grinding and double shot peening). The surface roughness, residual stress distribution and micro-hardness were characterized by roughness tester, X-ray diffraction (XRD) stress tester and micro-hardness tester. The rotating-bending fatigue life with notched specimens (stress concentration factor, Kt = 1.7) was investigated. The results indicate that the fatigue life of specimens increased largely by GCSSP, GCSP and GDSP compared with AR specimens respectively. Furthermore, GDSP process can obtain the best surface residual stress field distribution, gradient distribution of micro-hardness, surface roughness and improvement of the high-temperature fatigue property.
来源 航空材料学报 ,2020,40(2):53-60 【核心库】
DOI 10.11868/j.issn.1005-5053.2019.000108
关键词 喷丸 ; 高温合金 ; 疲劳 ; 表面完整性
地址

1. 中国航发北京航空材料研究院, 航空材料先进腐蚀与防护航空重点实验室, 北京, 100095  

2. 中国航发南方工业有限公司, 湖南, 株洲, 412002

语种 中文
文献类型 研究性论文
ISSN 1005-5053
学科 金属学与金属工艺
基金 国家重大科技专项 ;  中国航发自主创新专项资金项目
文献收藏号 CSCD:6680367

参考文献 共 21 共2页

1.  Xu Z. The influence of shot peening on the fatigue response of Ti-6Al-4V surfaces subject to different machining processes. International Journal of Fatigue,2018,111:196-207 被引 6    
2.  Field M. A review of measuring methods for surface integrity. Ann CIRP,1972,21:219-238 被引 3    
3.  Yao C F. Influence of high-speed milling parameter on 3D surface topography and fatigue behavior of TB6 titanium alloy. Transactions of Nonferrous Metals Society of China,2013,23(3):650-660 被引 16    
4.  Arunachalam S R. Effect of electrical discharge machining on corrosion and corrosion fatigue behavior of aluminum alloys. International Journal of Fatigue,2018,111:44-53 被引 2    
5.  Prabhakarn S. Laser shock peening without coating induced residual stress distribution, wettability characteristics and enhanced pitting corrosion resistance of austenitic stainless steel. Applied Surface Science,2017,428:17-30 被引 7    
6.  He W F. The effects of laser shock peening on fatigue life in Ni-based superalloy. Advanced Materials Research,2010,135:209-214 被引 6    
7.  Bhaumik S K. Fatigue failure of aircraft components. Engineering Failure Analysis,2008,15(6):675-694 被引 9    
8.  Jiang X P. Effects of shot-peening and re-shot-peening on four-point bend fatigue behavior of Ti-6Al-4V. Materials Science & Engineering:A,2007,468(12):137-143 被引 2    
9.  Lindemann J. Effect of shot peening on fatigue performance of a lamellar titanium aluminide alloy. Acta Materialia,2006,54(4):1155-1164 被引 22    
10.  Yang Q. Effect of shotpeening on the fretting wear and crack initiation behavior of Ti-6Al-4V dovetail joint specimens. International Journal of Fatigue,2018,107:83-95 被引 7    
11.  吴庆辉. 喷丸处理对DD6合金表面状态和中温疲劳性能的影响. 热加工工艺,2017,46(12):158-161 被引 3    
12.  Foss B J. Analysis of shot-peening and residual stress relaxation in the nickelbased superalloy RR1000. Acta Materialia,2013,61(7):2548-2559 被引 13    
13.  Bache M R. Environment and time dependent effects on the fatigue response of an advanced nickel based superalloy. International Journal of Fatigue,2009,31(11):1719-1723 被引 5    
14.  Wu D. Surface characterization and fatigue evaluation in GH4169 superalloy:Comparing results after finish turning; shot peening and surface polishing treatments. International Journal of Fatigue,2018,113:222-235 被引 4    
15.  王旭青. 复杂形状FGH95粉末盘形件固溶处理组织及性能研究. 材料工程,2009(增刊1):61-63 被引 4    
16.  马国君. FGH95粉末高温合金长期时效组织稳定性研究. 钢铁研究学报,2011(增刊2):462-465 被引 3    
17.  王欣. 表面完整性对C250型超高强度钢高周疲劳性能的影响. 中国表面工程,2014,27(2):69-74 被引 6    
18.  Child D J. Assessment of surface hardening effects from shot peening on a Nibased alloy using electron backscatter diffraction techniques. Acta Materialia,2011,59(12):4825-4834 被引 11    
19.  Liu Y G. Characterization of surface layer in TC17 alloy treated by air blast shot peening. Materials & Design,2015,65:120-126 被引 14    
20.  汝继来. Rene'95粉末合金喷丸强化研究. 航空材料学报,1996,16(1):32-35 被引 1    
引证文献 11

1 詹玉婷 喷丸强化对自制螺母疲劳寿命性能的影响分析 中国腐蚀与防护学报,2021,41(3):395-399
被引 1

2 黄小康 高温合金机器人柔性磨削表面完整性研究进展 航空制造技术,2021,64(7):38-52
被引 3

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