超声振动载荷下S06钢的长寿命疲劳性能

胡燕慧; 钟群鹏; 张 峥; 韩邦成

超声振动载荷下S06钢的长寿命疲劳性能

1.
北京航空航天大学材料科学与工程学院, 北京 100191
2. 北京航空航天大学仪器科学与光电工程学院, 北京 100191

详细信息

作者简介:
胡燕慧(1979-),女,河北蔚县人,博士生,orangehyh@126.com.

中图分类号: O 346.2
计量
- 文章访问数: 2891
- HTML全文浏览量: 113
- PDF下载量: 1468
- 被引次数: 0
出版历程
- 收稿日期: 2009-03-23
- 网络出版日期: 2010-04-30

Fatigue properties of S06 steel in long life regime under ultrasonic frequency

1.
School of Materials Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. School of Instrument Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 采用超声疲劳试验方法对新型沉淀硬化马氏体不锈钢S06钢在10⁶~10⁹周次范围的疲劳性能进行测定,结果表明:S06钢在循环周次大于10⁷周次的范围仍然发生疲劳断裂,在10⁶~10⁹之间,应力寿命曲线持续下降,不存在疲劳极限,用10⁷周次的条件疲劳极限来对S06钢长寿命构件进行无限寿命设计是不安全的.用载荷类型相同并且试样尺寸相近的高频疲劳试验方法对S06钢10⁴~10⁷周次的疲劳性能进行测定,将数据与超声疲劳试验结果进行对比发现:超声疲劳试验方法获得的S06钢的疲劳强度更高.用两种加载频率下10⁶~10⁷周次左右的试验数据拟合得到中值应力寿命曲线,根据应力寿命关系式中的疲劳强度系数的比值来对超声疲劳试验数据进行修正.在考虑了裂纹萌生机制和进行了频率影响修正的情况下,用线性异方差回归方法将超声疲劳试验数据拟合得到S06钢的长寿命P-S-N曲线,为长寿命构件的疲劳设计提供了基础.
- S06钢 /
- 超声疲劳试验方法 /
- 高频疲劳试验方法 /
- 线性异方差回归分析 /
- P-S-N 曲线
Abstract: S06 steel is a new kind of precipitation-hardened stainless martensite steel. The fatigue properties between 10⁶~10⁹ cycles of S06 steel were tested with ultrasonic fatigue testing machine. Results show that fatigue failure takes place after 10⁷ cycles and an endurance limit does not exist for S06 steel. Fatigue design on infinite life criterion can-t be used for components made of this steel. High-cycle fatigue testing method with the same loading mode and approximate specimen dimension with that of ultrasonic fatigue tests was used to study the fatigue properties between 10⁴~10⁷ cycles. The results show that fatigue strength of S06 steel is higher with ultrasonic fatigue testing method. Ultrasonic fatigue testing data was amended by comparing the fatigue strength coefficient of Basquin formula. The P-S-N curves at 10⁶~10⁹ cycles of S06 steel considering cracking initiation mechanism and frequency effect were fit with linear variance regression analysis method and the curves can be used for fatigue design of engineering components with long lifetime.
- S06 steel /
- ultrasonic fatigue testing method /
- high-cycle fatigue testing method /
- linear variance regression analysis /
- P-S-N curve

HTML全文

参考文献(1)

[1] Marines I,Bin X,Bathias C.An understanding of very high cycle fatigue of metals[J].International Journal of Fatigue,2003,25:1101-1107 [2] Bathias C,Drouillac L,Francois P L.How and why the fatigue S-N curve does not approach a horizontal asymptote[J].International Journal of Fatigue,2001,23:S143-S151 [3] Bathias C.There is no infinite fatigue life in metallic materials[J].Fatigue & Fracture of Engineering Materials & Structures,1999,22:559-565 [4] Marines-Garcia I,Paris P C,Tada H,et al.Fatigue crack growth from small to large cracks on very high cycle fatigue with fish-eye failures[J].Engineering Fracture Mechanics,2008,75(6):1657-1665 [5] 高镇同,熊峻江.疲劳可靠性[M].北京:北京航空航天大学出版社,2000:133-137 Gao Zhentong,Xiong Junjiang.Fatigue reliability[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2000:133-137(in Chinese) [6] Jing Ling,Jwo Pan.A maximum likelihood methof for estimating P-S-N curves[J].International Journal of Fatigue,1997,19(5):415-419 [7] 傅惠民.线性异方差回归分析[J].航空学报,1994,15(3):295-302 Fu Huimin.Linear variance regression analysis[J].ACTA Aeronautica ET Astronautica SINICA,1994,15(3):295-302(in Chinese) [8] 傅惠民.三参数幂函数回归分析[J].航空动力学报,1994,9(2):186-190 Fu Huimin.Power function with three parameters regression analysis[J].Journal of Aerospace Power,1994,9(2):186-190(in Chinese) [9] Akiniwa Y,Miyamoto N,Tsuru H,et al.Notch effect on fatigue strength reduction of bearing steel in the very high cycle regime[J].International Journal of Fatigue,2006,28:1555-1565 [10] 姚枚,王声平,李金魁.表面强化件的疲劳强度分析及金属的内部疲劳极限[J].金属热处理学报,1993,11:33-41 Yao Mei,Wang Shengping,Li Jinkui.An aspect of internal fatigue limit for metals with aid of strength appraisal on hardened steels[J].Acta Metallrugica Sinica,1993,11:33-41(in Chinese) [11] Gao Y K,Yao M,Shao P G,et al.Another mechanism for fatigue strength improvement of metallic parts by shot peening[J].J Mater Eng Perform,2003,12:507-511 [12] 王弘,高庆.超声疲劳试验中载荷频率对材料疲劳性能的影响[J].理化检验:物理分册,2005,41(9):433-435 Wang Hong,Gao Qing.Effect of load frequency on fatigue behavior of material in ultrasonic fatigue testing[J].PTCA(Part:A phys test),2005,41(9):433-435(in Chinese) [13] Peter P G,Todd S G.Effect of strain rate on flow properties,metal handbook(Vol 8)[M].9th ed.Ohio:ASM,1995:38-46

施引文献

资源附件(0)

访问统计