Volume 27 Issue 4
Apr.  2012
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2012  >  27(4): 811-816
GAO Chao, CHENG Li, PENG Hua, SHEN Jing-sheng, QIU Chen-lin, LIU Yan-jie. Investigation of ultra-high cycle fatigue behavior of TC17 alloy at a frequency of 20kHz[J]. Journal of Aerospace Power, 2012, 27(4): 811-816.
Citation: GAO Chao, CHENG Li, PENG Hua, SHEN Jing-sheng, QIU Chen-lin, LIU Yan-jie. Investigation of ultra-high cycle fatigue behavior of TC17 alloy at a frequency of 20kHz[J]. Journal of Aerospace Power, 2012, 27(4): 811-816.
shu

Investigation of ultra-high cycle fatigue behavior of TC17 alloy at a frequency of 20kHz

  • 1.

    The Engineering Institute, Air Force Engineering University, Xi’an 710038, China

  • 2.

    School of Communication Engineering, Chong Qing University, Chongqing 400044, China

  • Received Date: 2011-05-22
  • Rev Recd Date: 2012-02-12
  • Publish Date: 2012-04-28
    Abstract
  • The bending fatigue system was developed using the piezoelectric ultrasonic fatigue testing technology and experimental investigation of the ultra-high cycles fatigue life for TC17 alloy subjected to bending fatigue deformation has been conducted.The experimental resultes show that the specimens were tested to failure in the range of 107-109 cycles and the fatigue limit decreases with the increasing number of cycles between 107 and 109 for R=-1.0 and there was no obvious fatigue limit.The S-N curve for TC17 is a continuous decline curve between 107 and 109 cycles.The fractographic study showes that fatigue failures are mostly initiated at the surface of the test specimens.When there are subsurface inclusions,fatigue cracks initiated from subsurface inclusions,and the composition of inclusions is mainly oxides of aluminums.

     

    • FullText(HTML)
  • loading
    • References(14)
  • [1]
    Marines I,Dominguez G,Baudry G,et al.Fatigue and fracture crack growth of aluminum alloys at very high numbers of cycles[J].International Journal of Fatigue,2003,25(10):37-46.
    [2]
    Papakyriacou M,Mayer H,Pypen C,et al.Fatigue behaviour of dup1ex phase alloys in the very high cycle regime[J].Mater. Sci. Eng. A,2001,308(1):43-52.
    [3]
    Stanzl-Tschegg S E,Mayer H.How and why the fatigue S-N curve does not approach a horizontal assymptote[J].International Journal of Fatigue,2001,23(Supplement):231-237.
    [4]
    McEvily A J,Nakamura T,Oguma H,et al.On the mechanism of very high cycle fatigue in Ti-6Al-4V[J].Scripta Materialia,2008,59:1207-1209.
    [5]
    USDepartment of Defense.MIL-HDBK,1783BW/CHANGE2, engine structural integrity programs(ENSIP)[S].Washington:US Department of Defense,2004.
    [6]
    Morrissey R,Nicholas T.Staircase testing of a titanium alloy in the gagacycle regime[J].International Journal of Fatigue,2006,28:1577-1582.
    [7]
    周承恩,洪友士.GCrl5钢超高周疲劳行为的实验研究[J].机械强度,2004,26(Supplement):157-160. ZHOU Chengen,HONG Youshi.Experimental investigation on very-high-cycle fatigue of GCr15 steel[J].Journal of Mechanical Strength,2004,26(Supplement):157-160.(in Chinese)
    [8]
    XUE Hongqian,TAO Hong,WANG Qingyuan,et al.Development of a three-point bending fatigue testing methodology at 20kHz frequency[J].International Journal of Fatigue,2007,29:2085-2093.
    [9]
    唐维维,王弘.超声弯曲疲劳实验方法及其应用[J].力学与实践,2008,30(6):43-46. TANG Weiwei,WANG Hong.Method of ultrasonic bending fatigue and application[J].Mechanics in Engineering,2008,30(6):43-46.(in Chinese)
    [10]
    Ritchie R O,Boyce B L,Campbell J P,et al.Thresholds for high-cycle fatigue in a turbine engine Ti-6Al-4V alloy[J].International Journal of Fatigue,1999,21:653-662.
    [11]
    McEvily A J,Nakamura T,Oguma H,et al.On the mechanism of very high cycle fatigue in Ti-6Al-4V[J].Scripta Materialia,2008,59:1207-1209.
    [12]
    Zuo J H,Wang Z G,Han E H.Effect of microstructure on ultra-high cycle fatigue behavior of Ti-6Al-4V[J].Materials Science and Engineering A,2008,473:147-152.
    [13]
    Lanning D B,Nicholas T,Haritos G K.Effect of plastic prestrain on high cycle fatigue of Ti-6Al-4V[J].Mechanics of Materials,2002,34:127-134.
    [14]
    Pollak R D.Analysis of methods for determining high cycle fatigue strength of a material with investigation of Ti-6Al-4V gigacycle fatigue behavior.Wright-Patterson AFB OH:Air Force Institute of Technology,2005:50-55.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(572.0KB)
    XML

    Article Metrics

    Article views (2008) PDF downloads(665) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return