期刊文献+

THEORETICAL ANALYSIS AND EXPERIMENTAL VERIFICATION ON TERNARY-WAVES METHOD TO COMPILE ACCELERATED SPECTRA 被引量:1

THEORETICAL ANALYSIS AND EXPERIMENTAL VERIFICATION ON TERNARY-WAVES METHOD TO COMPILE ACCELERATED SPECTRA
下载PDF
导出
摘要 The equivalent damage calculation formulae of fatigue crack formation andgrowth are established. In order to compile the fatigue crack formation and growth accelerated loadspectra, the main wave shapes and load sequence of the actual load spectrum are kept constant, andthe carrier waves are cut off. And secondary waves are put together into new secondary waves toshorten the test time according to the equivalent damage calculation formulae respectively. Then bythe fatigue cumulative damage calculation of the fatigue crack formation and growth accelerated loadspectra, the one corresponding to the bigger damage is determined as the fatigue accelerated testload spectrum. Therefore in the test process, the fatigue accelerated test spectrum may be appliedtill fatigue failure, the engineering fatigue crack length of full-scale structure need not beinspected, and the fatigue crack formation accelerated load spectrum need not be transferred intothe fatigue crack growth accelerated load spectrum. Finally, it is verified by tests of two kinds ofspecimens that the damages of the specimens caused by the accelerated load spectra are near tothose by the actual load spectra; namely, the tested life of actual load spectra is similar to thatof accelerated load spectra. But the test time of accelerated load spectra is shortened by aboutthree-quarters that of actual load spectra. From these tests, it is also found that the fatigueaccelerated test spectrum has an advantage over FALSTAFF spectra. The equivalent damage calculation formulae of fatigue crack formation andgrowth are established. In order to compile the fatigue crack formation and growth accelerated loadspectra, the main wave shapes and load sequence of the actual load spectrum are kept constant, andthe carrier waves are cut off. And secondary waves are put together into new secondary waves toshorten the test time according to the equivalent damage calculation formulae respectively. Then bythe fatigue cumulative damage calculation of the fatigue crack formation and growth accelerated loadspectra, the one corresponding to the bigger damage is determined as the fatigue accelerated testload spectrum. Therefore in the test process, the fatigue accelerated test spectrum may be appliedtill fatigue failure, the engineering fatigue crack length of full-scale structure need not beinspected, and the fatigue crack formation accelerated load spectrum need not be transferred intothe fatigue crack growth accelerated load spectrum. Finally, it is verified by tests of two kinds ofspecimens that the damages of the specimens caused by the accelerated load spectra are near tothose by the actual load spectra; namely, the tested life of actual load spectra is similar to thatof accelerated load spectra. But the test time of accelerated load spectra is shortened by aboutthree-quarters that of actual load spectra. From these tests, it is also found that the fatigueaccelerated test spectrum has an advantage over FALSTAFF spectra.
出处 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2002年第4期308-313,共6页 中国机械工程学报(英文版)
基金 This project is supported by National Natural Science and Aeronautic Science Foundation of China (No. 50005003, No. 01A51011)
关键词 ternary-waves actual load-time history accelerated load spectra equivalent damage calculation main wave secondary wave carrier wave ternary-waves actual load-time history accelerated load spectra equivalent damage calculation main wave secondary wave carrier wave
  • 相关文献

参考文献5

二级参考文献24

共引文献80

同被引文献17

  • 1高伟,姜水生.分段曲线拟合与离散度加权的数据误差处理方法[J].中国测试技术,2005,31(6):55-56. 被引量:14
  • 2江龙平,徐可君.疲劳裂纹三维动态扩展灰色系统预测[J].机械工程学报,2006,42(1):86-89. 被引量:12
  • 3赵永翔,杨冰,张卫华.一种疲劳长裂纹扩展率新模型[J].机械工程学报,2006,42(11):120-124. 被引量:16
  • 4傅惠民 高镇同.P-S-N曲线拟合法[J].航空学报,1988,9(7):388-341.
  • 5PORTER T R.Method of analysis and prediction for variable amplitude fatigue crack growth[J].Engineering Fracture Mechanics,1972,4:717-736.
  • 6MCMASTER F J,SMITH D J.Predictions of fatigue crack growth in aluminium alloy 2024-T351 using constraint factors[J].International Journal of Fatigue,2001,23: S93-S101.
  • 7黄淑菊.两种加载方式下疲劳裂纹的扩展.机械工程学报,1984,20(2):69-78.
  • 8YISHENG W, SCHLJVE J.Fatigue crack closure measurements on 2024-T3 sheet specimens[J].Fatigue & Fracture of Engineering Materials & Structures,1995,18(9):917-921.
  • 9HUANG X P,TORGEIR M,CUI W C.An engineering model of Fatigue crack growth under variable amplitude loading[J].International Journal of Fatigue,2008,30:2-10.
  • 10ZHAO T,ZHANG J,JIANG Y.A study of fatigue crack growth of 7075-T651 aluminum alloy[J].International Journal of Fatigue,2008,30:1169-1180.

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部