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焊趾处椭圆表面裂纹的权函数与残余应力强度因子的权函数法 被引量:4

Weight function for weld toe semi-elliptical surface crack and calculating residual stress intensity factors by weight function method
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摘要 利用三维有限元计算了焊趾处半椭圆表面裂纹的应力强度因子。利用统一的权函数形式,结合得到裂纹半长比a/c=0.2;0.4;0.6;0.8,a/t=0.1~0.8的有限元数据,得到了适用于T型接头焊趾处半椭圆表面裂纹最深点和表面点的权函数。权函数的准确性,用有限元在裂纹面施加高阶载荷进行了验证,对于表面点和最深点,半长比a/c=0.2~0.8,a/t=0.1~0.8,权函数与有限元结果误差在8%以下。基于得到的权函数,计算了T型接头焊趾处半椭圆表面裂纹的残余应力强度因子Kres,并与有限元计算结果进行对比,对比误差在10%以下,表明新的权函数能很好地预测T型接头焊趾处的残余应力强度因子。 The stress intensity factors(SIFs) of semi-elliptical surface cracks at the weld toe were analyzed by using finite element analysis(FEA). Based on the obtained stress intensity factor data of surface cracks with aspect ratio from a/c=0.2~0.8 and a/t=0.1~0.8 by FEA, new weight functions for the calculation of T-butt weld toe surface cracks SIFs at both surface and deepest point were derived under constant and linear distributed stresses. The new weight functions were extended for higher order stress distribution situation and validated through the results obtained by FEA under parabolic and cubic stress loading. The difference between weight function and FEA is less than 10% for cracks with aspect ratio a/c=0.2~0.8, a/t=0.1~0.8 at both surface point and deepest point. The derived weight function is used to calculate the SIFs of weld toe surface crack due to residual stress, results comparison with FEA method shows new weight function can make good predication for the weld toe surface crack SIFs.
作者 徐磊 黄小平
出处 《船舶力学》 EI CSCD 北大核心 2017年第4期443-454,共12页 Journal of Ship Mechanics
关键词 T型接头 焊趾 表面裂纹 应力强度因子 权函数 残余应力 T-butt weld toe surface crack stress intensity factor weight function residual stress
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  • 1Suresh S,Ritchie R O.On the influence of environment on the load ratio dependence of fatigue thresholds in pressure vessel steel[J].Engng Fracmre Mech.,1983,18:785-800.
  • 2Chang T,Guo W.Effects of strain hardening and stress state on fatigue crack closure[J].Int J Fatigue,1999,21:881-888.
  • 3BS7910.Guide on methods for assessing the acceptability of flaws in structures[M].British Standards Institution,1999.
  • 4King R.A review of fatigue crock growth rates in air and seawater[M].HSE Report OTH 511,London,Health & Safety Executive Books,1998:ISBN 0717621437.
  • 5Tsukuda H,Ogiyama H,Shiraishi T.Fatigue crack growth and closure at high stress ratios[J].Fatigue Fract Eng Mater Struct.,1995,18:503-514.
  • 6Tan J M L,Fitzpatrick M E,Edwards L.Stress intensity factors for through-thickness cracks in a wide plate:Derivation and application to arbitrary weld residual stress fields[J].Eng.Frac.Mech.,2007,74:2030-2054.
  • 7Huang X P,Moan T.Improved modeling of the effect of R-ratio on crack growth rate[J].Int.J Fatigue,2007,29:591-602.
  • 8Huang Xiaoping.Fatigue crack growth rote recommended in BS7910 and a unique crack growth rote curve under different load ratios[C]//ASME PVP 2007/CREEP 8 Conference July 22-26,2007.San Antonio,Texas,USA,2007.
  • 9Huang X P,Moan T,Cui W C.An engineering model of fatigue crack growth under variable amplitude loading[J].Int.J Fatigue,2008,30:2-10.
  • 10Huang X P,Moan T,Cui W C.A unique crack growth rate curve method for fatigue life prediction of steel structures[J].Ships and Offshore Structures,2009,4(2):165-173.

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