A predictive fatigue life model for anodized 7050 aluminium alloy

The objective of this study is to predict fatigue life of anodized 7050 aluminum alloy specimens. In the case of anodized 7050-T7451 alloy, fractographic observations of fatigue tested specimens showed that pickling pits were the predominant sites for crack nucleation and subsequent failure. It has been shown that fatigue failure was favored by the presence of multiple cracks. From these experimental results, a fatigue life predictive model has been developed including multi-site crack consideration, coalescence between neighboring cracks, a short crack growth stage and a long crack propagation stage. In this model, all pickling pits are considered as potential initial flaws from which short cracks could nucleate if stress conditions allow. This model is built from experimental topography measurements of pickled surfaces which allowed to detect the pits and to characterize their sizes (depth, length, width). From depth crack propagation point of view, the pickling pits are considered as stress concentrator during the only short crack growth stage. From surface crack propagation point of view, machining roughness is equally considered as stress concentrator and its influence is taken into account during the all propagation stage. The predictive model results have been compared to experimental fatigue data obtained for anodized 7050-T7451 specimens. Predictions and experimental results are in good agreement.

[1]  B. Hillberry,et al.  A model of initial flaw sizes in aluminum alloys , 2001 .

[2]  Hiroshi Noguchi,et al.  Tension of a finite-thickness plate with a pair of semi-elliptical surface cracks , 1990 .

[3]  Lee,et al.  The effect of pitting corrosion on fatigue life , 2000 .

[4]  H. Voorwald,et al.  Influence of anodization on the fatigue strength of 7050-T7451 aluminium alloy , 2007 .

[5]  A fatigue multi-site cracks model using coalescence, short and long crack growth laws, for anodized aluminum alloys , 2010 .

[6]  C. Mabru,et al.  Influence of Anodizing Process on Fatigue Life of Machined Aluminium Alloy , 2010 .

[7]  J. Newman,et al.  Stress-intensity factor equations for cracks in three-dimensional finite bodies subjected to tension and bending loads , 1984 .

[8]  A. Cree,et al.  Effect of anodised coatings on fatigue crack growth rates in aluminium alloy , 1997 .

[9]  S. Pantelakis,et al.  Fatigue and damage tolerance behaviour of corroded 2024 T351 aircraft aluminum alloy , 2005 .

[10]  David Taylor,et al.  Physically short crack propagation in metals during high cycle fatigue , 2009 .

[11]  M. E. Haddad,et al.  Prediction of non propagating cracks , 1979 .

[12]  Catherine Mabru,et al.  Influence of surface treatments on fatigue life of Al 7010 alloy , 2010 .

[13]  C. R. Feng,et al.  On fatigue crack initiation from corrosion pits in 7075-T7351 aluminum alloy , 2000 .

[14]  S. Rokhlin,et al.  Effect of pitting corrosion on fatigue crack initiation and fatigue life , 1999 .

[15]  C. Blanc,et al.  Characterisation of sealed anodic films on 7050 T74 and 2214 T6 aluminium alloys , 2002 .

[16]  Corrosion , 1941, Science.

[17]  Jianhua Liu,et al.  Effect of the Microstructure of Al 7050-T7451 on Anodic Oxide Formation in Sulfuric Acid , 2009 .

[18]  Sia Nemat-Nasser,et al.  Interacting dissimilar semi-elliptical surface flaws under tension and bending , 1982 .

[19]  J. Duszczyk,et al.  The effect of oxide coatings on fatigue properties of 7475-T6 aluminium alloy. , 2007 .

[20]  G. Thompson,et al.  Boric/sulfuric acid anodizing of aluminum alloys 2024 and 7075: Film growth and corrosion resistance , 1999 .

[21]  Jérôme Limido,et al.  Modelling the influence of machined surface roughness on the fatigue life of aluminium alloy , 2008 .

[22]  Kenan Genel,et al.  Effect of anodic oxidation on fatigue performance of 7075-T6 alloy , 2008 .

[23]  M. A. Przystupa,et al.  Microstructure based fatigue life predictions for thick plate 7050-T7451 airframe alloys , 1997 .

[24]  C. Mabru,et al.  Surface characterization and influence of anodizing process on fatigue life of Al 7050 alloy , 2011 .

[25]  Mirco D. Chapetti,et al.  Fatigue propagation threshold of short cracks under constant amplitude loading , 2003 .

[26]  J. Newman,et al.  Fatigue-life prediction methodology using small-crack theory , 1999 .

[27]  S. Pearson Initiation of fatigue cracks in commercial aluminium alloys and the subsequent propagation of very short cracks , 1975 .

[28]  D. Hall,et al.  Relationship of microstructure to fatigue strength loss in anodised aluminium–copper alloys , 2005 .

[29]  C. Mabru,et al.  Effect of sealed anodic film on fatigue performance of 2214-T6 aluminum alloy , 2012 .

[30]  J. Lankford THE INFLUENCE OF MICROSTRUCTURE ON THE GROWTH OF SMALL FATIGUE CRACKS , 1985 .

[31]  R. Sadeler Effect of a commercial hard anodizing on the fatigue property of a 2014-T6 aluminium alloy , 2006 .