The Effect of Peening on the Fatigue Life of 7050 Aluminium Alloy
The Effect of Peening on the Fatigue Life of 7050 Aluminium Alloy
The Effect of Peening on the Fatigue Life of 7050 Aluminium Alloy
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C<strong>on</strong>tents<br />
1. INTRODUCTION ............................................................................................................... 1<br />
2. REVIEW ........................................................................................................................2<br />
2.1 General........................................................................................................................ 2<br />
1.2 F/A-18 <str<strong>on</strong>g>Peening</str<strong>on</strong>g> Processes ........................................................................................ 6<br />
3. AMRL RESULTS ............................................................................................................... 14<br />
3.1 Overview <str<strong>on</strong>g>of</str<strong>on</strong>g> <str<strong>on</strong>g>Peening</str<strong>on</strong>g> Research Programs .......................................................... 14<br />
3.2 Early research - definiti<strong>on</strong> <str<strong>on</strong>g>of</str<strong>on</strong>g> potential problem .............................................. 14<br />
3.2.1 Assessment <str<strong>on</strong>g>of</str<strong>on</strong>g> RAAF aircraft................................................................. 21<br />
3.2.2 Surface roughness/residual stress measurement............................... 22<br />
1.1.3 Summary <str<strong>on</strong>g>of</str<strong>on</strong>g> AMRL <str<strong>on</strong>g>Peening</str<strong>on</strong>g> Specificati<strong>on</strong> .......................................... 26<br />
1.3 Rework <str<strong>on</strong>g>Peening</str<strong>on</strong>g> Research..................................................................................... 26<br />
1.3.1 Different rework process comparis<strong>on</strong>s................................................. 27<br />
1.1.2 F/A-18 fleet rework simulati<strong>on</strong>............................................................. 33<br />
1.1.3 Summary <str<strong>on</strong>g>of</str<strong>on</strong>g> AMRL Rework <str<strong>on</strong>g>Peening</str<strong>on</strong>g> Specificati<strong>on</strong>............................ 35<br />
1.4 <str<strong>on</strong>g>Peening</str<strong>on</strong>g> <strong>Life</strong> Improvement Factor (LIF).............................................................. 35<br />
1.5 Fleet Applicati<strong>on</strong>s Research.................................................................................. 37<br />
1.5.1 Y470 Crotch Repair Program ................................................................. 37<br />
1.5.2 Fleet Y470.5 X19 Pocket Repair program ............................................. 40<br />
1.1.3 IFOSTP <strong>Fatigue</strong> Tests .............................................................................. 45<br />
4. DISCUSSION..................................................................................................................... 46<br />
5. CONCLUSION................................................................................................................... 48<br />
6. ACKNOWLEDGMENTS ................................................................................................. 52<br />
APPENDIX A: ...................................................................................................................... 53<br />
6.1 Spectrum Details..................................................................................................... 53<br />
6.2 Almen Definiti<strong>on</strong>.................................................................................................... 53<br />
6.3 Saturati<strong>on</strong> Curve ..................................................................................................... 54<br />
7.4 Surface Roughness.................................................................................................. 56