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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

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