Surface Modification and Repair for Aircraft Life Enhancement and Structural Restoration

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Abstract:

Maintenance of ageing military aircraft structures encompasses both engineering and scientific management. In support of this, surface modification and repair methods are used on an opportunity basis to extend the life of aircraft in terms of fatigue and safety. Often, certain surface modification technologies have proved to be both cost effective and amenable for safe application. Some candidate technologies include shot peening, cold spray, deep surface rolling, friction stir welding, laser shock peening, and laser cladding. Whilst some technologies have been successfully applied to Australian Defence Force (ADF) aircraft in the past, some newer technologies are also being considered. The supersonic particle deposition (SPD) technology also known as cold spray coating has been recently approved for application on a helicopter gear box. Another technology of significance to ADF application is Laser Cladding (LC) technology. This paper briefly summarises the research work on these technologies at DSTO and discusses potential applications for aircraft components in the near future. It also provides an analysis of technologies and their potential advantages and disadvantages.

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Periodical:

Materials Science Forum (Volumes 654-656)

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763-766

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Online since:

June 2010

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[1] P.K. Sharp, J.Q. Clayton and G. Clark, Fat. Fract. Eng. Mater. Struct., Vol. 17 (1994), p.243.

Google Scholar

[2] Q. Liu, S.A. Barter and G. Clark, (2002a), The Australian Conference of Applied Mechanics 2002 (ACAM 2002), Sydney, February 20-22, (2002).

Google Scholar

[3] P. K. Sharp, S. A. Barter and G. Clark, DSTO Technical Note, DSTO-TN-0279, Defence Science and Technology Organisation Commonwealth of Australia, (2000).

Google Scholar

[4] A. H. Clauer and J.L. Dulaney, 3rd National Turbine Engine High Cycle Fatigue Conference, February 2-5, San Antonio Texas, (1998).

Google Scholar

[5] SAE Aerospace, Aerospace material Specification-Laser peening, AMS 2546, August (2004).

Google Scholar

[6] Q. Liu, C.H. Yang, K. Ding, S.A. Barter and L. Ye, Fat. Fract. Eng. Mater. Struct., Vol. 30 (2007), p.1110.

Google Scholar

[7] W. Zhuang and B. Wicks, ASME J. Engng for Gas Turbines & Power, Vol. 125 (2003), p.1021.

Google Scholar

[8] F. Raletz, M. Vardelle and G. Ezo'o, Surface & Coatings Technology, Vol. 201 (2006), p. (1942).

Google Scholar

[9] D.R. Gerrard, A. Butler, V. Champagne, P. Leyman, D. Helfrich, ASM-TSS Cold Spray Conference, Akron, USA September (2007).

Google Scholar

[10] B. Hinton, T. Trueman, S. Galea, I. Cole, S. Miah, L. Davidson and Q. Liu, Conference on Corrosion & Prevention 2008, Wellington, New Zealand, 16 - 19 November (2008).

Google Scholar

[11] P.E. Denney and R. Duhamel, Industrial laser Solutions, Vol. 13 (1998), p.19.

Google Scholar

[12] Tam, S.C., Williams, R. and Yang, L.J., J. Mater. Proc. Technol., Vol. 23 (1990), p.177.

Google Scholar

[13] K. C, Meinert, Jr. and P. Bergan, Laser Materials Processing, Laser Institute of America, 87 (Part 2), 1999, F49-F57.

Google Scholar

[14] D. Waldron, I st Inter. Symp. on Friction Stir Welding, Rockwell Science Center, Thousand Daks, California, 14-16 June, (1999).

Google Scholar

[15] D. Lohwasser, International Institute of Welding Annual Report, IIW Doc. IX-1982-00, (2000).

Google Scholar

[16] G. Clark, DSTO Technical Note Report, DSTO-TN-0489, Defence Science and Technology Organisation, Commonwealth of Australia, (2003).

Google Scholar