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Aspects of battle damage repair of helicopter structures

Published online by Cambridge University Press:  03 February 2016

J. Wang  and
A. Baker
J. Wang
Affiliation:
Air Vehicles Division, Defence Science and Technology Organisation, Australia
A. Baker
Affiliation:
Defence Science and Technology Organisation, Co-operative Research Centre for Advanced Composite Structures, Australia
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Abstract

This paper summarises recent research conducted at the Defence Science and Technology Organisation in the area of aircraft battle damage repair, covering aspects such as ballistic testing, ballistic damage prediction, non-destructive damage inspection, structure residual-strength assessment, repair materials and techniques, repair design approaches, repair implementation and demonstration. The research has been focused on military helicopter composite structures. This paper provides an overview of a wide range of research conducted and detailed information in selected areas. Considerations for future research directions are also briefly discussed.

Type
Research Article
Information
The Aeronautical Journal , Volume 114 , Issue 1155 , May 2010 , pp. 321 - 332
Copyright
Copyright © Royal Aeronautical Society 2010 

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References

1. Srull, D.W., Simms, E.D. and Schaible, R.A., Battle damage repair of tactical weapons: An Assessment (AD-A213117) Logistics Management Institute, Bethesda MD, August 1989.Google Scholar
2. Resnyansky, A.D., The impact response of composite materials involved in helicopter vulnerability assessment: Literature Review. Defence Science and Technology Organisation. DSTO-TR-1842, 2006.Google Scholar
3. Jacobson, M., Addendum to design manual for impact damage tolerant aircraft structure, AGARD-AG-238. Northrop Corporation Aircraft Division, Hawthorne, CA90250, USA, 1998.Google Scholar
4. Wang, J and Mirabella, L., Ballistic damage on structurally loaded composite panels, 2007, J Battlefield Technology, 10, (1).Google Scholar
5. http://www.tip.csiro.au/IMP/SmartMeasure/BaNDIcoot.htm.Google Scholar
6. Wang, J. and Bartholomeusz, R., Ballistic damage in carbon/epoxy composite panels, J Battlefield Technology, 2004, 7, (1).Google Scholar
7. Penetration equations handbook for kinetic-energy penetrators, joint technical co-ordinating group for munitions effectiveness, 61JTCG/ME-E-AS-77-16.Google Scholar
8. LS-DYNA Version 960, Livermore Software Technology Corporation, Livermore, California, USA, 2002.Google Scholar
9. Resnyansky, A.D and Katselis, G., Ballistic and material testing procedures and test results for composite samples. Defence Science and Technology Organisation, 2004. DSTO-TR-1617.Google Scholar
10. Carstensen, T., Composite field repair inspection, materials and demonstrations conducted under survivable affordable repairable airframe program (SARAP), AHS Structures and Survivability Specialists’ Meeting, 25-27 October, Williamsburg, VA, USA, 2005.Google Scholar
11. SP Product Catalogue. Gurit Composite Technologies. Mona Vale, NSW, Australia, 2004.Google Scholar
12. Hysol, E.A., 9396C-2 Epoxy paste adhesive data sheet. Loctite Aerospace. USA. Internet address: www.loctite.com Google Scholar
13. ACG LTM45-1 Component prepreg data sheet. Advanced Composites Group Ltd. DERBY, UK. Web address: www.advanced-composites.com.Google Scholar
14. ACG XVTA262 Film Adhesive Data Sheet. Advanced Composites Group Ltd. DERBY, UK. Web address: www.advanced-composites.com.Google Scholar
15. Wang, J., (1) Experimental evaluation of mechanical properties and lap joint bond strength of a UV curable composite material system, DSTO Report C07/1030689/1/AVD, 2007; (2) Enhancement of bonding strength of a UV curable composite material system, DSTO Report C07/1030689/2/AVD, 2008.Google Scholar
16. HexPly® M18/1 180°C curing epoxy matrix, Product datasheet, Hexel, June 2005.Google Scholar
17. Brunel, J.E. and Gresle, B., Battle field damage repair of a helicopter composite frame-to-skin junction. Accepted for publication in J Battlefield Technology.Google Scholar
18. Rider, A., Surface treatments for field level bonded repairs to aluminium and titanium structure. Defence Science and Technology Organisation. DSTO-TR-2153. 2008.Google Scholar
19. Wang, J., Gunnion, A. and Baker, A., Battle damage repair of a frame-skin junction of Tiger helicopter – Depot repair. Accepted for publication in J Composites: Part A.Google Scholar
20. Wang, J., Stankiewicz, M., Zhou, Z. and Baker, A., Battle damage repair of a frame-skin junction of Tiger helicopter – a sole external repair approach. Accepted for publication in J Composite Structures.Google Scholar
21. Hart-Smith, L.J., Adhesive-bonded double lap joints, NASA Langley Research Center Report NASA CR-112235, 1973.Google Scholar
22. Composite materials and adhesive bonded repairs, engineering and design procedures, Royal Australian Air Force Publication, AAP 7021.016-1, 2003.Google Scholar