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Carbon Fibre Polymer Matrix Structural Composites

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Aerospace Materials and Material Technologies

Part of the book series: Indian Institute of Metals Series ((IIMS))

Abstract

This chapter concisely surveys the applications and properties of polymer matrix structural composites (PMCs), concentrating on carbon fibre reinforced composites. These are the most widely used composite materials, notably in aerospace, and are commonly called carbon fibre reinforced plastics (CFRP). A major source for this chapter is Baker et al. (Composite materials for aerospace structures. American Institute of Aeronautics and Astronautics, Inc., Reston, Virginia, USA, 2nd edn, 2004).

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References

  1. Baker A, Dutton S, Kelly D (2004) Composite materials for aerospace structures, 2nd edn. American Institute of Aeronautics and Astronautics Inc., Reston, VA 20191, USA

    Google Scholar 

  2. Prasad NE, Gokhale AA, Wanhill RJH (eds) (2014) Aluminum–lithium alloys: processing, properties and applications. Butterworth-Heinemann, Elsevier Inc., Oxford, UK

    Google Scholar 

  3. Wanhill RJH (2013) Aerospace applications of aluminum-lithium alloys. In: Prasad NE, Gokhale AA, Wanhill RJH (eds) Aluminum-lithium alloys, processing, properties and applications. Butterworth-Heinemann, Elsevier Inc., Oxford, UK, pp 503–535

    Google Scholar 

  4. Grimshaw MN, Grant CG, Diaz JML (2001) Advanced technology tape laying for affordable manufacturing of large composite structures. In: Repecka L, Garemi FF (eds) 2001: a materials and processes odyssey. Society for the Advancement of Material and Process Engineering, Covina, CA 91724-3759, USA, pp 2484–2494

    Google Scholar 

  5. Department of Defense Handbook (2002) Composite materials handbook. Volume 1, polymer matrix composites guidelines for characterization of structural materials, MIL-HDBK-17-1F. Document Automation and Production Service (DAPS), Philadelphia, PA 19111-5094, USA

    Google Scholar 

  6. Department of Defense Handbook (2002) Composite materials handbook. Volume 2: polymer matrix composites materials properties, MIL-HDBK-17-2F. Document Automation and Production Service (DAPS), Philadelphia, PA 19111-5094, USA

    Google Scholar 

  7. Department of Defense Handbook (2002) Composite materials handbook. Volume 3: polymer matrix composites materials usage, design, and analysis, MIL-HDBK-17-3F. Document Automation and Production Service (DAPS), Philadelphia, PA 19111-5094, USA

    Google Scholar 

  8. Mouritz AP (2012) Introduction to aerospace materials. Woodhead Publishing Limited, Cambridge, UK

    Book  Google Scholar 

  9. AGARD Report 785 (1992) The utilization of advanced composites in military aircraft. Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine, France

    Google Scholar 

  10. Peel CJ (1990) The development of aluminium lithium alloys: an overview. In: New light alloys. AGARD Lecture Series No. 174, Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine, France, pp 1-1–1-55

    Google Scholar 

  11. Campbell FC (2010) Structural composite materials. ASM International, Materials Park, OH 44073-0002, USA

    Google Scholar 

  12. Wright GA (1992) An overview of concerns relating to fluid effects on composites. In: The utilization of advanced composites in military aircraft. AGARD Report 785, Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine, France, pp 13-1–13.6

    Google Scholar 

  13. Brosius D (2003) Advanced pultrusion takes off in commercial aircraft structures. Gardner Business Media, Inc., Cincinnati, OH 45244, USA. www.compositesworld.com

  14. Lequeu P, Lassince P, Warner T (2007) Aluminium alloy development for the Airbus A380—Part 2. Adv Mater Processes 165(7):41–44

    Google Scholar 

  15. Vogelesang LB (2004) Fibre metal laminates, the development of a new family of hybrid materials. In: Guillaume G (ed) ‘ICAF 2003: fatigue of aeronautical structures as an engineering challenge, vol I, pp 3–27. Engineering Materials Advisory Services, Warrington, UK

    Google Scholar 

  16. Halpin JC, Kim H (2007) Managing impact risk for composite structures: unifying durability and damage tolerance perspective. FAA/EASA/Industry composite damage tolerance and maintenance workshop, 7–11 May 2007, Amsterdam, the Netherlands

    Google Scholar 

  17. Halpin JC, Kim H (2009) Managing damage threats for composite structures: unifying durability and damage tolerance perspective. In: 3rd FAA/EASA/Industry composite damage tolerance and maintenance workshop, 1–5 June 2009, Tokyo, Japan

    Google Scholar 

  18. Fawcett AJ Jr, Oakes GD (2006) Boeing composite airframe damage tolerance and service experience. In: FAA/Wichita State University composite damage tolerance & maintenance workshop, 19–21 July 2006, Chicago, Illinois, USA

    Google Scholar 

  19. Waite S (2006) Damage/defect types and inspection—some regulatory concerns. FAA/Wichita State University composite damage tolerance & maintenance workshop, 19–21 July 2006, Chicago, Illinois, USA

    Google Scholar 

  20. Clark G, Saunders DS (1991) Morphology of impact damage growth by fatigue in carbon fibre composite laminates. Mater Forum 15:333–342

    Google Scholar 

  21. Ilcewicz L (2006) Composite damage tolerance and maintenance safety issues. In: FAA/Wichita State University composite damage tolerance & maintenance workshop, 19–21 July 2006, Chicago, Illinois, USA

    Google Scholar 

  22. Fualdes C, Thévenin R (2006) Composites @ airbus damage tolerance methodology. FAA/Wichita State University composite damage tolerance & maintenance workshop, 19–21 July 2006, Chicago, Illinois, USA

    Google Scholar 

  23. Ilcewicz L (2009) Updates to AC 20-107B ‘Composite Aircraft Structure’. In: 3rd FAA/EASA/Industry composite damage tolerance and maintenance workshop, 1–5 June 2009, Tokyo, Japan

    Google Scholar 

  24. Waite S (2014) Composite materials: developing continued airworthiness issues. In: SIASA (Support to the Improvement of Aviation Safety in Africa) workshop on technology evolution—impact on airworthiness, 23–24 Sept 2014, Windhoek, Namibia

    Google Scholar 

  25. Federal Aviation Administration (2010) Composite aircraft structure. Advisory Circular FAA AC-20-107B, Change 1, 24 Aug 2010. U.S. Department of Transportation, Washington, DC 20590, USA

    Google Scholar 

  26. Smith RA (2009) Composite defects and their detection. In: Rawlings RD (ed) Materials science and engineering, vol III. Encyclopedia of Life Support Systems, UNESCO, Paris, France, pp 103–143

    Google Scholar 

  27. Ilcewicz LB (2004) Composite technology development for commercial airframe stru ctures. In: Kelly A, Zweben C, Bader MG, Kedward KT, Sawada Y (eds) Comprehensive composite materials, volume 6: design and applications. Elsevier Science Ltd., Oxford, UK, pp 121–163

    Google Scholar 

  28. Modlin CT, Zipay JJ (2014) The 1.5 & 1.4 ultimate factors of safety for aircraft and spacecraft—history, definition and applications. ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/2 140011147

    Google Scholar 

  29. Calomfirescu M, Hickethier H (2010) Damage tolerance of composite structures in aircraft industry. Composites Europe 2010, 14–16 Sept 2010, Essen, Germany

    Google Scholar 

  30. Ball DL, Norwood DS, TerMaath SC (2006) Joint Strike Fighter airframe durability and damage tolerance certification. AIAA paper 2006-1867, In: 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 1–4 May 2006, Newport, Rhode Island, USA

    Google Scholar 

  31. Gorss J (2003) High performance carbon fibers. American Chemical Society Commemorative Booklet, 17 Sept 2003, Washington, DC 20036, USA

    Google Scholar 

  32. Dow MB, Smith DL (1989) Damage tolerant composite materials produced by stitching carbon fabrics. In: Proceedings of the 21st International SAMPE Technical Conference 25–28 Sept 1989, Atlantic City, New Jersey. Society for the Advancement of Materials and Process Engineering, Covina, CA 91724-3759, USA, pp 595–605

    Google Scholar 

  33. Davis JG Jr, Bohon HL (eds) (1991) First NASA advanced composites technology conference. NASA Conference Publication 3104, Parts 1 and 2, NASA Scientific and Technical Information Program STI Support Services, NASA Langley Research Center, Hampton, VA 23681-2199, USA

    Google Scholar 

  34. NASA Facts (1997) The advanced stitching machine: making composite wing structures of the future. National Aeronautics and Space Administration FS-1997-08-31-LaRC, Aug 1997, Langley Research Center, Hampton, VA 23681, USA

    Google Scholar 

  35. Velicki A, Thrash P, Jegley D (2009) Airframe development for the Hybrid Wing Body aircraft. Paper AIAA 2009-932, 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 5–8 Jan 2009, Orlando, Florida, USA

    Google Scholar 

  36. Velicki A, Jegley D (2011) PRSEUS development for the Hybrid Wing Body aircraft. Paper AIAA 2011-7025, AIAA centennial of naval aviation forum “100 years of achievement and progress”. 21–22 Sept 2011, Virginia Beach, Virginia, USA

    Google Scholar 

  37. Velicki A, Jegley D (2014) PRSEUS structural concept development. Paper AIAA-2014-0259, 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 13–17 Jan 2014, National Harbor, MD 20745, USA

    Google Scholar 

  38. Jegley DC, Velicki A (2015) Development of the PRSEUS multi-bay pressure box for a Hybrid Wing Body vehicle. Paper in: AIAA 2015 Science and Technology Forum and Exposition, 5–9 Jan 2015, Kissimmee, Florida, USA

    Google Scholar 

  39. Liebeck RH (2004) Design of the blended wing body subsonic transport. J Aircr 41(1):10–25

    Article  MathSciNet  Google Scholar 

  40. Blaiszik BJ, Kramer SLB, Olugebefola SC, Moore JS, Sottos NR, White SR (2010) Self-healing polymers and composites. Annu Rev Mater Res 40:179–211

    Article  Google Scholar 

  41. Smith JG Jr (2012) An assessment of self-healing fiber reinforced composites. NASA Technical Memorandum NASA/TM-2012-217325, NASA Center for Aerospace Information, Hanover, MD 21076-1320, USA

    Google Scholar 

  42. Yin T, Zhou L, Rong MZ, Zhang MQ (2008) Self-healing woven glass fabric/epoxy composites with the healant consisting of micro-encapsulated epoxy and latent curing agent. Smart Mater Struct 17(1), 15019 (8 pp)

    Google Scholar 

Bibliography

  1. Tong L, Mouritz AP, Bannister MK (2002) 3D fibre reinforced polymer composites. Elsevier Science Ltd., Oxford, UK

    Google Scholar 

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Correspondence to R. J. H. Wanhill .

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Wanhill, R.J.H. (2017). Carbon Fibre Polymer Matrix Structural Composites. In: Prasad, N., Wanhill, R. (eds) Aerospace Materials and Material Technologies . Indian Institute of Metals Series. Springer, Singapore. https://doi.org/10.1007/978-981-10-2134-3_14

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  • DOI: https://doi.org/10.1007/978-981-10-2134-3_14

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