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Establishment of Aerospace Composite Materials Data Center for Qualification

  • 투고 : 2015.12.04
  • 심사 : 2015.12.29
  • 발행 : 2015.12.31

초록

It is well known that the polymer matrix composite materials have good specific strength, making them appropriate for use in transport vehicle. Since the property of composite materials can be obtained only after manufacturing parts, the property depends on greatly on the fabrication process, which is different from metallic system. Therefore, in order to use composite materials for aircraft, the certifying agency requires a robust database with extensive tests and proof of the process unlike metals. Recently developed material qualification methodology by NCAMP (National Center for Advanced Materials Performance) has been accepted by FAA and EASA and can be applied to type certificate reducing time and cost of developing a composite materials database for aircraft application. This paper summarizes a study to establish the composite materials database to apply the NCAMP methodology to composite materials characterization for composite aircraft and to provide the effective materials database through Aerospace Composite Materials Data Center to be approved by Korea Civil Aviation Certification Agency.

키워드

참고문헌

  1. Hale, J., Aero Quarterly, Boeing.com/commercial/aeromagazine, April 2006, pp. 17-23.
  2. Tomblin, J.S., Ng, C.Y., and Raju, K.S., "Material Qualification and Equivalency for Polymer", Matrix Material Systems," FAA Technical Report, DOT/FAA/AR-03/19, September 2003, NTIS, Springfield, VA. USA.
  3. Tomblin, J., Statement before the Subcommittee on Science, Technology & Space, U.S. Senate Commerce Committee, February 27, 2003.
  4. Lee, H.-S., "Material Qualification, Equivalency, and Acceptance Test for Aerospace Composite Materials", Journal of the Korean Society for Composite Materials, Vol. 19, No. 3, 2006, pp. 1-6.
  5. Ilcewicz, L., "Composite Safety and Certification Initiatives", 2012 Conference of Society of Advanced Materials and Process Engineering, May 23, 2012, Baltimore, MD, U.S.A
  6. Ilcewicz, L., "Long-Term Planning Efforts", in Executive Committee Meeting, 49th MIL-HDBK-17 Coordination Group Meeting, 5 December 2005 Santa Monica, CA.
  7. FAA Memorandum AIR100-2010-120-003, "Acceptance of Composite Specifications and Design Values Developed using the NCAMP Process", September 20, 2010.
  8. EASA CM-S-004 Issue: 01 "Composite Materials-Shared Databases, Acceptance of Composite Specifications and Design Values Developed using the NCAMP Process", European Aviation Safety Agency Certification Memoranda, September 4, 2013.
  9. Press Release, U.S.-Korea, Revised the Bilateral Aviation Safety Agreement, Airworthiness Division, Ministry of Land, Infrastructure and Transport, October 28, 2014.
  10. AC21-23B, November 17, 2004, Federal Aviation Administration.
  11. Lee, H.-S., Yoon, J.-H., Yoo, J.-T., and Min, K.J., "A Case Study of Composite Materials Characterization for Certification", 2015 Conference of Society of Advanced Materials and Process Engineering, Baltimore, MD, U.S.A. 2015.5.18.
  12. ISO/IEC 17025, General Requirements for the Competence of Testing and Calibration Laboratories, International Organization for Standardization.
  13. AGATE-WP3.1-031200-130-Design Guideline, National Institute for Aviation Research, March 1, 2002, Wichita, KS, U.S.A.
  14. 59th Polymer Matrix Composites Coordination Group Meeting, August 20-23, 2012, Boston, MA. USA.
  15. Composite Materials Handbook-17-1G(2012), SAE International, Warrendale, PA., USA.
  16. Ng, Y., "NCAMP Qualification Training", October 24, 2015, Korea Aerospace Research Institute.
  17. Clarkson, E., "NCAMP Data Analysis Training", September 21, 2015, Korea Aerospace Research Institute.
  18. Davies, C.R., 2nd FAA Workshop on Composite Material Control, September 16-18, 2003, Chicago, Il. USA.
  19. Ng, Y., "Differences between CMH-17 Rev G and NCAMP", 56th Polymer Matrix Composites Coordination Group Meeting, 19 - 22 July 2010 - Costa Mesa, CA. USA.
  20. Technical Report, "Development of Composite Materials Database and Data Sharing System for Small Aircraft", Air Transportation Advancement Program of the Korea Institute of Construction & Transportation Technology Evaluation and Planning, May 2015, Korea Ministry of Land, Infrastructure and Transport.
  21. Civil Aviation Certification Agency, Technical Guide 12, "Guidance on Polymer Matrix Composite Systems Qualification", July 2013, Korea Ministry of Land, Infrastructure and Transport.
  22. Freeman, T., Tomblin, J., and Ng, Y., 49th MIL-HDBK-17 Coordination Group Meeting, 5-9 December 2005 Santa Monica, CA.
  23. McCarvill, W., Ward, S., Bogucki, G., and Tomblin, J.S., "Guidelines and Recommended Criteria for the Development of a Material Specification for Carbon Fiber/Epoxy Unidirectional Prepregs", FAA Technical Report, DOT/FAA/AR-02/109, NTIS, March 2003, Springfield, VA. USA.
  24. Bogucki, G., McCarvill, W., Ward, S., and Tomblin, J.S., "Guidelines for the Development of Process Specifications, Instructions, and Controls for the Fabrication of Fiber-Reinforced Polymer Composites", FAA Technical Report, DOT/FAA/AR-02/110, NTIS, March 2003, Springfield, VA. USA.
  25. Public Notice 2015-28, "Notice of New, Renew, and Cancelation of National Standard Reference Data Center", January 28, 2015, Korean Minister of Trade, Industry and Energy.
  26. FAA AC No: 20-107B, Composite Aircraft Structure, September 8, 2009.
  27. Proceedings of the 60th Polymer Matrix Composites Coordination Group Meeting, April 8, 2015, Seattle, WA. USA.
  28. Lee, H.-S., Lee, S.A., and Choi, J.-U., "Development of Materials Characterization Procedure for Composite Aircraft", Applied Mechanics and Materials Vols. 325-326, 2013, pp. 46-49. https://doi.org/10.4028/www.scientific.net/AMM.325-326.46
  29. https://www.kolas.go.kr
  30. Tomblin, J., Tauriello, J.D., and Doyle, S.P., "A Composite Material Qualification Method That Results in Cost, Time and Risk Reduction", Proceedings of the 32nd International SAMPE Technical Conference, November 5-9 2000, Boston, MA. USA
  31. https://www.cmh17.org/RESOURCES/StatisticsSoftware.aspx
  32. Shyprykevich, P., "The Role of Statistical Data Reduction in the Development of Design Allowables for Composites, Test Methods for Design Allowables for Fibrous Composites," 2nd Volume, ASTM STP 1003, C.C. Chamis, Ed., American Society for Testing and Materials, Philadelphia, PA, 1989, pp. 111-135.