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Structural Health Monitoring Approach to the Aerospace Structures

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In the article only selected information regarding the SHM applications has been presented. These applications are associated with damage detection and damage growth monitoring. That approach has got crucial influence on the aircraft maintenance procedures. SHM ensures higher reliability and safety of the structures as well as repair monitoring. Right now in the AFIT, there is being conducted research work focused on the application of the SHM system for the integration with the aerospace structures for periodical and on-line monitoring.
Słowa kluczowe
Rocznik
Tom
Strony
14--18
Opis fizyczny
Bibliogr. 11 poz., fot., rys., wykr.
Twórcy
autor
  • Air Force Institute of Technology, Warsaw, Poland
Bibliografia
  • [1] (1997). Aging of U.S. Air Force Aircraft. USA, Washington D.C.: National Academy Press. (NMAB-488-2)
  • [2] Dragan, K. (2006). In-service Flaw Detection and Quantification on the MiG-29 Composite Vertical Tail Skin. In the 9th European Conference on Non-Destructive Testing, Berlin, 25-29 Września 2006.
  • [3] Rücker, W. (2006). SAMCO Final Report 2006, Guideline for Structural Health Monitoring. Berlin: Federal Institute of Materials Research and Testing (BAM).
  • [4] Giurgiutiu, V. (2008). Structural Heath Monitoring and NDE - An Air Force Office of Scienific Research Structural Mechanics Program Perspective. In the 4th European Workshop on SHM, Kraków, July 2-4 2008, (35 - 39).
  • [5] Speckmann, H., & Henrich, R. (2004). Structural Health Monitoring (SHM) - Overview On Technologies Under Development. In the 16th WCNDT 2004 - World Conference on NDT, Canada: Montreal, August 30 - Sep 3 2004.
  • [6] Light Utility Helicopter Safety in Australia, RESEARCH PAPER BE04/73, Australian Transport Safety Bureau (ATSB), June 2004.
  • [7] Web page http://www.ntsb.gov/publictn/1996/SIR9603.pdf
  • [8] Shaniavski, A., A. (2004). Scale levels for fatigue fracture mechanisms of in-service crack growth in longerons of helicopter rotor blades. International Journal of Fracture. 128 (1), p. 17-24. DOI: 10.1023/B:FRAC.0000040960.52699.b9.
  • [9] Chronkite, J., D. (1993). Practical Application of Health and Usage Monitoring (HUMS) to Helicopter Rotor, Engine and Drive System. In the 49th Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society.
  • [10] Dragan, K. (2009). NDE activities connected with Service Life Extension of Main Rotor Blades of Polish Military Helicopters. In the 12th Aging Aircraft Conference, Kansas City, USA, 4-7 May 2009.
  • [11] Graff, K., F. (1991). Waves motion in elastic solids. New York: Dover Publications, Inc.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-715a812e-918a-47ed-8cfe-1d962f23c8a6
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