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Monitoring of Crack Growth in a Structure Under a Composite Patch

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In civil as well as in military aviation, boron, carbon and aramid fiber reinforced composites are employed for the repair of metal structures. After such composite bonded repairs, the monitoring of the repaired structure along with the composite patch and its bond is necessary. The paper describes the possibilities of utilizing NDT methods for periodical check-ups and examinations. Also, a novel approach to continuous monitoring of the repaired structure is presented.
Słowa kluczowe
Rocznik
Tom
Strony
103--111
Opis fizyczny
Bibliogr. 12 poz., fot., rys., tab., wykr.
Twórcy
  • Air Force Institute of Technology, Warsaw, Poland
autor
  • Air Force Institute of Technology, Warsaw, Poland
autor
  • Air Force Institute of Technology, Warsaw, Poland
autor
  • Air Force Institute of Technology, Warsaw, Poland
Bibliografia
  • [1] Sałaciński M., Synaszko P., Kornas Ł. (2010). Periodyczne Monitorowanie Metalowej Struktury Samolotu Po Wykonanej Naprawie Metodą Composit Bonded Repair, Krajowa Konferencja Badań Nieniszczących, Szczyrk, 2010.
  • [2] Baker, A., Chester, R. & Mazza, J. (2003). Bonded Repair Technology for Aging Aircraft. Ageing Mechanisms and Control. Specialists’ Meeting on Life Management Techniques for Ageing Air Vehicles. [Technical Report, RT=-MP-079(II)]
  • [3] Baker, A., Rose, F. & Jones, R. (2002). Advances is the Bonded Composite Repair of Metallic Aircraft Structure,Vol.1, Victoria, Australia.
  • [4] U.S. Department of Transportation Federal Aviation Administration. (2003). Guidelines for the Development of Process Specifications, Instructions, and Controls for the Fabrication of Fiber-Reinforced Polymer Composites. Office of Aviation Research Washington. (DOT/FAA/AR-02/110)
  • [5] Baker, A., Rose, F. & Jones, R. (2002). Advances is the Bonded Composite Repair of Metallic Aircraft Structure,Vol.2, Victoria, Australia,
  • [6] Růžička M. , Kulíšek V., Henzl P., Krimbalis P., Dvořák M., Běhal J. (2007). Health Monitoring Of Composite Repairs Of Aircraft Structures, NDT for Safety, November 07-09, 2007, Czech Republic, Prague.
  • [7] Baker, A. (2006). Structural Health Monitoring of a Bonded Composite Patch Repair on a Fatigue-Cracked F-111C Wing., Victoria, Australia: Air Vehicles Division. (DSTO-RR-0335)
  • [8] Dolce, F. (2010). Role of NDI in ABDR Assesment, Equipment & Logistics. Conference Battle Damage Repair Techniques and Procedure on Air Vehicles, Prague - Czech Republic, Kosice - Slovak, Warsaw - Poland, 2010.
  • [9] Lewitowicz, J., Loroch, L., Manerowski, J. (2006). Problemy badań i eksploatacji techniki lotniczej, Tom 6. Warszawa: Wydawnictwo ITWL.
  • [10] Dragan, K., Synaszko, P., Sałaciński, M., Klimaszewski, S. (2010). Damage Detection And Failure Mode Distribution For The MiG-29 Vertical Stabilizer. Conference Aircraft Airworthnees and Sustainment, Austin, Texsas, 2010.
  • [11] PRI Research and Development Corp. (2001). MOI Magneto/Optic Eddy Current Imager. Operator’s Manual, Torrance, USA.
  • [12] Uhl, T., Ostachowicz, W., Holnicki-Szulc, J. (2008). Structural Health Monitoring, Poland.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-c4d3c0c1-2b00-47ff-a977-0f394db2d25e
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