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The increasing use of composite structures in aircraft constructions has made it necessary to develop repair methods that will restore the component’s original design strength without compromising its structural integrity. In this paper, the complex repair technology of the composite wing of a light plane, which was damaged during an aircraft crash, is described. The applied repair scheme should meet all the original design requirements for the plane structure.
Słowa kluczowe
Rocznik
Tom
Strony
149--157
Opis fizyczny
Bibliogr. 3 poz.
Twórcy
autor
- Faculty of Mechanical Engineering and Robotics, AGH University of Science and Technology, al. Mickiewicza, 30-059 Cracow, Poland
autor
- Faculty of Mechanical Engineering and Robotics, AGH University of Science and Technology, al. Mickiewicza, 30-059 Cracow, Poland
autor
- Polytechnical Institute, State Higher Vocational School Stanislaus Pigon in Krosno, Rynek 1, 38-400 Krosno, Poland
Bibliografia
- 1. Kelly Tony, Bill Clyne. 1999. “Composite materials: reflections on the first half century”. Physics Today 52(11): 37-41. ISSN 0031-9228. DOI: 10.1063/1.882882.
- 2. Katnam Kali-Babu, Lucas Da Silva, Trevor Young. 2013. “Bonded repair of composite aircraft structures: a review of scientific challenges and opportunities”. Progress in Aerospace Sciences 61(2): 26-42. ISSN 0376-0421. DOI: 10.1016/j.paerosci.2013.03.003.
- 3. Soutis Constantinos. 2005. “Fibre reinforced composites in aircraft construction”. Progress in Aerospace Sciences 41(2): 143-151. ISSN 0376-0421. DOI: 10.1016/j.paerosci.2005.02.004.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-d2fa675a-81e2-4a3f-8194-291ca29c924e