Damage Detection and Size Quantification of FML with the Use of NDE

• Autorzy: Dragan K. , Kornas Ł. , Kosmatka M. , Leski A. , Sałaciński M. , Synaszko P. , Bieniaś J.

Identyfikatory

DOI

10.2478/v10164-012-0051-8

• Języki publikacji: EN

Abstrakty

EN

Composite materials have been developed in recent years. A new generation of structural composite materials for advanced aircraft is Fibre Metal Laminates (FML). They are hybrid composites consisting of alternating thin layers of metal sheets and fiber-reinforced composite material. FMLs have both low weight and good mechanical properties (high damage tolerance: fatigue and impact characteristics, corrosion and fire resistance). Quality control of materials and structures in aircraft is an important issue, also for Fibre Metal Laminates. For FML parts, a 100% non-destructive inspection for internal quality during the manufacturing process is required. In the case of FML composites, the most relevant defects that should be detected by non-destructive testing are porosity and delaminations. In this paper, a number of different non-destructive methods for the inspection of Fibre Metal Laminates were studied. The possibility of quality control of manufactured FML laminates - detection of defects as well as the procedures and processes are presented and discussed.

Słowa kluczowe

EN

fibre metal laminates; composites; non-destructive testing

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Fatigue of Aircraft Structures
• Rocznik: 2012
• Tom: Iss. 4
• Strony: 5--9
• Opis fizyczny: Bibliogr. 5 poz., rys., wykr., wzory

Twórcy

autor

Dragan K.

• Air Force Institute of Technology, Warsaw, Poland

autor

Kornas Ł.

• Air Force Institute of Technology, Warsaw, Poland

autor

Kosmatka M.

• Air Force Institute of Technology, Warsaw, Poland

autor

Leski A.

• Air Force Institute of Technology, Warsaw, Poland

autor

Sałaciński M.

• Air Force Institute of Technology, Warsaw, Poland

autor

Synaszko P.

• Air Force Institute of Technology, Warsaw, Poland

autor

Bieniaś J.

• Lublin University of Technology, Lublin, Poland

Bibliografia

• [1] K. Dragan, J. Bieniaś, M. Sałaciński, P. Synszako (2011). Inspection methods for quality control of fibre metal laminates in aerospace components. Composites. No 2, 130-135.
• [2] G. Reyes Villanueva, W.J. Cantwell (2004). The high velocity impact response of composite and FML-reinforced sandwich structures. Composites Science and Technology. 64(1), 35-54.
• [3] S.H. Song, Y.S. Byun, T.W. Ku, W.J. Song, J. Kim, B.S. Kang (2010). Experimental and Numerical Investigation on Impact Performance of Carbon Reinforced Aluminum Laminates. Journal of Materials Science & Technology. 26(4), 327-332.
• [4] Edson Cocchieri Botelho, Rogério Almeida Silva, Luiz Cláudio Pardini, Mirabel Cerqueira Rezende (2006). A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures. Materials Research. 9(3), 247-256.
• [5] Instytut Techniczny Wojsk Lotniczych. (2011). Ocena możliwości diagnostycznych poszczególnych metod do wybranych rodzajów uszkodzeń. Określenie wykrywalności i dokładności poszczególnych metod, Warszawa. (Sprawozdanie Nr 146/31/2011).

Uwagi

EN

The work was supported by the Operational Programme - Innovative Economy (IE OP) financed from the European Regional Development Fund - Project "Modern Material Technologies in Aerospace Industry", No. POIG.01.01.02-00-015/08-00.

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.