SavedAdd your journal

Journals / Mühendis ve Makina / 2019 / Cilt: 60 - Sayı: 697

A Review on Fiber Metal Laminates and Their Usage in Aerospace Industry

Fiber Metal Laminatlar ve Uçak Sanayiinde Kullanımı Üzerine Bir İnceleme

Orhan GÜLCAN
Kazım TEKKANAT
Burhan ÇETİNKAYA
Pages
262–288
DOI
—
🏛️Bibliographic metadata and full text access for this article are provided via DergiPark.
DergiPark Record ↗
✨

AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

The aim of this study is to provide a broad literature review about the history of FML, their usage areas, variants and properties (static, fatigue, impact, corrosion and thermal resistance) and to suggest research areas in the future.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In todays competitive aerospace environment, it is very important to design and produce aircrafts with high performance and lightweights and in this context, to find new production processes and new production materials.
📊
Key Findings & Data:Forth is reason, Fiber metal laminates (FML) developed by Delft University, are special composite materials that can be used as an alternative to the conventional aluminium materials used in aircrafts for their high fatigue resistance.
💡
Conclusion & Impact:The aim of this study is to provide a broad literature review about the history of FML, their usage areas, variants and properties (static, fatigue, impact, corrosion and thermal resistance) and to suggest research areas in the future.
🔬Design:Review & Systematic Survey
📍Scope:Comprehensive Sample
⚙️Variables:Laminat · fiber · arall

Abstract

In todays competitive aerospace environment, it is very important to design and produce aircrafts with high performance and lightweights and in this context, to find new production processes and new production materials. Forth is reason, Fiber metal laminates (FML) developed by Delft University, are special composite materials that can be used as an alternative to the conventional aluminium materials used in aircrafts for their high fatigue resistance. The aim of this study is to provide a broad literature review about the history of FML, their usage areas, variants and properties (static, fatigue, impact, corrosion and thermal resistance) and to suggest research areas in the future.

Özet

Günümüzün rekabetçi havacılık ortamında, yüksek performanslı ve hafif uçakların tasarlanması, üretilmesi ve bu kapsamda, yeni üretim metodlarının ve yeni üretim malzemelerinin kullanılması önem arz etmektedir. Bu amaçla, Delft Üniversitesi tarafından geliştirilen Fiber metal laminatlar (FML), yüksek yorulma dirençlerinden dolayı, uçaklarda kullanılan geleneksel alüminyum malzemelere alternatif olarak kullanılabilecek özel kompozit malzemelerdir. Bu çalışmanın amacı FML’lerin tarihçesi, kullanım alanları, çeşitleri ve özellikleri (statik, yorulma, darbe, korozyonve ısı dayanımı) hakkında geniş bir literatür özeti sunmak ve ilerde yapılabilecek çalışmalar hakkında fikir vermektir.

🔖

Cite This Article

GÜLCAN, O., TEKKANAT, K., ÇETİNKAYA, B. (2019). A Review on Fiber Metal Laminates and Their Usage in Aerospace Industry. Mühendis ve Makina, Cilt: 60 - Sayı: 697, 262–288. https://ajindex.com/articles/294813

📄 Full Text PDF Viewer

📄

PDF görüntüleyici hazırlanıyor...

References (10)

  1. Vogelesang, L.B., Vlot, A. 2000. “Development of fibre metal laminates for advanced aerospace structures”, Journal of Materials Processing Technology, vol. 103, p. 1-5.
  2. Şen, İlhan. 2015. “Lay-up optimisation of fibre metal laminates: development of a design methodology for wing structures”, PhD Thesis, Delft University of Technology, The Netherlands. Sinmazçelik, T., Avcu, E., Bora, M. Ö., Çoban, O. 2011. “A review: Fibre metal laminates, background, bonding types and applied test methods”, Materials and Design, vol. 32, p. 3671-3685.
  3. Alderliesten, R. 2005. “Fatigue crack propagation and delamination growth in Glare”, PhD Thesis, Delft University of Technology, The Netherlands. Alderliesten R.C., Benedictus R. 2007. ”Fiber/metal composite technology for future primary aircraft structures”, 48th Aiaa/Asme/Asce/Ahs/Asc structures, structural dynamics, and materials conference, 23-26
  4. April, Honolulu, Hawaii. Vlot, A. 1993. “Impact properties of fibre metal laminates”, Composites Engineering, vol. 3, no. 10, p. 911-927.
  5. Gutowski, T. G. 1997. ”Advanced composites manufacturing”, First edition, John Wiley & Sons, New York, USA. Alderliesten, R. 2009. “On the development of hybrid material concepts for aircraft structures”, Recent Patents in Engineering, vol. 3, p. 25-38.
  6. Roebroeks, G. H. J. J., Hooijmeijer, P. A., Kroon, E. J., Heinimann, M. B. 2007. “The development of CentrAl”, First International Conference on Damage Tolerance of Aircraft Structures, Delft University of Technology, The Netherlands. Laliberte, J. F., Poon, C., Straznicky, P. V., Fahr, A. 2000. “Applications of fiber-metal laminates”, Polymer Composites, vol. 21, no. 4, p. 558-567.
  7. Müller, B., Hagenbeek, M., Sinke, J. 2016. “Thermal cycling of (heated) fibre metal laminates”, Composite Structures, vol. 152, p. 106-116.
  8. Vlot, A., Vogelesang, L.B., de Vries, T. J. 1999. “Towards application of fibre metal laminates in large aircraft”, Aircraft Engineering and Aerospace Technology, vol. 71, no. 6, p. 558-570.
  9. Das, R., Chanda, A., Brechou, J., Banerjee, A. 2016. “Impact behaviour of fibre-metal laminates”, Dynamic Deformation, Damage and Fracture in Composite Materials and Structures, Elsevier Ltd. Schijve, J., Van Lipzig, H.T.M., Van Gestel, G.F.J.A., Hoeymakers, A.H.W. 1979. “Fatigue properties of adhesive-bonded laminated sheet material of aluminum alloys”, Engineering Fracture Mechanics, vol. 12, p. 561-579
  10. Vermeeren, C. A. J. R. 2003. “An historic overview of the development of fibre metal lam