nach oben

Erschienen in:

2017 | OriginalPaper | Buchkapitel

2. Laminate Concepts & Mechanical Properties

verfasst von : René Alderliesten

Erschienen in: Fatigue and Fracture of Fibre Metal Laminates

Verlag: Springer International Publishing

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config

KI-gestützte Suche

Aus

Abstract

Inspired by the successful application of ARALL and GLARE on aeronautical structures, many researchers and scientists have pursued the development of FML concepts. The fact that the majority of these studies never reached maturity on structural applications may be explained by the observation that FML was mostly treated as a material concept. As a result, not enough consideration was given to the final structural applications. Nonetheless, many FML variants with their properties presented in the literature constitute valuable information for future developments. Therefore, an overview of all the FMLs and the most characteristic properties are given in this chapter.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

über 102.000 Bücher
über 537 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Finance + Banking
Management + Führung
Marketing + Vertrieb
Maschinenbau + Werkstoffe
Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

über 67.000 Bücher
über 390 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Maschinenbau + Werkstoffe

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Vorheriges Kapitel Introduction

Nächstes Kapitel Patents and Intellectual Property

Vlot A (2001) GLARE—history of the development of a new aircraft material. Kluwer Academic Publishers, Dordrecht, The Netherlands

Vogelesang LB (2003) Fibre metal laminates—the development f a new family of hybrid materials. In: Editor, G, (ed) Proceedings of the 22rd fatigue of aeronautical structures as an engineering challenge, ICAF symposium, vol I, EMAS publishing, UK, p 1–41

De Boer T (2001) Next generation fibre metal laminates. In: Vlot A, Gunnink JW (eds) Fibre Metal Laminates—an introduction. Kluwer Academic Publishers, Dordrecht, The Netherlands

DIALFAST Development of innovative and advanced laminates for future aircraft structure. Project funded by the European Commission within the 6th framework programme, 2004–2007

Department of Defence (2005) Technology readiness assessment (TRA). Deskbook, USA

Marissen R (1988) Fatigue Crack Growth in ARALL, a hybrid Aluminium-Aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate. PhD Dissertation, Delft University of Technology

Roebroeks GHJJ (1991) Towards GLARE—The Development of a fatigue insensitive and damage tolerant aircraft material. PhD Thesis, Delft University of Technology, Delft

Vlot A, Gunnink JW (eds) (2001) Fibre Metal Laminates—an introduction. Kluwer Academic Publishers, Dordrecht, The Netherlands

Bucci RJ, Mueller LN, Vogelesang LB, Gunnink, JW (1988) Proceedings of the 33rd international sampe symposium. pp 1237–1248

10.

Van Hengel C, Kortbeek P (2009) ARALL and GLARE FML’s: three decades of bridging the gap between theory and operational practice. In: M. Bos (ed) ICAF 2009, bridging the gap between theory and operational practice, pp 601–615

11.

Da Silva DA, Botelho EC, Rezende MC (2008) Hygrothermal aging effect on fatigue behavior of GLARE. J. Reinf. Plast. & Comp 28(20):2487–2499CrossRef

12.

Khan SU, Alderliesten RC, Benedictus R (2009) Delamination in Fibre Metal Laminates under variable amplitude loading. Composites Science and Technology 69(15–16):2604–2615CrossRef

13.

Mangkoesoebroto RH (1987) The Effect of fibre volume fraction on the mechanical properties and the fatigue behaviour of ARALL laminates. Masters Thesis, Delft University of Technology

14.

Structural Laminates Company (1994) QA Reports B0319B-2, B1008B-1, B0904A-3, 510 Constitution Blvd., New Kensington, PA 15064

15.

Vermeeren CAJR (1990) The blunt notch behaviour of metal laminates: ARALL and GLARE. Report LR-617, Delft University of Technology

16.

Wiltink FJ, Bodegom VJW van (1994) Flight-simulation fatigue tests on notched specimens of Fiber-metal laminates. Test results used in LRV-10, Report LRV-11, Delft University of Technology

17.

Alderliesten RC (2009) On the development of hybrid material concepts for aircraft structures. Recent Patents on Engineering 3(1):25–38CrossRef

18.

Boertien MFHC (1992) Evaluation of solid S2 and R glass fibers versus hollow S2 glass fibers for Fibre Metal Laminates. Preliminary thesis, Delft University of Technology

19.

Roebroeks G (2000) The metal volume fraction approach. Report TD-R-00-003, Structural Laminates Industries

20.

Pellenkoft FJ (2000) Initial sizing study of GLARE-based alternative floor panel concepts for the containerised cargo compartment of the A3XX. Report B2 V-00-44, Delft University of Technology

21.

Mattousch AC (1991) Bearing strength tests on GLARE sheets for the application in lugs. Preliminary thesis, Delft University of Technology

22.

Roebroeks GHJJ (2007) The development of Central. DTAS 2007

23.

Vermeeren CAJR (1990) Ultra high modulus carbon fibres in ARALL Laminates. Memorandum M-641, Delft University of Technology

24.

Vermeeren CAJR (1991) The application of carbon fibres in ARALL laminates. Report L-658, Delft University of Technology

25.

Koos MG de (1990) PEEK carbon fibre reinforced titanium laminates. Master Thesis, Delft University of Technology

26.

Kleinendorst RGJ (1990) Corrosion properties of carbon ARALL. Master Thesis, Delft University of Technology

27.

Medenblik EW (1994) Titanium fibre-metal laminates. Master Thesis, Delft University of Technology

28.

Lin CT, Kao PW, Yang FS (1991) Fatigue behaviour of carbon fibre reinforced aluminium laminates. Composites 22(2):135–141CrossRef

29.

Lin CT, Kao PW, Jen M-HR (1994) Thermal residual strains in carbon–fibre aluminium laminates. Composites 25(4):303–307CrossRef

30.

Lin CT, Kao PW (1995) Effect of fiber bridging on the fatigue crack propagation in carbon fiber-reinforced aluminium laminates. Mater Sci Eng A 190:65–73CrossRef

31.

Lin CT, Kao PW (1996) Fatigue delamination growth in carbon fibre reinforced aluminium laminates. Compos Part A 27A:9–15CrossRef

32.

Silva JMA, Ferreira JAM, Devezas TC (2003) Fatigue damage of carbon–epoxy laminates with embedded optical fibres. Mater Sci Technol 19:809–814CrossRef

33.

Bradshaw RD, Gutierrez SE (2007) Characterization of fatigue crack initiation and growth in hybrid aluminium–graphite fibre composite laminates using image analysis. Fatigue Fract Eng Mater Struct 30:766–781CrossRef

34.

Meyers LG, Roebroeks GHJJ (1986) De HP-PE vezel, enkele experimenten. Technische Hogeschool Delft, Luchtvaart en Ruimtevaarttechniek

35.

TOYOBO Co. Ltd (2001) PBO Fiber Zylon®, technical information. (revised 2001.9)

36.

Huang YK, Frings PH, Hennes E (2002) Mechanical properties of Zylon/epoxy composite. Compos B Eng 33(2):109–115CrossRef

37.

Jagt OC van der (1998) Mechanical behaviour of a new polymer fibre (‘M5’) in advanced composite structures. In M.A. Erath (ed) Proceedings of the 19th international conference on SAMPE Europe progress through innovation and cost effectiveness, Paris, April 22–24, 1998. ISBN 3-9520477-5-9 pp 227–239

38.

Jagt OC van der, Beukers A (1999) The potential of a new rigid-rod polymer fibre (‘M5’) in advanced composite structures. Polymer 40:1035–1044CrossRef

39.

Sihombing KM (1999) The application of M5-fibre in fibre-metal laminates. Delft University of Technology, Netherlands

40.

Asporo YAR (1999) Towards M5 FML, a preliminary research on the new Fiber Metal Laminate with M5 Fiber. MSc thesis, Delft University of Technology

41.

Burianek DA (2001) Mechanics of fatigue damage in Titanium-Graphite hybrid Laminates. PhD dissertation, Massachusetts Institute of Technology

42.

Burianek DA, Spearing SM (2002) Fatigue damage in titanium-graphite hybrid laminates. Compos Sci Technol 62:607–617CrossRef

43.

Rans CD (2008) Evaluation of the fatigue crack propagation and delamination growth behaviour of Titanium-Carbon laminates. Report B2 V-08-06, Delft University of Technology

44.

Rans CD, Alderliesten RC, Benedictus R (2011) Predicting the influence of temperature on fatigue crack propagation inn Fibre Metal Laminates. Eng Fract Mech 78:2193–2201CrossRef

45.

Rensma E (2007) Investigation of innovative concepts for hybrid structures. MSc thesis, Delft University of Technology

46.

Shahinian R (2006) The next generation of fibre metal laminates. A preliminary study of the material properties of carbon fibre-reinforced stainless steel laminates. Internship report, Hogeschool van Amsterdam

47.

Rooijen RGJ (2006) Bearing strength characteristics of standard and steel reinforced GLARE. PhD dissertation, Delft University of Technology, Delft

48.

Pärnänen T, Kanerva M, Sarlin E, Saarela O (2015) Debonding and impact damage in stainless steel fibre metal laminates prior to metal fracture. Compos Struct 119:777–786CrossRef

49.

Cortes P, Cantwell WJ (2006) The fracture properties of a fibre–metal laminate based on magnesium alloy. Compos B 37:163–170CrossRef

50.

Alderliesten R, Rans C, Benedictus R (2008) The applicability of magnesium based Fibre Metal Laminates in aerospace structures. Compos Sci Technol 68(14):2983–2993CrossRef

51.

Coonen M (2010) Applicability of MgAl‐FML’s in aerospace. MSc thesis, Delft University of Technology

52.

Van Velze TM (1988) Thermoplastics in ARALL laminates—Development, production and testing of ARALL laminates with a thermoplastic matrix. MSc thesis, Delft University of Technology

53.

van der Hoeven W (2007) Preliminary evaluation of a high temperature Fibre Metal Laminate, Report NLR-CR-2007-596. National Aerospace Laboratory, The Netherlands

54.

Langdon GS, Cantwell WJ, Nurick GN (2005) The blast response of novel thermoplastic-based fibre-metal laminates—some preliminary results and observations. Compos Sci Technol 65:861–872CrossRef

55.

Langdon GS, Cantwell WJ, Nurick GN (2007) Localised blast loading of fibre–metal laminates with a polyamide matrix. Compos B 38:902–913CrossRef

Titel: Laminate Concepts & Mechanical Properties
verfasst von: René Alderliesten
Verlag: Springer International Publishing
Buch: Fatigue and Fracture of Fibre Metal Laminates
Print ISBN: 978-3-319-56226-1

Electronic ISBN: 978-3-319-56227-8

Copyright-Jahr: 2017
DOI: https://doi.org/10.1007/978-3-319-56227-8_2

Premium Partner

Marktübersichten

Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.

Zur Marktübersicht