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Reference > Aviation > General
Technology > Material Science

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Fibre Metal Laminates: An Introduction

Author(s): Vlot, Ad; Gunnink, Jan Willem; Vlot, Ad
ISBN10: 1402000383
ISBN13: 9781402000386
Cover: Hardcover
 
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List Price $239.00 
Our Price $228.36
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SummaryTable of Contents
Fibre metal laminates were developed at Delft University of Technology in The Netherlands, from the beginning of the 1980s. This is a new family of hybrid materials consisting of thin metal layers bonded together by fibres embedded in an adhesive. As a result of this build-up, fibre metal laminates possess a mixture of the characteristics of both metals and composite materials. Initial development led to the `Arall' variant using aramid fibres, which was first applied on the C-17 military transport aircraft around 1990. Large-scale application became possible with a variant using glass fibres, dubbed `Glare', which was selected for the Airbus A380 super jumbo in 2001. This is the first book to discuss these new materials and it deals mostly with Glare. It covers most of the relevant aspects of the materials, from static mechanical properties, fatigue and impact to design, production and maintenance of aircraft structures. This book contains the basic information on these new materials necessary for engineers and aircraft operators alike.

This is the first book to discuss these new materials, and deals mostly with Glare. It covers most of the relevant aspects of the materials, from static mechanical properties, fatigue, and impact to design, production, and maintenance of aircraft structures.
Preface vii
A Material Properties 1(98)
Historical overview
3(20)
Glare features
23(16)
Next Generation Fibre Metal Laminates
39(14)
Long-term behaviour
53(16)
Material design allowables and qualification
69(10)
New aluminium alloys for Glare
79(20)
B Methods 99(136)
Stress-strin curve
101(10)
Shear yield strength
111(6)
Blunt notch strength
117(16)
Stability
133(22)
Fatigue
155(18)
Fatigue of riveted joints
173(24)
Residual strength
197(22)
Damage tolerance aspects
219(16)
C Design Aspects 235(90)
Fuselage barrel design and design for manufacturing
237(18)
Cut-outs; door surronding
255(12)
Detailed design concepts
267(14)
Numerical modelling: delamination buckling
281(18)
Glare - from invention to innovation
299(10)
Secondary applications
309(16)
D Production 325(56)
Machineability
327(10)
Formability
337(18)
Curved panels
355(14)
Quality control
369(12)
E Safety, Maintenance and Inspection 381(144)
Inspection and maintenance
383(16)
Burn-through and lighting strike
399(10)
Impact properties
409(18)
Corrosion
427(14)
Riveted repairs
441(10)
Bonded repair patches
451(26)
Bonded repairs for C-5A fuselage crown cracking
477(22)
Eddy current inspection
499(14)
Glare as part of Sustainable and Environmentally Sound Engineering
513(12)
Authors and Affiliations 525(2)
Sponsors 527

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