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  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 |
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vii | |
| A Material Properties |
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1 | (98) |
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3 | (20) |
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23 | (16) |
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Next Generation Fibre Metal Laminates |
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39 | (14) |
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53 | (16) |
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Material design allowables and qualification |
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69 | (10) |
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New aluminium alloys for Glare |
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79 | (20) |
| B Methods |
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99 | (136) |
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101 | (10) |
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111 | (6) |
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117 | (16) |
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133 | (22) |
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155 | (18) |
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Fatigue of riveted joints |
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173 | (24) |
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197 | (22) |
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219 | (16) |
| C Design Aspects |
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235 | (90) |
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Fuselage barrel design and design for manufacturing |
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237 | (18) |
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Cut-outs; door surronding |
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255 | (12) |
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267 | (14) |
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Numerical modelling: delamination buckling |
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281 | (18) |
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Glare - from invention to innovation |
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299 | (10) |
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309 | (16) |
| D Production |
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325 | (56) |
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327 | (10) |
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337 | (18) |
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355 | (14) |
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369 | (12) |
| E Safety, Maintenance and Inspection |
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381 | (144) |
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Inspection and maintenance |
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383 | (16) |
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Burn-through and lighting strike |
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399 | (10) |
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409 | (18) |
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427 | (14) |
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441 | (10) |
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451 | (26) |
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Bonded repairs for C-5A fuselage crown cracking |
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477 | (22) |
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499 | (14) |
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Glare as part of Sustainable and Environmentally Sound Engineering |
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513 | (12) |
| Authors and Affiliations |
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525 | (2) |
| Sponsors |
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527 | |
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