Cantitate/Preț
Produs

Fibre Metal Laminates: An Introduction

Editat de Ad Vlot, Jan Willem Gunnink
en Limba Engleză Hardback – 30 sep 2001
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.
Citește tot Restrânge

Toate formatele și edițiile

Toate formatele și edițiile Preț Express
Paperback (1) 163047 lei  43-57 zile
  SPRINGER NETHERLANDS – 30 noi 2001 163047 lei  43-57 zile
Hardback (1) 163619 lei  43-57 zile
  SPRINGER NETHERLANDS – 30 sep 2001 163619 lei  43-57 zile

Preț: 163619 lei

Preț vechi: 199536 lei
-18% Nou

Puncte Express: 2454

Preț estimativ în valută:
31313 32526$ 26010£

Carte tipărită la comandă

Livrare economică 03-17 februarie 25

Preluare comenzi: 021 569.72.76

Specificații

ISBN-13: 9781402000386
ISBN-10: 1402000383
Pagini: 532
Ilustrații: VIII, 532 p.
Dimensiuni: 155 x 235 x 36 mm
Greutate: 0.93 kg
Ediția:2001
Editura: SPRINGER NETHERLANDS
Colecția Springer
Locul publicării:Dordrecht, Netherlands

Public țintă

Research

Cuprins

A Material Properties.- 1 Historical overview.- 2 Glare features.- 3 Next Generation Fibre Metal Laminates.- 4 Long-term behaviour.- 5 Material design allowables and qualification.- 6 New aluminium alloys for Glare.- B Methods.- 7 Stress-strain curve.- 8 Shear yield strength.- 9 Blunt notch strength.- 10 Stability.- 11 Fatigue.- 12 Fatigue of riveted joints.- 13 Residual strength.- 14 Damage tolerance aspects.- C Design Aspects.- 15 Fuselage barrel design and design for manufacturing.- 16 Cut-outs; door surrounding.- 17 Detailed design concepts.- 18 Numerical modelling: delamination buckling.- 19 Glare — from invention to innovation.- 20 Secondary applications.- D Production.- 21 Machineability.- 22 Formability.- 23 Curved panels.- 24 Quality control.- E Safety, Maintenance and Inspection.- 25 Inspection and maintenance.- 26 Burn-through and lightning strike.- 27 Impact properties.- 28 Corrosion.- 29 Riveted repairs.- 30 Bonded repair patches.- 31 Bonded repairs for C-5A fuselage crown cracking.- 32 Eddy current inspection.- 33 Glare as part of Sustainable and Environmentally Sound Engineering.- Authors and Affiliations.- Sponsors.

Recenzii

`Engineers wanting to learn about this material, whether from a design/analysis or manufacturing viewpoint, won't find a better reference than Fibre Metal Laminates: An Introduction.'