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Advances in the Bonded Composite Repair of Metallic Aircraft Structure, 2 Volume Set [Hardcover]

A.A. Baker (Author), L.R.F. Rose (Author), R. Jones (Author)


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Book Description

February 6, 2003 0080426999 978-0080426990 1st
The availability of efficient and cost-effective technologies to repair or extend the life of aging military airframes is becoming a critical requirement in most countries around the world, as new aircraft becoming prohibitively expensive and defence budgets shrink. To a lesser extent a similar situation is arising with civil aircraft, with falling revenues and the high cost of replacement aircraft.



This book looks at repair/reinforcement technology, which is based on the use of adhesively bonded fibre composite patches or doublers and can provide cost-effective life extension in many situations. From the scientific and engineering viewpoint, whilst simple in concept, this technology can be quite challenging particularly when used to repair primary structure. This is due to it being based on interrelated inputs from the fields of aircraft design, solid mechanics, fibre composites, structural adhesive bonding, fracture mechanics and metal fatigue. The technologies of non-destructive inspection (NDI) and, more recently smart materials, are also included. Operational issues are equally critical, including airworthiness certification, application technology (including health and safety issues), and training.



Including contributions from leading experts in Canada, UK, USA and Australia, this book discusses most of these issues and the latest developments. Most importantly, it contains real histories of application of this technology to both military and civil aircraft.


Product Details

  • Hardcover: 1122 pages
  • Publisher: Elsevier Science; 1st edition (February 6, 2003)
  • Language: English
  • ISBN-10: 0080426999
  • ISBN-13: 978-0080426990
  • Product Dimensions: 9.5 x 6.9 x 2.2 inches
  • Shipping Weight: 5.2 pounds
  • Amazon Best Sellers Rank: #3,789,461 in Books (See Top 100 in Books)

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Inside This Book (learn more)
First Sentence:
Acoustic fatigue is due to a very high intensity excitation as a result of pressure waves caused by either engine or aerodynamic effects. Read the first page
Key Phrases - Statistically Improbable Phrases (SIPs): (learn more)
composite doublers, patched specimen, patching efficiency, engineered flaws, unabated crack, orthotropic patch, bonded composite repair technology, bonded composite repairs, cracked plate repaired, load transfer region, maximum peel stress, adhesive shear strain, bondline defects, disbond initiation, edge restraint factor, disbond growth, doubler edge, patched panels, stiffening ratio, waterbreak test, wedge test data, patch efficiency, bonded repair technology, disbond length, disbond size
Key Phrases - Capitalized Phrases (CAPs): (learn more)
Elsevier Science Ltd, New York, Air Vehicles Division, Marcel Dekker, Martinus Nijhoff Publishers, Fishermans Bend, Boeing Paper, Strain Analysis, Adhesive Bonding of Aluminum Alloys, Air Force Contract, Engineered Materials Handbook, Aeronautical Research Laboratory, Aerospace Congress, Engineering Fracture Mechanics, Long Beach, Royal Australian Air Force, Sandia National Laboratories, Australian Department of Defence, Composite Repair of Aircraft Structures, Douglas Aircraft Company, Douglas Paper, Experimental Mechanics, Noyes Publications, Park Ridge, Technical Memorandum
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