Aircraft Fatigue Management

Lieferzeit: Lieferbar innerhalb 14 Tagen

48,14 

SpringerBriefs in Applied Sciences and Technology

ISBN: 9819974674
ISBN 13: 9789819974672
Autor: Molent, Lorrie
Verlag: Springer Verlag GmbH
Umfang: ix, 64 S., 3 s/w Illustr., 17 farbige Illustr., 64 p. 20 illus., 17 illus. in color.
Erscheinungsdatum: 19.12.2023
Auflage: 1/2024
Produktform: Kartoniert
Einband: Kartoniert
Artikelnummer: 748002 Kategorie:

Beschreibung

Fatigue occurs under cyclic loading and can significantly degrade the operational capability and safety of metallic aircraft components and structures. This book provides summaries of some metallic aircraft structural integrity issues, innovative but established examples of maintaining operational capabilityairworthiness, and assessments of safe in-service fatigue lives. These topics are based on a through-life fatigue management philosophy that ensures safe and continued operation, including during life extensions that are almost inevitably required. This philosophy is underpinned by observations of the behaviour of fatigue cracks in actual structures subjected to realistic service loading conditions. The book includes topics like aircraft design requirements, individual aircraft fatigue loads monitoring, airframe fatigue testing, sources of fatigue-nucleating discontinuities, and prediction of fatigue crack growth from these discontinuities. All these aspects contribute to discussing methods of assuring the structural integrity and operational capability of realistically cracked structures. The book also discusses the exponential behaviour of lead or dominant cracksthose leading to first failureand the practical significance of differences between fatigue fracture topographies produced under constant amplitude and variable amplitude loading. The book can be a valuable reference for researchers and professionals interested in aircraft fatigue management and allied fields.

Autorenporträt

Mr. Lorrie Molent is an acknowledged authority in the elds of aircraft structural integrity, structural mechanics, structural and fatigue testing, advanced composite bonded repair, aircraft vulnerability, and aircraft accident investigation. He has more than 280 publications in these technical areas. Mr. Molent is a qualied aircraft accident investigator. He has been attached to both the then Australian Civil Aviation Department and the US Navy NAVAIR Structures in Washington D.C. as an airworthiness engineer and has a broad network of collaborators nationally and internationally. Until October 2020, Mr. Molent was the Australias Defence Science and Technology Groups Head of Emerging Aircraft Structural Integrity. In 2010, he was presented with the Ministers Award for Achievements in Defence Science, and he was awarded with a member of the Order of Australia (AM) in 2016. He also has numerous other team achievement awards. Currently, he works as a consultant and trainer in aircraft structural integrity, air accident investigation, and novel fatigue analyses methods.

Herstellerkennzeichnung:


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69121 Heidelberg
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E-Mail: juergen.hartmann@springer.com

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