Fatigue of Beta Processed and Beta Heat-treated Titanium Alloys (SpringerBriefs in Applied Sciences and Technology) - Softcover

Wanhill, Russell

Softcover

ISBN 10: 940072523X ISBN 13: 9789400725232

Verlag: Springer, 2011

Inhaltsangabe

This publication reviews most of the available literature on the fatigue properties of? annealed Ti-6Al-4V and titanium alloys with similar microstructures. The focus is on? processed and? heat-treated alloys because? annealed Ti-6Al-4V has been selected for highly loaded and fatigue-critical structures, including the main wing-carry-through bulkheads and vertical tail stubs, of advanced high-performance military aircraft. An important aspect of the review is a concise survey of fatigue life assessment methods and the required types of fatigue data. This survey provides the background to recommendations for further research, especially on the fatigue behaviour of? annealed Ti-6Al-4V under realistic fatigue load histories, including the essential topic of short/small fatigue crack growth. Such research is required for independent fatigue life assessments that conform to the aircraft manufacturer's design requirements, and also for life reassessments that most probably will have to be made during the service life of the aircraft.

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This publication reviews most of the available literature on the fatigue properties of annealed Ti-6Al-4V and titanium alloys with similar microstructures. The focus is on processed and heat-treated alloys because annealed Ti-6Al-4V has been selected for highly loaded and fatigue-critical structures, including the main wing-carry-through bulkheads and vertical tail stubs, of advanced high-performance military aircraft.

An important aspect of the review is a concise survey of fatigue life assessment methods and the required types of fatigue data. This survey provides the background to recommendations for further research, especially on the fatigue behaviour of annealed Ti-6Al-4V under realistic fatigue load histories, including the essential topic of short/small fatigue crack growth. Such research is required for independent fatigue life assessments that conform to the aircraft manufacturer 's design requirements, and also for life reassessments that most probably will have" "to be made during the service life of the aircraft.

Details zur Ausgabe

• Verlag: Springer
• Erscheinungsdatum: 2011
• Sprache: Englisch
• ISBN 10: 940072523X
• ISBN 13: 9789400725232
• Einband: Taschenbuch
• Anzahl der Seiten: 64
• Kontakt zum Hersteller: Springer Nature Customer Service Center GmbH; ProductSafety@springernature.com; ; Europaplatz 3; Heidelberg; 69115; Deutschland