Fatigue in aerostructures—where structural health monitoring can contribute to a complex subject-Reference-Cited by-同舟云学术

Fatigue in aerostructures—where structural health monitoring can contribute to a complex subject

Published:2006-12-13 Issue:1851 Volume:365 Page:561-587
ISSN:1364-503X
Container-title:Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences
language:en
Short-container-title:Phil. Trans. R. Soc. A.

Author:

Boller Christian¹,Buderath Matthias²

Affiliation:

1. Department of Mechanical Engineering, University of SheffieldMappin Street, Sheffield S1 3JD, UK

2. EADS Military Air Systems81663 München, Germany

Abstract

An overview of the aircraft design and maintenance process is given with specific emphasis on the fatigue design as well as the phenomenon of the ageing aircraft observed over the life cycle. The different measures taken to guarantee structural integrity along the maintenance process are addressed. The impact of structural health monitoring as a means of possibly revolutionizing the current aircraft structural monitoring and design process is emphasized and comparison is made to jet engines and helicopters, where health monitoring has already found the respective breakthrough.

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Link

https://royalsocietypublishing.org/doi/pdf/10.1098/rsta.2006.1924

Reference31 articles.

1. Anon. 1995 HSB Handbuch Struktur Berechnung ; Document 12571-01 DASA-Airbus Germany.

2. Anon. 2005 Air Transport Association (ATA) Specifications Revision 2005 . Washington DC: ATA.

3. Balageas D. (ed.) 2002 Proc. of the First European Workshop on Structural Health Monitoring Cachan France . DEStech Publ. Inc.

4. Betz D. Trutzel M. N. Staudigel L. Schmuecker M. Huelsmann E. Czernay U. Muehlmann H.-C. & Muellert T. 2001 Fiber-optic smart sensing of aviation structures. In Proc. of 3rd Internat. Workshop on Struct. Health Monitoring pp. 306–315. Boca Raton FL: CRC Press.

5. Betz D. Thursby G. Culshaw B. & Staszewski W. J. 2004 Damage identification using Lamb waves and fibre Bragg grating sensors. In Proc. of 2nd Europ. Workshop on Structural Health Monitoring pp. 1151–1158. DEStech Publ.

Cited by 54 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Strategies towards a more sustainable aviation: A systematic review;Progress in Aerospace Sciences;2023-02

2. Improved Modeling of Maintenance for Future Vertical Lift;Industrial and Systems Engineering Review;2022-12-25

3. Mechanism for superior fatigue performance of warm laser shock peened IN718 superalloy after high-temperature ageing;Journal of Alloys and Compounds;2022-11

4. Dynamics analysis and structural synthesis of wind energy production device with closed loop conveyor;Vibroengineering PROCEDIA;2022-08-25

5. Multi-level damage diagnosis on stiffened composite panels based on a damage-uninformative digital twin;Structural Health Monitoring;2022-07-01