Abstract
In recent years, significant progress has been made in understanding the behaviour of Fibre Metal Laminates, especially Glare. Now, this material has been chosen to serve as skin material in fuselage sections of the Airbus A380. However, a very challenging task must still be solved. All the available knowledge and research results must be transferred into quality standards and procedures, design and sizing methods in order to meet the stringent requirements set up by clients, airworthiness authorities and Airbus quality standards. Therefore, the following paper describes major activities that are carried out to transfer Glare from an invention into a real innovation in the aerospace industry.
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References
B. van Wimersma, A3XX status reporting on in-service experience and full-scale testing of Glare, AI/LE-T-presentation, 1998.
T. de Vries, Blunt and sharp notch behaviour of Glare laminates, Dissertation, Delft University of Technology, 2001
R.P.T. Müller, An experimental and analytical investigation on the fatigue behaviour of fuselage riveted lap joints, Dissertation, Delft University of Technology, 1995.
R.A.M. Coenen, Design of a quality assurance system for structural laminates, Dissertation, Delft University of Technology, 1998.
O.J. Bosker, Tsai-Hill criterion to predict the bi-axial blunt notch strength of Glare, Report: TD-R-0001A, Structural Laminates Industries, 2001
T. Beumler, Glare durability program, summary of the results, Minutes of meeting EMF-932/99, 1999.
F. Hashagen, Numerical analysis of failure mechanisms in fibre metal laminates, Dissertation, Delft University of Technology, 1998.
G. Roebroeks, The metal volume fraction approach, TD-R-003-06, SLI report, Structural Laminates Company, 2000.
R.M. Jones, Mechanics of composite materials, Mc-Graw-Hill Book Company, New York, 1980.
M.C.Y. Niu, Airframe structural design, Hong Kong Conmilit Press Ltd, Hong Kong, 1988
E.F. Bruhn, Analysis and design of flight vehicle structures, Jacobs Publishing, Inc, Indianapolis, 1973.
K. Verolme, The development of a design tool for fiber metal laminate compression panels, Dissertation, Delft University of Technology, 1995.
O. Erdmann, et al., SCHADI Theory Manual, EADS-Germany, 2000.
O. Erdmann, Letter from Mr Erdmann (EADS-Germany) to Mr Van Hengel (Structural Laminates Industries), EADS-Germany, 2000.
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© 2001 Springer Science+Business Media Dordrecht
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Hashagen, F., Haack, C., Wiedemann, M. (2001). Glare — from invention to innovation. In: Vlot, A., Gunnink, J.W. (eds) Fibre Metal Laminates. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-0995-9_19
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DOI: https://doi.org/10.1007/978-94-010-0995-9_19
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-4020-0391-2
Online ISBN: 978-94-010-0995-9
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