Skip to main content

Glare — from invention to innovation

  • Chapter
Fibre Metal Laminates
  • 607 Accesses

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.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 229.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 299.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 299.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. B. van Wimersma, A3XX status reporting on in-service experience and full-scale testing of Glare, AI/LE-T-presentation, 1998.

    Google Scholar 

  2. T. de Vries, Blunt and sharp notch behaviour of Glare laminates, Dissertation, Delft University of Technology, 2001

    Google Scholar 

  3. R.P.T. Müller, An experimental and analytical investigation on the fatigue behaviour of fuselage riveted lap joints, Dissertation, Delft University of Technology, 1995.

    Google Scholar 

  4. R.A.M. Coenen, Design of a quality assurance system for structural laminates, Dissertation, Delft University of Technology, 1998.

    Google Scholar 

  5. O.J. Bosker, Tsai-Hill criterion to predict the bi-axial blunt notch strength of Glare, Report: TD-R-0001A, Structural Laminates Industries, 2001

    Google Scholar 

  6. T. Beumler, Glare durability program, summary of the results, Minutes of meeting EMF-932/99, 1999.

    Google Scholar 

  7. F. Hashagen, Numerical analysis of failure mechanisms in fibre metal laminates, Dissertation, Delft University of Technology, 1998.

    Google Scholar 

  8. G. Roebroeks, The metal volume fraction approach, TD-R-003-06, SLI report, Structural Laminates Company, 2000.

    Google Scholar 

  9. R.M. Jones, Mechanics of composite materials, Mc-Graw-Hill Book Company, New York, 1980.

    Google Scholar 

  10. M.C.Y. Niu, Airframe structural design, Hong Kong Conmilit Press Ltd, Hong Kong, 1988

    Google Scholar 

  11. E.F. Bruhn, Analysis and design of flight vehicle structures, Jacobs Publishing, Inc, Indianapolis, 1973.

    Google Scholar 

  12. K. Verolme, The development of a design tool for fiber metal laminate compression panels, Dissertation, Delft University of Technology, 1995.

    Google Scholar 

  13. O. Erdmann, et al., SCHADI Theory Manual, EADS-Germany, 2000.

    Google Scholar 

  14. O. Erdmann, Letter from Mr Erdmann (EADS-Germany) to Mr Van Hengel (Structural Laminates Industries), EADS-Germany, 2000.

    Google Scholar 

Download references

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2001 Springer Science+Business Media Dordrecht

About this chapter

Cite this chapter

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

Download citation

  • 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

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics