Skip to main content

Eddy current inspection

  • Chapter
Fibre Metal Laminates

Abstract

The eddy current non-destructive inspection technique can be used effectively on fibre metal laminates. It uses the principle of electromagnetic induction, i.e. the interaction between a magnetic field with an electrically conductive object. With this method, the different Fibre Metal Laminate types can be easily discriminated and fatigue cracks in the metal layers of the laminate can reliably be detected in, e.g. plain material, lap joints and spliced laminates.

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. C. Borsboom, Eddy Current Testing of Fiber-Metal Laminates, Structural Laminates Company, Technical Report TD-R-93008, Delft, The Netherlands, June 1993.

    Google Scholar 

  2. V.S. Cecco, et al, Eddy Current Testing, Volume 1, Atomic Energy of Canada Limited, 1987, originally published under the title ‘Eddy Current Manual’, 1983, chapters 1 — 6, p. 164.

    Google Scholar 

  3. H.L. Libby, Introduction To Electromagnetic Nondestructive Test Methods, Wiley-Interscience, 1971, Chapters 1 and 2.

    Google Scholar 

  4. J. Blitz, Electromagnetic And Magnetic Methods Of NDT, Brunei University, Uxbridge, England, 1991, p. 13–15, 89–91, 116–125, 137–139, 141–147, 150–152.

    Google Scholar 

  5. C. Borsboom, Damage Tolerance of Glare Lap Joints in Pressurized Fuselage Structures, Master’s Thesis, Delft University of Technology, Faculty of Aerospace Engineering, Structure and Materials Laboratory, Delft, August 1994.

    Google Scholar 

  6. R.G.P Müller, An Experimental and Analytical Investigation on the Fatigue Behaviour of Fuselage Riveted Lap Joints, PhD Thesis, Delft University of Technology, Delft, 1995.

    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

Borsboom, C. (2001). Eddy current inspection. In: Vlot, A., Gunnink, J.W. (eds) Fibre Metal Laminates. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-0995-9_32

Download citation

  • DOI: https://doi.org/10.1007/978-94-010-0995-9_32

  • 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