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Electromagnetic Dent Removal for Aircraft Repair
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English
Abstract
The electromagnetic dent removal process removes dents from many aluminum structures where access is either limited to one surface (e.g., bonded aluminum honeycomb parts) or where access to the rear surface is restricted by equipment or other structures.
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Authors
Citation
Roseberry, T., "Electromagnetic Dent Removal for Aircraft Repair," SAE Technical Paper 890923, 1989, https://doi.org/10.4271/890923.Also In
References
- Hendrickson, I. G. Hansen, K. A. Electromagnetic Force (EMF) Machine Tension Proofloading and Dent Pulling of Aerospace Structures Eleventh Symposium on Nondestructive Evaluation San Antonio, Texas April 20-22 1977
- Wilson, M. H. Srivastavsa, V. D. Design of Efficient Flux Concentrators for Pulsed High Magnetic Fields The Review of Scientific Instruments 36 8 1 August 1965
- Zittel, G Magneform - An Accepted Production Tool Fifth International Conference on High-Energy Rate Fabrication Denver, Colorado June 24-26 1975
- Hansen, K. A. Hendrickson, I. G. Development of Single-Turn Flux Concentrator for the Electromagnetic Force (EMF) Machine Boeing report B-8180-10-188 December 22 1976