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Electromagnetic Dent Removal for Aircraft Repair
ISSN: 0148-7191, e-ISSN: 2688-3627
Published April 01, 1989 by SAE International in United States
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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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CitationRoseberry, T., "Electromagnetic Dent Removal for Aircraft Repair," SAE Technical Paper 890923, 1989, https://doi.org/10.4271/890923.
- 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
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- 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