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Modeling and strain gauging of eddy current repulsion deicing systemsWork described in this paper confirms and extends work done by Zumwalt, et al., on a variety of in-flight deicing systems that use eddy current repulsion for repelling ice. Two such systems are known as electro-impulse deicing (EIDI) and the eddy current repulsion deicing strip (EDS). Mathematical models for these systems are discussed for their capabilities and limitations. The author duplicates a particular model of the EDS. Theoretical voltage, current, and force results are compared directly to experimental results. Dynamic strain measurements results are presented for the EDS system. Dynamic strain measurements near EDS or EIDI coils are complicated by the high magnetic fields in the vicinity of the coils. High magnetic fields induce false voltage signals out of the gages.
Document ID
19930038699
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, Samuel O.
(Electroimpact, Inc. Seattle, WA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 93-0296
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A22696
Funding Number(s)
CONTRACT_GRANT: NAS3-26252
Distribution Limits
Public
Copyright
Other

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