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Autonomous Deicing System For Airplane WingPrototype autonomous deicing system for airplane includes network of electronic and electromechanical modules at various locations in wings and connected to central data-processing unit. Small, integrated solid-state device, using long coils installed under leading edge, exciting small vibrations to detect ice and larger vibrations to knock ice off. In extension of concept, outputs of vibration sensors and other sensors used to detect rivet-line fractures, fatigue cracks, and other potentially dangerous defects.
Document ID
19930000623
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Hickman, G. A.
(Innovative Dynamics)
Gerardi, J. J.
(Innovative Dynamics)
Date Acquired
August 16, 2013
Publication Date
October 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 10
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
LEW-15376
Accession Number
93B10623
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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