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Ice Detector and Deicing Fluid Effectiveness Monitoring SystemAn ice detector and deicing fluid effectiveness monitoring system for an aircraft is disclosed. The ice detection portion is particularly suited for use in flight to notify the flight crew of an accumulation of ice on an aircraft lifting and control surfaces, or helicopter rotors, whereas the deicing fluid effectiveness monitoring portion is particularly suited for use on the ground to notify the flight crew of the possible loss of the effectiveness of the deicing fluid. The ice detection portion comprises a temperature sensor and a parallel arrangement of electrodes whose coefficient of coupling is indicative of the formation of the ice, as well as the thickness of the formed ice. The fluid effectiveness monitoring portion comprises a temperature sensor and an ionic-conduction cell array that measures the conductivity of the deicing fluid which is indicative of its concentration and, thus, its freezing point. By measuring the temperature and having knowledge of the freezing point of the deicing fluid, the fluid effectiveness monitoring portion predicts when the deicing fluid may lose its effectiveness because its freezing point may correspond to the temperature of the ambient.
Document ID
19960035821
Acquisition Source
Ames Research Center
Document Type
Other - Patent
Authors
Seegmiller, H. Lee B.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 17, 2013
Publication Date
June 4, 1996
Subject Category
Air Transportation And Safety
Report/Patent Number
Patent Number: US-Patent-5,523,959
Patent Application Number: US-Patent-Appl-SN-233676
Patent Number: NASA-Case-ARC-12045-1-GE
Accession Number
96N30526
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-5,523,959|NASA-Case-ARC-12045-1-GE
Patent Application
US-Patent-Appl-SN-233676
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