DocumentCode :
1035357
Title :
An Electric Deicing System for Aircraft
Author :
Giloy, E.W.
Author_Institution :
Electrical Design Engineering Section, The Glenn L. Martin Company, Baltimore, Md.
Volume :
68
Issue :
2
fYear :
1949
fDate :
7/1/1949 12:00:00 AM
Firstpage :
1051
Lastpage :
1057
Abstract :
This paper covers an electric ice removal system as applied to a recent experimental airplane. The system is described in detail from the power generators to the ice removal blankets and includes such items as extent of ice protection coverage, construction and installation of ice removal blankets, system electric power requirements, and system control. The paper does not treat the subject of ice protection in any of its theoretical aspects. The complete ice protection system installation is believed to be the first of its kind in this country.
Keywords :
Aircraft; Airplanes; Electric resistance; Engines; Ice surface; Power generation; Power system protection; Resistance heating; Rubber; Skin;
fLanguage :
English
Journal_Title :
American Institute of Electrical Engineers, Transactions of the
Publisher :
ieee
ISSN :
0096-3860
Type :
jour
DOI :
10.1109/T-AIEE.1949.5060049
Filename :
5060049
Link To Document :
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