DocumentCode
1476745
Title
Automatic temperature control for aircraft
Author
Gund, R. A.
Author_Institution
General Electric Company, Schenectady, N. Y.
Volume
64
Issue
10
fYear
1945
Firstpage
730
Lastpage
734
Abstract
AUTOMATIC temperature control for aircraft long has been neglected, and it is only during the war that adequate attention has been given to this important subject. The increased duties imposed upon flight personnel by the requirements of modern military aircraft, together with the necessity for reducing air drag to the minimum consistent with required cooling, have prompted aircraft designers to give consideration to automatic operation of cowl flaps, oil and coolant flaps, and intercooler doors. Automatic flap operation can be appreciated fully when it is considered that engine cowl flaps fully opened might represent an air drag as high as 40 miles per hour on a 400-mile-per-hour airplane.
Keywords
Coils; Cooling; Heating; Relays; Temperature sensors; Thermostats;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1945.6441307
Filename
6441307
Link To Document