DocumentCode :
1471901
Title :
Solenoid-operated hydraulic valves for aircraft applications
Author :
Goepfrich, George A.
Author_Institution :
Bendix Aviation Corporation, South Bend, Ind.
Volume :
63
Issue :
11
fYear :
1944
Firstpage :
866
Lastpage :
868
Abstract :
DURING the past several years there has been a definite trend by some aircraft manufacturers to eliminate hydraulic controls from combat airplanes. The vulnerability of hydraulic systems used on airplanes manufactured during this period and to a certain extent today are big factors in promoting this trend. Space requirements in the cockpit of an airplane to mount control valves and accommodate necessary piping to these valves, difficulty with packings at extremely cold temperatures, and the lack of flexibility of the control system are other factors that contributed to the aforementioned trend.
Keywords :
Airplanes; Coils; Fluids; Relays; Springs; Switches; Valves;
fLanguage :
English
Journal_Title :
Electrical Engineering
Publisher :
ieee
ISSN :
0095-9197
Type :
jour
DOI :
10.1109/EE.1944.6440580
Filename :
6440580
Link To Document :
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