DocumentCode :
1370251
Title :
Weight analysis of aircraft actuators
Author :
Geyer, M. Howard ; Treseder, R. C.
Author_Institution :
General Motors Corporation, Dayton, Ohio
Volume :
71
Issue :
2
fYear :
1952
fDate :
4/1/1952 12:00:00 AM
Firstpage :
118
Lastpage :
126
Abstract :
THE work that must be expended to actuate adjustable flight surfaces and to operate the landing gear, bomb doors, and other movable structures on aircraft often exceeds pilot capabilities. At the same time, the increase in physical size of aircraft in recent years has all but ruled out mechanical transmission systems. To provide for power amplification and to eliminate mechanical links, the aircraft designer uses a multitude of remotely controlled actuating devices, known more simply to the aircraft industry as actuators.
Keywords :
Actuators; Aircraft; Batteries; Compressors; Fasteners; Fluids; Generators;
fLanguage :
English
Journal_Title :
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher :
ieee
ISSN :
0097-2185
Type :
jour
DOI :
10.1109/TAI.1952.6371255
Filename :
6371255
Link To Document :
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