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