DocumentCode :
1346458
Title :
Aircraft tachometer indicator ¿ An analysis of design factors affecting starting performance
Author :
Akeley, L. T.
Author_Institution :
General Electric Company, Lynn, Mass.
Volume :
73
Issue :
6
fYear :
1955
Firstpage :
398
Lastpage :
403
Abstract :
FIFTY years of powered flight have brought changes to aircraft controls. A pilot cannot properly control the flight of today´s powerful machines without the use of instruments. Many of the newer instruments and control devices embody electronic elements for sensitivity and speed of response. Some have servo-system operation for highest accuracy. One of the oldest instruments, the engine speed indicator,1 still has an important place on the aircraft instrument panel. Without electronic components or servo elements the simple dragmagnet ¿ eddy-current disk type of tachometer instrument continues to provide a highly accurate and dependable service to the pilot.
Keywords :
Equations; Hysteresis motors; Magnetic hysteresis; Mathematical model; Rotors; Shafts; Torque;
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.1955.6367089
Filename :
6367089
Link To Document :
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