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