DocumentCode
1496029
Title
Electrical prerotation of landing gear wheels
Author
Keyser, J. H.
Author_Institution
Lockheed Aircraft Corporation, Burbank, Calif.
Volume
67
Issue
12
fYear
1948
Firstpage
1154
Lastpage
1159
Abstract
Landing wheel prerotation often has been considered as a means of reducing tire wear, however a more careful study of the problem brings out other more important advantages, the most important of which is reduction of structural loads. The wheel prerotation described in this article has a number of features to insure reliability. Since adequate electrical prerotation has been achieved, it appears to be well worth consideration for use on very large aircraft with multiple landing wheels.
Keywords
Acceleration; Blades; Gears; Induction motors; Tires; Torque; Wheels;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1948.6444490
Filename
6444490
Link To Document