DocumentCode :
1442491
Title :
The power-recovery system of testing aircraft engines
Author :
Cassidy, G. E. ; Mosteller, W. A. ; Wright, W. L.
Author_Institution :
General Electric Company, Schenectady, N. Y.
Volume :
62
Issue :
5
fYear :
1943
fDate :
5/1/1943 12:00:00 AM
Firstpage :
240
Lastpage :
246
Abstract :
FOR its part in the development of the power-recovery system of testing aircraft engines the electrical industry may properly take pride. It has aided the war effort by helping to give to the aircraft-engine industry a testing technique that contains advantages not previously available. In this system of testing worth-while energy can be saved — more than half that required to operate an aircraft-engine manufacturing plant — and power demand can be reduced to the extent that power-demand costs and the capacities of power-supplying apparatus are materially reduced, engines can be tested with the ease and the quietness typical of electric machinery, testing can be carried on in buildings of simplified design, accurate electric load readings can be obtained to check and substantiate readings taken by conventional engine-testing methods, and, as reported by an aircraft engine builder, testing may be accomplished more quickly than with other systems. All of this can be done too on a basis that is economically sound.
Keywords :
Aircraft propulsion; Couplings; Engines; Generators; Loading; Synchronous machines; Testing;
fLanguage :
English
Journal_Title :
Electrical Engineering
Publisher :
ieee
ISSN :
0095-9197
Type :
jour
DOI :
10.1109/EE.1943.6435731
Filename :
6435731
Link To Document :
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