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Functioning of reduction gears on airplane enginesIn undertaking to analyze the functioning conditions of a reduction gear on an aviation engine, we will consider an ordinary twelve-cylinder V-engine. The reduction gear employed consists either of a pair of spur gears, one of which is integral with the engine shaft and the other with the propeller shaft, or of a planetary system of gears.
Document ID
19930090733
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Matteucci, Raffaelli
Date Acquired
September 6, 2013
Publication Date
March 1, 1926
Report/Patent Number
NACA-TM-352
Report Number: NACA-TM-352
Accession Number
93R20023
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GEARS, REDUCTION
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