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Lighter, More-Efficient Helicopter TransmissionsImproved gear system intended primarily for use in helicopter transmits torque from horizontal or nearly horizontal shafts of two engines to vertical output shaft supporting rotor. Apportions torques equally along multiple, redundant drive paths, reducing stresses on individual gear teeth, and enables one engine to continue to turn rotor when other engine fails. Design concept also applied to couple two airplane engines to set of propellers in such way both propellers turn as long as at least one engine operates.
Document ID
19930000795
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bossler, Robert B., Jr.
(Lucas Western, Inc.)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 12
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-15158
Report Number: LEW-15158
ISSN: 0145-319X
Accession Number
93B10795
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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