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Wormgear geometry adopted for implementing hydrostatic lubrication and formulation of the lubrication problemThe geometrical parameters for a wormgear intended to be used as the transmission in advanced helicopters are finalized. The resulting contact pattern of the meshing tooth surfaces is suitable for the implementation of hydrostatic lubrication Fluid film lubrication of the contact is formulated considering external pressurization as well as hydrodynamic wedge and squeeze actions. The lubrication analysis is aimed at obtaining the oil supply pressure needed to separate the worm and gear surfaces by a prescribed minimum film thickness. The procedure of solving the mathematical problem is outlined.
Document ID
19950013151
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sun, D. C.
(State Univ. of New York Binghamton, NY, United States)
Yuan, Qin
(State Univ. of New York Binghamton, NY, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publisher: NASA
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-195416
AD-A290331
ARL-CR-219
NAS 1.26:195416
E-9345
Report Number: NASA-CR-195416
Report Number: AD-A290331
Report Number: ARL-CR-219
Report Number: NAS 1.26:195416
Report Number: E-9345
Accession Number
95N19567
Funding Number(s)
PROJECT: DA PROJ. 1L1-61102-AH-45
CONTRACT_GRANT: NAG3-1316
PROJECT: RTOP 505-62-OJ
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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