NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Study of Lubricant Jet Flow Phenomena in Spur Gears: Out of Mesh ConditionOil jet lubrication on the disengaging side of a gear mesh was analyzed. Results of the analysis were computerized and used to determine the oil jet impingement depth for several gear ratios and oil jet to pitch line velocity ratios. A gear test rig using high speed photography was used to experimentally determine the oil jet impingement depth on the disengaging side of mesh. Impingement depth reached a maximum at gear ratio near 1.5 where chopping by the leading gear tooth limited impingement depth. The pinion impingement depth is zero above a gear ratio of 1.172 for a jet velocity to pitch time velocity ration of 1.0 and is similar for other velocity ratios. The impingement depth for gear and pinion are equal and approximately one half the maximum at a gear ration of 7.0.
Document ID
19770025560
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Townsend, D. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Akin, L. S.
(Western Gear Corp. Lynnwood, Calif., United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1977
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-73694
E-9230
Report Number: NASA-TM-73694
Report Number: E-9230
Meeting Information
Meeting: 1977 Intern. Gear Conf.
Location: Chicago
Start Date: September 28, 1977
End Date: September 30, 1977
Sponsors: ASME
Accession Number
77N32504
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available