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Effect of two synthetic lubricants on life of AISI 9310 spur gearsSpur-gear fatigue tests were conducted with two lubricants using a single lot of consumable-electrode vacuum-melted (CVM) AISI 9310 spur gears. The gears were case carburized and hardened to Rockwell C60. The gear pitch diameter was 8.89 cm. The lot of gears was divided into two groups, each of which was tested with a different lubricant. The test lubricants can be classified as synthetic polyol-ester-based lubricants. One lubricant was 30 percent more viscous that the other. Both lubricants have similar pressure viscosity coefficients. Test conditions included a bulk gear temperature of 350 K, a maximum Hertz stress of 1.71 GPa at the pitch line, and a speed of 10,000 rpm. The surface fatigue life of gears tested with one lubricant was approximately 2.4 times that for gears tested with the other lubricant. The lubricant with the 30 percent higher viscosity gave a calculated elastohydrodynamic (EHD) film thickness that was 20 percent higher than the other lubricant. This increased EHD film thickness is the most probable reason for the improvement in surface fatigue life of gears tested with this lubricant over gears tested with the less viscous lubricant.
Document ID
19910020285
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Townsend, Dennis P.
(NASA Lewis Research Center Cleveland, OH., United States)
Shimski, John
(Naval Air Propulsion Test Center Trenton, NJ., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
E-6004
AVSCOM-TR-91-C-011
NASA-TM-104352
NAS 1.15:104352
Report Number: E-6004
Report Number: AVSCOM-TR-91-C-011
Report Number: NASA-TM-104352
Report Number: NAS 1.15:104352
Accession Number
91N29599
Funding Number(s)
PROJECT: DA PROJ. 1L1-62211-A-47A
PROJECT: RTOP 505-63-36
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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