NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Ball Bearings Equipped for In Situ Lubrication on DemandIn situ systems that provide fresh lubricants to ball/race contacts on demand have been developed to prolong the operational lives of ball bearings. These systems were originally intended to be incorporated into ball bearings in mechanisms that are required to operate in outer space for years, in conditions in which lubricants tend to deteriorate and/or evaporate. These systems may also be useful for similarly prolonging bearing lifetimes on Earth. Reservoirs have been among the means used previously to resupply lubricants. Lubricant- resupply reservoirs are bulky and add complexity to bearing assemblies. In addition, such a reservoir cannot be turned on or off as needed: it supplies lubricant continuously, often leading to an excess of lubricant in the bearing. A lubricator of the present type includes a porous ring cartridge attached to the inner or the outer ring of a ball bearing (see Figure 1). Oil is stored in the porous cartridge and is released by heating the cartridge: Because the thermal expansion of the oil exceeds that of the cartridge, heating causes the ejection of some oil. A metal film can be deposited on a face of the cartridge to serve as an electrical-resistance heater. The heater can be activated in response to a measured increase in torque that signals depletion of oil from the bearing/race contacts. Because the oil has low surface tension and readily wets the bearing-ring material, it spreads over the bearing ring and eventually reaches the ball/race contacts. The Marangoni effect (a surface-tension gradient associated with a temperature gradient) is utilized to enhance the desired transfer of lubricant to the ball/race contacts during heating. For a test, a ball bearing designed for use at low speed was assembled without lubricant and equipped with a porous-ring lubricator, the resistance heater of which consumed a power of less than 1 W when triggered on by a torque-measuring device. In the test, a load of 20 lb (.89 N) was applied and the bearing was turned at a rate of 200 RPM. The lubricator control was turned on at the beginning of the test, turned off for about 800 seconds, then turned on again. As shown in Figure 2, the controlled lubricator stabilized the torque in a low range, starting immediately after initial turn-on and immediately after resumption of the lubricator control.
Document ID
20110014764
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Tech Brief
Authors
Marchetti, Mario
(National Academy of Sciences - National Research Council Cleveland, OH, United States)
Jones, William R., Jr.
(NASA Glenn Research Center Cleveland, OH, United States)
Pepper, Stephen V.
(NASA Glenn Research Center Cleveland, OH, United States)
Jansen, Mark
(Sest, Inc. Cleveland, OH, United States)
Predmore, Roamer
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
March 1, 2005
Publication Information
Publication: NASA Tech Briefs, March 2005
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LEW-17414
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available