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Improved Apparatus for Testing Monoball BearingsA desk-sized apparatus for testing monoball bearings and their lubricants offers advantages, relative to prior such apparatuses, of (1) a greater degree of automation and (2) capability of operation under wider and more realistic ranges of test conditions. The ranges of attainable test conditions include load from 100 to greater h than 50,000 lb (445 to greater than 2.22 x 10(exp 5) N), resisting torque up to 30,000 lb-in. (approximately equal to 3,390 N-m), oscillating rotation through an angle as large as 280 degrees, and oscillation frequency from 0 to 6 Hz. With addition of some components and without major modification of the apparatus, it is also possible to perform tests under environmental conditions that include temperature from -320 to 1,000 F (-196 to +538 C), relative humidity from 0 to 100 percent, and either air at ambient pressure, high vacuum, or an atmosphere of monatomic oxygen. In the apparatus (see Figure 1), a monoball bearing specimen is driven in oscillating rotation by a hydraulic rotary actuator through a series of shafts, one of which incorporates a torque meter and one of which is a flexible coupling. The torque meter measures the resisting torque; the flexible coupling accommodates misalignment, wear, and compression of the specimen and ensures equal loading on opposite sides of the monoball. Not shown in the figure is an angular-position sensor that is used for measuring the angle of rotation of the shafts.
Document ID
20110014161
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Hall, Phillip B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Novak, Howard L.
(USBI/USA Co. United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2006
Publication Information
Publication: NASA Tech Briefs, November 2006
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-31706-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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