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Title
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Solid Lubricated Bearing Technology. Part I. Solid Lubricated High Speed Ball Bearing
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Date
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1971
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Index Abstract
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Not Available
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Photo Quality
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Complete
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Report Number
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AFAPL TR 71-69 Part 1
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Corporate Author
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Wetinghouse Research Labs, Pittsburgh, Pennsylvania
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Laboratory
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Air Force Aero Propulsion Laboratory
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Extent
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59
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NTRL Accession Number
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AD731163
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Identifier
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AD0731163
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Access Rights
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Approved for public release; distribution unlimited.
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Distribution Classification
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1
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Contract
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F33615-70-C-1736
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DoD Project
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3048
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DoD Task
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304806
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Distribution Conflict
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No
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Abstract
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This report describes the first year's effort of a two year program that has as its objective the development of improved self-contained, solid lubricated ball bearings capable of at least 25 hours operation at speeds approaching 60,000 rpm. The program encompasses a temperature range of -40F to 600F and a maximum load combination of 75 lb thrust/25 lb radial. The work is a follow-on effort to the completed Air Force funded program F33615-68-C-1250. During this reporting period, a high speed test stand was designed and manufactured that is capable of functionally evaluating the performance of solid lubricated, 207 ball bearings over a 30,000 to 60,000 rpm speed range. The device incorporates a 40 H.P., variable speed motor driving a transmission having a 15:1 gear ratio. A test head containing two test bearings is coupled to the output shaft of the transmission. The functional test portion of the program has thus far achieved a maximum life of 15 hours on a solid lubricated ball bearing operating at 30,000 rpm and a temperature of 200F.
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Report Availability
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Full text available
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Date Issued
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1971-08
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Publisher
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Wright-Patterson Air Force Base, OH : Air Force Aero Propulsion Laboratory, Air Force Systems Command
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Provenance
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource
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Creator
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Boes, D. J.