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A New High-Speed, High-Cycle, Gear-Tooth Bending Fatigue Test CapabilityA new high-speed test capability for determining the high cycle bending-fatigue characteristics of gear teeth has been developed. Experiments were performed in the test facility using a standard spur gear test specimens designed for use in NASA Glenn s drive system test facilities. These tests varied in load condition and cycle-rate. The cycle-rate varied from 50 to 1000 Hz. The loads varied from high-stress, low-cycle loads to near infinite life conditions. Over 100 tests were conducted using AISI 9310 steel spur gear specimen. These results were then compared to previous data in the literature for correlation. Additionally, a cycle-rate sensitivity analysis was conducted by grouping the results according to cycle-rate and comparing the data sets. Methods used to study and verify load-path and facility dynamics are also discussed.
Document ID
20110012902
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stringer, David B.
(Army Research Lab. Cleveland, OH, United States)
Dykas, Brian D.
(Army Research Lab. Cleveland, OH, United States)
LaBerge, Kelsen E.
(Army Research Lab. Cleveland, OH, United States)
Zakrajsek, Andrew J.
(Purdue Univ. West Lafayette, IN, United States)
Handschuh, Robert F.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
June 1, 2011
Subject Category
Mechanical Engineering
Report/Patent Number
E-17745
NASA/TM-2011-217039
ARL-TR-5506
Report Number: E-17745
Report Number: NASA/TM-2011-217039
Report Number: ARL-TR-5506
Meeting Information
Meeting: 67th Annual Forum and Technology Display (Forum 67)
Location: Virginia Beach, VA
Country: United States
Start Date: May 3, 2011
End Date: May 5, 2011
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
WBS: WBS 877868.02.07.03.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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