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Operational Condition and Superfinishing Effect on High-Speed Helical Gearing System PerformanceAn experimental effort has been conducted on an aerospace-quality helical gear train to investigate the thermal behavior of the gear system. Oil inlet temperature was varied from 160 to 250 F. Also, the test gears were run in both an as-ground condition and after isotropic superfinishing (ISF) condition. In-depth temperature measurements were made across the face width and at the axial end of the gear mesh. Supply power measurements were made at varying speeds and loads up to 5000 hp and 15000 rpm (pitch line velocity to 24000 feet per minute). Test results from the parametric studies and the superfinishing process are presented. The tests indicated that superfinishing offered no improvement in performance due to the high lubricant film thickness generated by the extremely high pitch line velocity that the majority of the tests were conducted. Increasing lubricant inlet temperature had the most dramatic effect on performance improvement.
Document ID
20070022618
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Handschuh, R.
(Army Research Lab. Cleveland, OH, United States)
Kilmain, C.
(Bell Heliciopter Textron Inc. Fort Worth, TX, United States)
Ehinger, R.
(Bell Heliciopter Textron Inc. Fort Worth, TX, United States)
Date Acquired
August 23, 2013
Publication Date
June 1, 2007
Subject Category
Mechanical Engineering
Report/Patent Number
E-15897
NASA/TM-2007-214696
ARL-TR-4099
Report Number: E-15897
Report Number: NASA/TM-2007-214696
Report Number: ARL-TR-4099
Meeting Information
Meeting: American Helicopter Society 63rd Annual Forum and Technology Display
Location: Virginia Beach, VA
Country: United States
Start Date: May 1, 2007
End Date: May 3, 2007
Sponsors: American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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