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Experimental Comparison of Face-Milled and Face-Hobbed Spiral Bevel GearsAn experimental comparison of face-milled and face-hobbed spiral bevel gears was accomplished. The two differently manufactured spiral bevel gear types were tested in a closed-loop facility at NASA Glenn Research Center. Strain, vibration, and noise testing were completed at various levels of rotational speed and load. Tests were conducted from static (slow-roll) to 12600 rpm and up to 269 N-m (2380 in.-lb) pinion speed and load conditions. The tests indicated that the maximum stress recorded at the root locations had nearly the same values, however the stress distribution was different from the toe to the heel. Also, the alternating stress measured was higher for the face-milled pinion than that attained for the face-hobbed pinion (larger minimum stress). The noise and vibration results indicated that the levels measured for the face-hobbed components were less than those attained for the face-milled gears tested.
Document ID
20020006307
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Handschuh, Robert F.
(Army Research Lab. Cleveland, OH United States)
Nanlawala, Michael
(Illinois Inst. of Tech. Chicago, IL United States)
Hawkins, John M.
(Rools-Royce Corp. Indianapolis, IN United States)
Mahan, Danny
(Army Aviation and Missile Command Redstone Arsenal, AL United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2001
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:210940
ARL-TR-1104
E-12793
NASA/TM-2001-210940
Meeting Information
Meeting: International Conference on Motion and Power Transmission
Location: Fukuoka
Country: Japan
Start Date: November 15, 2001
End Date: November 17, 2001
Sponsors: Japan Society of Mechanical Engineers
Funding Number(s)
PROJECT: DA Proj. 1L1-62211-A-47-A
PROJECT: RTOP 712-30-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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