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Low-noise, high-strength, spiral-bevel gears for helicopter transmissionsImprovements in spiral-bevel gear design were investigated to support the Army/NASA Advanced Rotorcraft Transmission program. Program objectives were to reduce weight by 25 percent, reduce noise by 10 dB, and increase life to 5000 hr mean-time-between-removal. To help meet these goals, advanced-design spiral-bevel gears were tested in an OH-58D helicopter transmission using the NASA 500-hp Helicopter Transmission Test Stand. Three different gear designs tested included: (1) the current design of the OH-58D transmission except gear material X-53 instead of AISI 9310; (2) a higher-strength design the same as the current but with a full fillet radius to reduce gear tooth bending stress (and thus, weight); and (3) a lower-noise design the same as the high-strength but with modified tooth geometry to reduce transmission error and noise. Noise, vibration, and tooth strain tests were performed and significant gear stress and noise reductions were achieved.
Document ID
19930013830
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lewicki, David G.
(NASA Lewis Research Center Cleveland, OH, United States)
Handschuh, Robert F.
(NASA Lewis Research Center Cleveland, OH, United States)
Henry, Zachary S.
(Bell Helicopter Co. Fort Worth, TX., United States)
Litvin, Faydor L.
(Chicago Univ. IL., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:106080
ARL-MR-71
NASA-TM-106080
AD-A263116
AIAA PAPER 93-2149
E-7698
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: AIAA, ASME, ASEE, SAE
Accession Number
93N23019
Funding Number(s)
PROJECT: DA PROJ. 1L1-62211-A-47-A
PROJECT: RTOP 505-62-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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