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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
19930065969
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lewicki, David G.
(NASA Lewis Research Center Cleveland, OH, United States)
Handschuh, Robert F.
(U.S. Army, Research Lab.; NASA, Lewis Research Center Cleveland, OH, United States)
Henry, Zachary S.
(Bell Helicopter Textron, Inc. Fort Worth, TX, United States)
Litvin, Faydor L.
(Illinois Univ. Chicago, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 93-2149
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASME, AIAA, SAE, ASEE
Accession Number
93A49966
Distribution Limits
Public
Copyright
Other

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