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Helical Face Gear Development Under the Enhanced Rotorcraft Drive System ProgramU.S. Army goals for the Enhanced Rotorcraft Drive System Program are to achieve a 40 percent increase in horsepower to weight ratio, a 15 dB reduction in drive system generated noise, 30 percent reduction in drive system operating, support, and acquisition cost, and 75 percent automatic detection of critical mechanical component failures. Boeing s technology transition goals are that the operational endurance level of the helical face gearing and related split-torque designs be validated to a TRL 6, and that analytical and manufacturing tools be validated. Helical face gear technology is being developed in this project to augment, and transition into, a Boeing AH-64 Block III split-torque face gear main transmission stage, to yield increased power density and reduced noise. To date, helical face gear grinding development on Northstar s new face gear grinding machine and pattern-development tests at the NASA Glenn/U.S. Army Research Laboratory have been completed and are described.
Document ID
20120000867
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Heath, Gregory F.
(Boeing Co. Mesa, AZ, United States)
Slaughter, Stephen C.
(Boeing Co. Mesa, AZ, United States)
Fisher, David J.
(Northstar Aerospace Milton, Ontario, Canada)
Lewicki, David G.
(NASA Glenn Research Center Cleveland, OH, United States)
Fetty, Jason
(Army Aviation Fort Eustis, VA, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2011
Subject Category
Mechanical Engineering
Report/Patent Number
AHS 2011-000270
NASA/TM-2011-217125
E-17814
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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