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Evaluation of a Variable Thickness Hybrid Composite Bull GearFor several years, NASA Glenn Research Center and the U.S. Army Research Laboratory have been investigating hybrid (compositesteel) gear technology for use in vertical lift drive systems. The hybrid gear concept replaces the structural portion of a gear between the shaft and the gear rim with a lightweight carbon fiber composite, in an effort to reduce the overall weight of a gear and increase the drive system power density. An overview of the concept of the hybrid gear design is described in Ref. 1, 2, and 3. The research presented in these references includes both small-scale and large-scale hybrid gear concepts all of which have a constant composite thickness throughout. The design described in this paper is of a variable thickness, such that the composite is thickest at the inner diameter and this thickness is gradually reduced toward the outer diameter. The resulting stair stepped design stems from dropping plies of the braided carbon fiber composite fabric gradually with increased radius. Additionally, the interlock pattern at the inner metallic adapter was adjusted slightly from previous designs to obtain a better stress distribution on the inner metallic adapter. The manufactured variable thickness web was tested both in static torsion tests and operationally in a relevant gearbox environment. The results of these experiments will be presented and compared to a baseline steel configuration.
Document ID
20180005466
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
LaBerge, Kelsen
(Army Research Lab. Cleveland, OH, United States)
Johnston, Joel
(Universities Space Research Association (USRA) Cleveland, OH, United States)
Handschuh, Robert
(NASA Glenn Research Center Cleveland, OH, United States)
Roberts, Gary D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 24, 2018
Publication Date
May 16, 2018
Subject Category
Mechanical Engineering
Report/Patent Number
GRC-E-DAA-TN56366
Meeting Information
Meeting: Annual Forum & Technology Display of the Vertical Flight Society
Location: Phoenix, AZ
Country: United States
Start Date: May 14, 2018
End Date: May 17, 2018
Sponsors: Vertical Flight Society
Funding Number(s)
WBS: WBS 664817.02.03.02.02.01
CONTRACT_GRANT: NNH15CO48B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Rotorcraft Propulsion
Drive Systems
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