Evaluation of a Variable Thickness Hybrid Composite Bull Gear

F-0074-2018-12859

5/14/2018

Authors
Abstract
Content

For several years, NASA Glenn Research Center and the U.S. Army Research Laboratory have been investigating hybrid (composite/steel) 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. Past research 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 prepreg 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.

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DOI
https://doi.org/10.4050/F-0074-2018-12859
Citation
LaBerge, K., Johnston, J., Handschuh, R., and Roberts, G., "Evaluation of a Variable Thickness Hybrid Composite Bull Gear," Vertical Flight Society 74th Annual Forum and Technology Display, Phoenix, Arizona, May 14, 2018, https://doi.org/10.4050/F-0074-2018-12859.
Additional Details
Publisher
Published
5/14/2018
Product Code
F-0074-2018-12859
Content Type
Technical Paper
Language
English