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Composites for Advanced Drive SystemsWith the desire for increased power/weight for advanced drive system configurations, the investigation of materials, like composites is being explored to determine the feasibility of integration into advanced drive systems. This area of research directly aligns with the vision of the NASA (National Aeronautics and Space Administration) Revolutionary Vertical Lift Technology (RVLT) Project, which is to enable a generation of vertical lift vehicles that can achieve aggressive goals in the areas of high speed, high efficiency, high performance, low noise, and low emissions.Composite materials are lightweight, especially when comparing to the metallic materials commonly utilized in rotorcraft drive systems. By integrating composite materials into the drive system, the potential for improvements to power/weight exists as well as other potential benefits such as reductions in vibration and/or noise. Each of these areas of potential benefit will largely influence the overall performance and reliability of future vertical lift vehicles. Prior NASA research has been performed that developed a prototype hybrid double helical bull gear which was successfully demonstrated (LaBerge, Kelsen E.; Handschuh, Robert F.; Roberts, Gary; Thorp, Scott;, 2016) and current NASA research is being performed to optimize the hybrid gear design.While the potential benefits of composite materials in vertical lift drive systems mentioned above are highly desirable, many challenges exist that need to be addressed. To address the benefits and challenges with the integration of composite materials in advanced vertical lift drive systems, the identification of advanced drive system configurations and technical challenges is required. For this project, Bell Helicopter Textron identified an advanced drive system configuration and provided conceptual designs for this advanced drive system configuration, identified technical challenges, and provided recommendations as to how those challenges can be overcome.
Document ID
20190027496
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Anderson, Cody
(Textron Bell Helicopter Fort Worth, TX, United States)
Morales, Gilbert
(Textron Bell Helicopter Fort Worth, TX, United States)
Date Acquired
July 18, 2019
Publication Date
July 1, 2019
Subject Category
Aircraft Design, Testing And Performance
Composite Materials
Report/Patent Number
GRC-E-DAA-TN64203
NASA/CR—2019-220145
E-19666
Report Number: GRC-E-DAA-TN64203
Report Number: NASA/CR—2019-220145
Report Number: E-19666
Funding Number(s)
WBS: 664817.02.03.02.02.04
CONTRACT_GRANT: NNA15AB11B
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
transmission
rotorcraft
gear
composite
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