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Powered wheels for aircraftEngineering details, project status, system design and specifications, and test results are presented on a powered-wheel drive system based on the Dynavector rotary actuator. The design and operation of the Dynavector system (with positive displacement very-low-inertia nonrotating vane motor) are reviewed. Feasibility studies, contract data, and findings of braking tests are described. Exploded diagrams of Dynavector details are displayed. Success in using powered wheels in lieu of aircraft main engines for on-ground movements should bring benefits in energy conservation, noise abatement, reduced pollution, and alleviated congestion in the terminal area.
Document ID
19760053630
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Long, M. J.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 760521
Meeting Information
Meeting: Air Transportation Meeting
Location: New York, NY
Start Date: May 18, 1976
End Date: May 20, 1976
Sponsors: Society of Automotive Engineers
Accession Number
76A36596
Distribution Limits
Public
Copyright
Other

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