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Shape optimization of disc-type flywheelsTechniques were developed for presenting an analytical and graphical means for selecting an optimum flywheel system design, based on system requirements, geometric constraints, and weight limitations. The techniques for creating an analytical solution are formulated from energy and structural principals. The resulting flywheel design relates stress and strain pattern distribution, operating speeds, geometry, and specific energy levels. The design techniques incorporate the lowest stressed flywheel for any particular application and achieve the highest specific energy per unit flywheel weight possible. Stress and strain contour mapping and sectional profile plotting reflect the results of the structural behavior manifested under rotating conditions. This approach toward flywheel design is applicable to any metal flywheel, and permits the selection of the flywheel design to be based solely on the criteria of the system requirements that must be met, those that must be optimized, and those system parameters that may be permitted to vary.
Document ID
19760021188
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nizza, R. S.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Energy Production And Conversion
Accession Number
76N28276
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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