ADVANCED COMPOSITE FLYWHEEL STRUCTURAL DESIGN FOR A PULSED DISK ALTERNATOR

Citation
Dh. Curtiss et al., ADVANCED COMPOSITE FLYWHEEL STRUCTURAL DESIGN FOR A PULSED DISK ALTERNATOR, IEEE transactions on magnetics, 31(1), 1995, pp. 26-31
Citations number
5
Categorie Soggetti
Engineering, Eletrical & Electronic","Physics, Applied
ISSN journal
00189464
Volume
31
Issue
1
Year of publication
1995
Part
1
Pages
26 - 31
Database
ISI
SICI code
0018-9464(1995)31:1<26:ACFSDF>2.0.ZU;2-4
Abstract
Electromagnetic guns require pulsed power supplies that deliver energy to the gun breech in the 2-6 millisecond regime. A flywheel energy st orage machine in which the disk rotor contains the field excitation wi ndings appears to be a practical approach to meeting energy/power dens ity requirements. The general concept of constructing an axisymmetric disk to obtain a radial to hoop elastic modulus ratio (E(r)/E(theta)) that optimizes the strength of a radially thick disk is presented. A c arbon fiber - epoxy rotor disk designed to operate at 650 meters pdr s econd rim speed with a 23% Copper conductor thickness fraction is revi ewed. Results of sub-scale and/or sub-thickness spin test disks are al so discussed.