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Advanced Flywheel Energy Storage for Pulsed Power Applications

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N00014-05-C-0365
Agency Tracking Number: N045-013-0384
Amount: $486,397.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: N04-T013
Solicitation Number: N/A
Timeline
Solicitation Year: 2004
Award Year: 2006
Award Start Date (Proposal Award Date): 2006-06-08
Award End Date (Contract End Date): 2007-12-08
Small Business Information
12880 Moore Street
Cerritos, CA 90703
United States
DUNS: 036250533
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Patrick McMullen
 Vice President
 (562) 293-1685
 pat@calnetix.com
Business Contact
 Patrick McMullen
Title: Vice President
Phone: (562) 293-1685
Email: pat@calnetix.com
Research Institution
 TEXAS A&M UNIV.
 Hamid Toliyat
 
3128 TAMU
College Park, TX 77843
United States

 (979) 862-3034
 Nonprofit College or University
Abstract

During the NAVY STTR Phase II Calnetix will further develop its concept of advanced flywheel system proposed in Phase I and will demonstrate the validity of the underlying principles through building and testing a system prototype. This prototype will be a fully functional system capable of supporting up to 2MW of pulse power with the ability of producing 500kW (30 seconds) loads in high-duty-cycle operation. The need for this system has been identified in both NAVY and commercial applications. The proposed design will feature several novel technical solutions resulting in a very compact and reliable high-performance system. These include unique magnetic suspension based around patented Calnetix homopolar PM-biased magnetic bearings, further improved to increase system efficiency and meet high dynamic load requirements encountered in NAVY applications; power electronic vector controls, which allows for boosting power output of PM machines by several times for short periods of time; as well as several technical solutions addressing thermal issues of operating a PM motor/generator in both high-duty-cycle and pulse-power flywheel applications. All of these innovations are rather fundamental in nature, and once proven, could be transferred to other flywheel systems varying in powers and amounts of stored energy. In particular, a concept of a flywheel system to provide sufficient energy and power to launch and aircraft in EMALS has been proposed during the Phase I study.

* Information listed above is at the time of submission. *

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