Rotor Dynamics of Flywheel Energy Storage Systems

Author:

Jayaraman C. P.1,Kirk J. A.2,Anand D. K.2,Anjanappa M.3

Affiliation:

1. Fairchild Space, Germantown, MD 20874

2. Department of Mechanical Engineering and The Systems Research Center, University of Maryland, College Park, MD 20742

3. University of Maryland—UMBC, Baltimore, MD 21228

Abstract

This paper deals with the dynamic analysis of the magnetic bearing stack system. The stack consists of a single flywheel supported by two magnetic bearings. To model the system, the dynamic equations of a magnetically suspended flywheel are derived. Next, the four control systems controlling the four degrees-of-freedom of the stack are incorporated into the model. The resulting dynamic equations are represented as first-order differential equations in a matrix form. A computer simulation program was then used to simulate the working of the magnetic bearing stack. Real time plots from the simulation are used to show the effect of dynamic coupling on torque response. Frequency response is used to determine the resonance frequencies of the stack system. It is found that system stability depends on flywheel speed. On the basis of the above results suggestions are made to improve stability and allow the stack to be spun beyond 60,000 rpm.

Publisher

ASME International

Subject

Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Magnetically Suspended VSCMGs for Simultaneous Attitude Control and Power Transfer IPAC Service;Journal of Dynamic Systems, Measurement, and Control;2010-08-11

2. MIMO Active Vibration Control of Magnetically Suspended Flywheels for Satellite IPAC Service;Journal of Dynamic Systems, Measurement, and Control;2008-06-05

3. Parametric Analysis of Fiber-Reinforced Laminated Momentum Wheel Rotors;Journal of Spacecraft and Rockets;2002-07

4. Parametric analysis of fiber-reinforced laminated momentum wheel rotors;19th AIAA Applied Aerodynamics Conference;2001-06-11

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