Fault-tolerant magnetic bearing control system architecture

• US 5,925,957 A
• Filed: 05/30/1997
• Issued: 07/20/1999
• Est. Priority Date: 05/30/1997
• Status: Expired due to Fees

• Current Assignee: Electric Boat Corporation (General Dynamics Corporation)
• Original Assignee: Electric Boat Corporation (General Dynamics Corporation)
• Inventors: Chapman, John H.
• Primary Examiner(s): Ramirez, Nestor
• Assistant Examiner(s): Nguyen, Tran N
• Application Number:
  US08/862,816
• Time in Patent Office: 781 Days
• Field of Search: 310/68 B, 310/90.5, 310/90, 310/51, 318/590, 318/591, 318/629, 318/565, 318/632, 318/621, 318/625
• US Class Current: 310/90.5
• CPC Class Codes: F16C 32/0442 with devices affected by abnormal, undesired or non-standard conditions such as shock-load, power outage, start-up or touchdown
• CPC Class Codes: F16C 32/0455 including digital signal processing [DSP] and analog/digital conversion [A/D, D/A]

Abstract

A fault-tolerant control system for a magnetic bearing arrangement which maximizes dynamic response of the control system is disclosed. The arrangement includes a main digital signal processor responsive to rotor position/velocity signals to supply control signals to bearing control coils and a secondary digital signal processor responsive to accelerometer signals to provide open-loop vibration control for correction of mass imbalance of the rotor system. In addition, sources of vibration which have fundamental frequencies at some multiple of the rotor system rotational frequency can also be controlled.

Claims

1. A bearing arrangement for devices comprising rotating and stationary members utilizing a magnetic field for levitating and controlling the positions of the rotating members along axes which include the axis of rotation and axes orthogonal thereto comprising control means including closed loop rotor position controller means comprising a first signal processing means and separate vibration sensing means comprising a second signal processing means which generates an open loop perturbation signal wherein the closed loop rotor position means includes one enabled closed-loop rotor position controller means and one disabled closed-loop rotor position controller means and the vibration sensing means simultaneously enables the disabled closed-loop rotor position controller means and disables the enabled closed-loop rotor position controller means if vibration sensed by the vibration sensing means exceeds a predetermined level.

2. A bearing arrangement in accordance with claim 1 further comprising at least one independent rotor position sensor for each axis dedicated to the one enabled closed-loop rotor position controller means and at least one independent rotor position sensor for each axis dedicated to each of the one disabled closed-loop rotor position controller means.

3. A bearing arrangement in accordance with claim 1 further comprising at least two independent power amplification means for receiving input signals dedicated to each of the one enabled closed-loop rotor position controller means and one disabled closed-loop rotor position controller means.

4. A bearing arrangement in accordance with claim 3 further comprising a control coil dedicated to each power amplification means for receiving current from each power amplification means and controlling the bearing along an axis of the bearing.

5. A bearing arrangement for rotating devices in accordance with claim 1 wherein the one enabled closed-loop rotor position controller means generates a control signal, and comprising means for summing both the open-loop perturbation signal and the control signal for use in attenuating vibration of the stationary members.

6. A bearing arrangement for rotating devices in accordance with claim 5 wherein the vibration sensing means includes a dedicated high frequency waveform synthesizer for generating an open-loop perturbation signal and the means for summing includes a high-speed summation device.

7. A bearing arrangement for rotating devices in accordance with claim 6 wherein the vibration sensing means includes means for generating the perturbation signal by applying arbitrary perturbation signals of known amplitudes, phase and frequency content relative to a rotating reference point located on the rotating members on at least one axis, means for calculating an influence coefficient matrix based on changes in vibration levels measured by the vibration sensing means, and means for calculating the amplitude, phase and frequency content of a perturbation signal that minimizes vibration measured by the vibration sensing means using the influence coefficient matrix.

8. A bearing arrangement as in claim 6 further comprising at least one attenuation means which decreases the amplitude of at least one rotor position signal sensed by the closed-loop position controller by a programmable gain at a programmable center frequency with a programmable filter quality.