Method and apparatus for balancing

• US 20070062278A1
• Filed: 10/30/2006
• Published: 03/22/2007
• Est. Priority Date: 03/31/1999
• Status: Active Grant

• Current Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Original Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Inventors: Dyer, Stephen
• Granted Patent: US 7,454,970 B2
• Time in Patent Office: Days
• US Class Current: 73/458
• CPC Class Codes: G01M 1/22 and converting vibrations due to imbalance into electric variables
• CPC Class Codes: G01M 1/36 by adjusting position of masses built-in the body to be tested

Abstract

A balanced rotating assembly with a spindle automatically provides balancer limits, which achieves a balancing state while substantially minimizing short term vibration increases and which provides for multi-plane balancer dithering.

Claims

1. A balanced assembly with a spindle comprising:

A first movable rotor and a second movable rotor which are deployed upon said rotating assembly and which are selectively movable about said spindle of said rotating assembly; and

a controller for controlling movement of said first movable rotor and second movable rotor and adapted to calculate a value and to periodically modify said value and to cause said first movable rotor and said second movable rotor to move in accordance with said calculated value and said modified value, wherein said values are adjusted during a plurality of control iterations to reduce vibrational signals from an at least one vibration sensor.

2. A rotating assembly, said rotating assembly including a controller for controlling a rotating assembly vibration comprising:

at least a first movable rotor and a second movable rotor which are selectively movable about said rotating assembly; and

at least one vibration sensor for communicating vibrational data to aid controller, and at least one position sensor for providing positioning information to said controller on the position of said first movable rotor and on the position of said second movable rotor, said controller controlling movement of said first movable rotor and said second movable rotor and adapted to calculate values and to adjust at least two parameters during at least two control iterations, wherein said controller is effective to cause said first rotor and said second rotor to move in accordance with said value to reduce vibrations sensed by said at least one vibration sensor.

3. The assembly of claim 2 wherein said controller calculates said value through recursive exponentially weighted averaging.

4. The assembly of claim 2 wherein said parameters are a gain parameter and a forgetting factor.

5. The assembly of claim 4 wherein said gain parameter is within a range of zero to one in value.

6. The assembly of claim 4 wherein said forgetting factor is within a range of zero to one in value.

7. The assembly of claim 4 wherein said controller automatically adjusts both said gain parameter and said forgetting factor during each of said control iterations.

8. The assembly of claim 2 wherein said controller comprising at least one vibration sensor is disposed in close proximity to said rotating assembly, wherein said at least one vibration sensor is an accelerometer which measures said rotating assembly vibration.

9. The assembly of claim 2 wherein said controller samples said vibrational data and depending upon a level of said sampled vibrational data moves said first and second rotor.

10. The assembly of claim 2 wherein said controller measures said rotating assembly vibration as a vibration error phasor with a phase angle and a magnitude and calculates a correction phasor with a correction magnitude and a correction phase angle.

11. A rotating machinery assembly, said assembly comprising:

at least one movable rotor member which is deployed upon said rotating machinery assembly, said at least one movable rotor member having a weight distribution, wherein said at least one movable rotor member is selectively movable to produce a corrective phasor with a correction magnitude and a correction phase angle;

a vibration sensor which senses a vibration and generates a vibration signal; and

a controller for controlling said at least one movable member wherein said controller receives said vibration signal from said vibration sensor and calculates a phasor value to selectively move said at least one movable rotor member to produce a corrective phasor to reduce said sensor vibration.

12. The assembly of claim 11 wherein said assembly includes at least one position sensor for providing positioning information on said at least one movable rotor member.

13. The assembly of claim 11, wherein said controller including a supervisory control strategy for deactivating controller movement of said movable member.

14. The assembly of claim 11, wherein said controller computes a synchronous vibration error phasor.

15. The assembly of claim 11, wherein said controller calculates an angular location of said at least one movable rotor.

16. A method for vibration balancing a rotatable assembly, said method comprising the steps of:

measuring a vibration of said assembly during a control interval;

calculating a value during said control interval;

adjusting at least one parameter based upon said calculated value;

deploying a vibration balancing rotor upon said assembly;

calculating a correction movement of said vibration balancing rotor as a function of said value; and

moving said vibration balancing rotor with said correction movement.

17. The method of claim 16 wherein said at least one parameter comprises a gain parameter and a forgetting factor.

18. The method of claim 17 wherein said step of adjusting said at least one parameter further comprises the steps of:

determining an accuracy of said calculated value;

increasing said at least one gain parameter and reducing said forgetting factor if said calculated value is relatively accurate; and

decreasing said gain parameter and increasing said forgetting factor if said calculated value is relatively inaccurate.

19. The method of claim 16 further comprising the step of determining a vibrational error signal as a phasor having a phase angle and a magnitude.