Method of and system for balancing a rotor

• US 4,489,606 A
• Filed: 07/26/1982
• Issued: 12/25/1984
• Est. Priority Date: 07/27/1981
• Status: Expired due to Term

• Current Assignee: Hitachi, Ltd.
• Original Assignee: Hitachi, Ltd.
• Inventors: Watanabe, Takashi, Shiohata, Kouki, Fujisawa, Fumio, Ishibashi, Yasumasa
• Primary Examiner(s): Gill, James J.
• Application Number:
  US06/401,720
• Time in Patent Office: 883 Days
• Field of Search: 73/66, 73/462, 364/463, 364/508
• US Class Current: 73/462
• CPC Class Codes: G01M 1/22 and converting vibrations due to imbalance into electric variables

Abstract

A method of and a system for reducing an excessive amplitude of unbalance vibration occurring in a rotor by actually measuring and comparing the unbalance vibration amplitude of the rotor with a desired level for judgement as to whether the desired value is exceeded, selecting a certain correction plane combination in accordance with the measured unbalance vibration amplitude. A correction mass to be added to the rotor is calculated using an influence coefficient corresponding to the selected correction plane combination, assuming that the correction mass is added to the rotor, estimated residual vibration amplitudes and root mean squares thereof are calculated at respective correction plane position combinations each having at least any two of positions of a plurality of correction planes on the rotor.

Claims

1. A rotor balancing method for reducing excessive amplitude of unbalanced vibration occuring in a rotor of a rotary machine, the method comprising the steps of:

actually measuring an unbalance vibration amplitude of said rotor;

judging whether a desired level is exceeded by the actually measured unbalance vibration amplitude;

selecting at least one of a plurality of correction plane combinations each having at least any two of the correction planes preset on said rotor, based on said actually measured vibration amplitude, when said desired level is exceeded by said actually measured unbalance vibration amplitude;

computing a correction mass to be added to said rotor, using one of a plurality of influence coefficients preset to the respective correction plane combinations, corresponding to said at least one selected correction plane combination;

computing on an assumption that said correction mass is added to said rotor, estimated residual vibration amplitudes and root mean squares of said estimated residual vibration amplitude;

comparing combinations of maximum values of said estimated residual vibration amplitudes and said root mean squares of said estimated residual vibration amplitudes corresponding respectively to correction plane position combinations with said desired level; and

selecting an appropriate correction plane position combination corresponding to at least one of said combinations of the maximum values and the root mean squares of said estimated residual vibration amplitudes which is below said desired level, the step of selecting said correction plane position combination includes selecting an optimum correction plane position combination corresponding to one of at least two combinations of the maximum value and the root means squares which has the minimum amplitude, so that an optimum correction mass is formed by said optimum correction plane position combination ans said correction mass; and

attaching said correction mass to said rotor.

2. A rotor balancing method according to claim 1, wherein said optimum correction plane position combination is selected manually by an operator.

3. A rotor balancing method according to claim 1, wherein said optimum correction plane position combination is selected automatically by a computer.

4. A rotor balancing method according to one of claims 2 or 3, further comprising the steps of:

comparing the estimated unbalance vibration amplitude upon an assumption that said optimum correction mass is applied to said rotor, with said desired level to judge whether the estimated unbalance vibration amplitude is lower than said desired level.

5. A rotor balancing mehtod according to claim 4, wherein, in the step of comparing the estimated unbalance, vibration amplitude is compared with said actually measured unbalance vibration amplitude and said desired level, and said optimum correction mass is determined as being the true optimum correction mass when said estimated unbalance vibration amplitude is below said desired level.

6. A rotor balancing method according to claim 5, wherein the selection of said correction plane combination is performed, based on at least one of critical speeds and rated speed of said actually measured unbalance vibration amplitude which exceeds said desired level.

7. A rotor balancing method according to claim 6, wherein said optimum correction plane position combination is selected manually by means of an operator.

8. A rotor balancing method according to claim 6, wherein said optimum correction plane position combination is selected manually by means of an operator.

9. A rotor balancing system for reducing excessive amplitude of unbalance vibration occuring in a rotor of a rotary machine comprising:

measuring means for actually measuring the unbalance vibration amplitude of said rotor;

judging means for judging whether the actually measured unbalance vibration amplitude exceeds a desired level;

first selection means for selecting, when said desired level is exceeded, at least one of a plurality of correction planes preset on said rotor, based on the actually measured unbalance vibration amplitude, said first selection means selects, when the actually measured unbalance vibration amplitude exceeds said desired level, at least one of a plurality of correction plane combinations each having at least any two of the correction planes preset on said rotor, based on the actually measured unbalance vibration amplitude;

first computing means for computing a correction mass to be added to said rotor, using one of a plurality of influence coefficients preset to respective correction planes, corresponding to said at least one selected correction plane, said first computing means computes the correction mass to be added to said rotor, using one of the influence coefficients respectively preset to said correction plane combinations, corresponding to said selected correction plane combination;

second computing means for computing, on an assumption that said correction mass is added to said rotor, estimated residual vibration amplitudes and the root means squares of said estimated residual vibration amplitudes; and

second selection means for comparing respective combinations of maximum values of said estimated residual vibration amplitudes and said root means squares of said estimated residual vibration amplitudes corresponding to the respective correction planes with said desired level, to select, as an appropriate correction plane, the correction plane corresponding to at least one of said combinations which is below said desired level, said second selection means compares with said desired level respective combinations of the maximum values of said estimated residual vibration amplitudes and the root means squares of said estimated residual vibration amplitudes respectively corresponding to correction plane position combinations to select, as an appropriate correction plane position combination, the correction plane position combination which corresponds to at least two of said combinations of the maximum value and root means squares which are below said desired level and to select, as an optimum correction plane position combination, the correction plane position combination corresponding to one of said at least two combinations of the maximum values and the root means squares which has the minimum amplitude, said second selection means includes a first display device which displays the respective combinations of the maximum values of said estimated residual vibration amplitudes and said root means squares of said estimated resilient vibration amplitudes corresponding respectively to said correction plane position combinations together with said desired level, said optimum correction plane position combination being visually selected among said combinations of the maximum values and the root means squares which are displayed on said first display device.

10. A rotor balancing system for reducing excessive amplitude of unbalance vibration occuring in a rotor of a rotary machine comprising:

measuring means for actually measuring the unbalance vibration amplitude of said rotor;

judging means for judging whether the actually measured unbalance vibration amplitude exceeds a desired level;

first selection means for selecting, when said desired level is exceeded, at least one of a plurality of correction planes preset on said rotor, based on the actually measured unbalance vibration amplitude, said first selection means selects, when the actually measured unbalance vibration amplitude exceeds said desired level, at least one of a plurality of correction plane combinations each having at least any two of the correction planes preset on said rotor, based on the actually measured unbalance vibration amplitude;

first computing means for computing a correction mass to be added to said rotor, using one of a plurality of influence coefficients preset to respective correction planes, corresponding to said at least one selected correction plane, said first computing means computes the correction mass to be added to said rotor, using one of the influence coefficients respectively preset to said correction plane combinations, corresponding to said selected correction plane combination;

second computing means for computing, on an assumption that said correction mass is added to said rotor, estimated residual vibration amplitudes and the root means squares of said estimated residual vibration amplitudes; and

second selection means for comparing respective combinations of maximum values of said estimated residual vibration amplitudes and said root means squares of said estimated residual vibration amplitudes corresponding to the respective correction planes with said desired level, to select, as an appropriate correction plane, the correction plane corresponding to at least one of said combinations which is below said desired level, said second selection means compares with said desired level respective combinations of the maximum values of said estimated residual vibration amplitudes and the root means squares of said estimated residual vibration amplitudes respectively corresponding to correction plane position combinations to select, as an appropriate correction plane position combination, the correction plane position combination which corresponds to at least two of said combinations of the maximum value and root means squares which are below said desired level and to select, as an optimum correction plane position combination, the correction plane position combination corresponding to one of said at least two combinations of the maximum values and the root means squares which has the minimum amplitude, said second selection means includes a computer which automatically selects said optimum correction plane position combination among the respective combinations of the maximum values of said estimated residual vibration amplitudes and the root means square of the estimated residual vibration amplitudes, based on a condition that said optimum correction plane position combination is below said desired level and has the smallest amplitude.

11. A rotor balancing system according to claim 9 or 10, wherein said first selection means selects said correction plane combination, based on at least one of critical speeds and rated speed of said actually measured unbalance amplitude which exceeds said desired level.

12. A rotor balancing system according to claim 11, further comprising:

deciding means for comparing said estimated unbalance vibration amplitude with said actually measured unbalance vibration amplitude and said desired level to decide a combination of said optimum correction plane position combination and said optimum correction mass when said estimated residual unbalance vibration amplitude is below said desired level.

13. A rotor balancing system according to claim 12, wherein said first selection means includes a second display device for displaying said actually measured unbalance vibration amplitudes and said desired level, said correction plane combination being selected by a visual check of an operator, based on said at least one of said critical speeds and rated speed of said actually measured unblance vibration amplitude displayed on said second display device, which exceeds said desired level.

14. A rotor balancing system according to claim 12, wherein said first selection means includes a computer which selects said correction plane combination based on a condition as to which of said critical speeds and rated speed of said actually measured unbalance vibration amplitude exceeds said desired level.

15. A rotor balance system according to claim 14, further comprising:

a memory device for storing the influence coefficients respectively preset to said correction plane combinations; and

said first and second selection means and said first and second computing means being constituted by a single computer unit.

16. A rotor balancing system according to claim 14, wherein said means for actually measuring the unbalance vibration amplitude of said rotor includes:

rotational speed detecting means for detecting the rotational speed of said rotor to produce a signal;

a vibration detector for detecting the vibration amplitude of said rotor to produce a signal; and

a vibration analyzer operative in response to the signal from said rotational speed detector and the signal from said vibration detector, to produce an unbalance vibration component signal synchronous with the rotational speed of said rotor;

said judging means judging whether said actually measured unbalance vibration of said rotor exceeds said desired level, based on said unbalance vibration component signal.