Apparatus and method for analyzing the condition and performance of turbomachines by processing signals representing rotor motion

• US 5,686,669 A
• Filed: 02/29/1996
• Issued: 11/11/1997
• Est. Priority Date: 02/29/1996
• Status: Expired due to Fees

• Current Assignee: Monitoring Technology Corporation
• Original Assignee: Monitoring Technology Corporation
• Inventors: Vosburgh, Frederick, Hernandez, Walter C.
• Primary Examiner(s): Snow, Walter E.
• Application Number:
  US08/610,085
• Time in Patent Office: 621 Days
• Field of Search: 73/657, 73/658, 73/659, 73/660, 73/661, 73/650, 340/683, 364/508
• US Class Current: 73/660
• CPC Class Codes: G01H 1/003 of rotating machines G01H1/10 takes precedence

Abstract

A method and device for processing encoder signals from turbomachines to produce frequency modulation signals representing fully isolated rotor vibrational resonances. Multi-sensor and multi-sideband group processing provides enhanced results. The method provides dramatically improved frequency resolution. Amplitude modulation and random noise effects are removed by a variety of artifact-free techniques. Signals then are completely separated into components for rotational vibration and translational vibration. Fully isolating rotational vibration unmasks previously undetectable signal components of diagnostic value. In cases of high background vibration, Wiener filtering removes the effects of exogenous vibration. By these various techniques, the present invention provides significantly enhanced diagnostic information regarding condition and performance in turbomachines.

Claims

1. A method for analyzing the condition and performance of turbomachines by processing signals representing rotor motion comprising the steps of:

a) acquiring signals from a plurality of sensing elements which detect motion of a rotor wherein at least one of said sensing elements detects rotational motion;

b) isolating signal components representing the rotational vibration and translational vibration components of said rotor motion;

c) analyzing said signal components over time to determine the condition and performance of said turbomachine.

2. The method of claim 1 wherein said at least one of said signals is an encoder signal, said encoder signals having a plurality of pulses per rotation of said rotor;

and said pulses have sideband groups comprised of carrier frequency and modulation frequency components.

3. The method of claim 2 wherein at least one of said sensing elements has a sensing axis perpendicular to the axis of rotation of said rotor.

4. The method of claim 3 wherein at least one of said sensing elements detects motion of a single encoder;

and said processing removes amplitude modulation components from said signals to produce amplitude modulation removed signals.

5. The method of claim 4 wherein said processing further includes forming combined sidebands free of amplitude modulation components for a plurality of subsignals of said signals.

6. The method of claim 5 wherein said amplitude modulation removed signals are combined to separate signal components due to rotational vibration from those due to translational vibration.

7. The method of claim 6 wherein said signals derive from two of said sensing elements having sensing fields oriented at 180 degrees relative to each other and said sensing elements lie in the plane of rotation.

8. The method of claim 7 further comprising the steps of:

d) normalizing said signals for phase and amplitude; and

e) adding said normalized signals in the frequency domain.

9. The method of claim 3 wherein said processing includes Wiener filtering to remove signal components due to extraneous vibration.

10. The method of claim 2 wherein said rotational vibration is analyzed for frequency shifts indicating cracking and erosion of rotor components.

11. The method of claim 2 wherein said motion is analyzed to determine balance, efficiency, flutter and stall of said rotor.

12. The method of claim 3 wherein two of said perpendicular sensing elements are closely adjacent and lie in a plane containing said axis of rotation such that one said element is centered over said encoder and the other sensing element lies over an edge of said encoder.

13. The method of claim 12 wherein said encoder signals are combined to determine vibration in the direction of said axis of rotation.

14. The method of claim 1 further comprising the step of communicating the results of said analyzing to an operator.

15. A device for detecting rotor vibrations and resonances in operating turbomachines comprising:

sensor means for sensing motion of a rotor at various points around the circumference of said rotor, yielding a plurality of signals;

conditioning means for conditioning and digitizing said signals to produce digital signals;

processing means for processing said digital signals to produce resampled signals, and other output;

analyzing means for determining the effects of sensor motion on said resampled signals and other output; and

interface means for communicating results of said processing and determining to an operator.

16. The device according to claim 15 wherein said sensor means comprise a sensor having a plurality of sensing elements, each sensing element having a known location and orientation relative to the other sensing elements wherein at least one of said sensor means senses encoder motion.

17. The device according to claim 16 wherein said sensing elements include at least one pair of sensor elements directable at the axis of rotation of said rotor with each sensing element having diametrically opposed sensing fields.

18. The device according to claim 17 wherein said sensor means include vibration detection means for detecting vibrations of said sensor means.

19. The device according to claim 18 wherein at least one of said sensing elements has first and second adjacent components, each component having sensing fields that lie in a plane which includes but are perpendicular to said axis of rotation;

and wherein the first said adjacent component detects a first translation along the axis of said sensing element and the second said component detects said first translation together with a second translation in the direction of said axis of rotation of the rotor.