Method and device for monitoring torsional vibrations of a rotary shaft of a turbine engine

• US 9,097,575 B2
• Filed: 11/22/2010
• Issued: 08/04/2015
• Est. Priority Date: 11/30/2009
• Status: Active Grant

• Current Assignee: Safran Aircraft Engine Company
• Original Assignee: Snecma (Safran SA)
• Inventors: Gerez, Valerio, Griffaton, Julien Christian Pascal, Jadczak, Edouard Joseph
• Primary Examiner(s): Lieu, Julie
• Application Number:
  US13/512,765
• Publication Number:
  US 20120229290A1
• Time in Patent Office: 1,716 Days
• Field of Search: None
• US Class Current: 1/1
• CPC Class Codes: G01H 1/006 of the rotor of turbo machines

Abstract

A method of monitoring twisting vibration of a rotary shaft of a turbine engine includes obtaining a vibratory acceleration signal from a sensor located on a stationary component of the turbine engine. This vibratory signal is characterized by a carrier frequency. The method also includes evaluating a frequency spectrum of the vibratory signal and searching for a pair of spectral lines of amplitudes greater than at least a first threshold. The lines are distributed in the spectrum on either side of the carrier frequency of the vibratory signal, and spaced apart therefrom by a twisting frequency of the shaft. Where appropriate, the method includes issuing a warning message.

Claims

1. A method of monitoring twisting vibration of a rotary shaft of a turbine engine, the method comprising:

obtaining a vibratory acceleration signal from an accelerometer located on a stationary component of the turbine engine, this vibratory signal being characterized by a carrier frequency;

evaluating a frequency spectrum of the vibratory signal;

searching for a pair of spectral lines of amplitudes greater than at least a first threshold, the lines being distributed in the spectrum on either side of the carrier frequency of the vibratory signal, and spaced apart therefrom by a twisting frequency of the shaft; and

where appropriate, issuing a warning message.

2. The monitoring method according to claim 1, further comprising:

evaluating an envelope signal of the vibratory signal;

evaluating a frequency spectrum of the envelope signal;

searching for at least one spectral line in the spectrum of the envelope signal that has an amplitude greater than a second threshold, and that exists at a multiple of the twisting frequency of the shaft; and

estimating a confidence level associated with the warning message as a function of the result of the searching for the at least one spectral line in the spectrum.

3. The monitoring method according to claim 2, wherein during the evaluating the envelope signal, the envelope signal is obtained from a Hilbert transform of the vibratory signal.

4. The monitoring method according to claim 1, further comprising:

searching for at least one other pair of spectral lines distributed in the spectrum of the vibratory signal on either side of the carrier frequency and spaced apart therefrom by a multiple of the twisting frequency of the shaft; and

estimating a level of severity associated with the warning message, this level of severity depending on the number of pairs of lines that are found in the searching for the at least one other pair of spectral lines and that are of amplitudes that exceed at least a third threshold.

5. A computer program including instructions for executing the steps of the monitoring method according to claim 1 when said program is executed by a computer.

6. A non-transitory computer readable recording medium having recorded thereon a computer program that, when executed by a computer, causes the computer to execute the monitoring method according to claim 1.

7. A monitoring device for monitoring twisting vibration of a rotary shaft of a turbine engine, the device comprising:

obtaining means for obtaining a vibratory acceleration signal from an accelerometer located on a stationary component of the turbine engine, the vibratory signal being characterized by a carrier frequency;

evaluation means for evaluating a frequency spectrum of the vibratory signal;

search means for searching for a pair of spectral lines of amplitudes greater than at least a first threshold, the lines being distributed in the spectrum on either side of the carrier frequency of the vibratory signal, and spaced apart therefrom by a twisting frequency of the shaft; and

issuing means for issuing a warning message activated where appropriate.

8. The monitoring device according to claim 7, further comprising:

evaluation means for evaluating an envelope signal of the vibratory signal;

evaluation means for evaluating a frequency spectrum of the envelope signal;

search means for searching for at least one spectral line in the spectrum of the envelope signal that is of an amplitude greater than a second threshold, and that is at a multiple of the twisting frequency of the shaft; and

estimator means for estimating a confidence level associated with the warning message, as a function of the result of the search.

9. The monitoring device according to claim 7, further comprising:

search means for searching for at least one other pair of spectral lines distributed in the spectrum of the vibratory signal on either side of the carrier frequency, and spaced apart therefrom by a multiple of the twisting frequency of the shaft; and

estimator means for estimating a severity level associated with the warning message, the severity level depending on the number of pairs that are found by the search means and that are of amplitudes that exceed at least a third threshold.

10. A turbine engine, comprising:

a monitoring device according to claim 7; and

an accelerometer located on a stationary component of the turbine engine and adapted to deliver a vibratory acceleration signal to the monitoring device.