Rotating machinery monitoring system

• US 9,840,935 B2
• Filed: 03/19/2015
• Issued: 12/12/2017
• Est. Priority Date: 03/31/2014
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Khibnik, Alexander I.
• Primary Examiner(s): Tran, Binh Q
• Application Number:
  US14/662,721
• Publication Number:
  US 20150345325A1
• Time in Patent Office: 999 Days
• Field of Search: 60772, 60773, 60800, 60803, 60 3934, 60 3935, 60804, 60722, 60725, 60418, 60448, 60449, 60700, 60702, 60706, 60712
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: G01M 15/14 Testing gas-turbine engines or jet-propulsion engines

Abstract

A method for monitoring rotating component includes receiving a continuous waveform sensor signal from a sensor apparatus, retaining the continuous waveform in a memory, and isolating at least one characteristic and/or at least one period of the waveform. The isolated characteristic and/or period is analyzed thereby determining the presence of a waveform anomaly.

Claims

1. A method for monitoring rotating component comprising:

an electronic control unit (ECU) receiving a sensor signal from a sensor apparatus, wherein the sensor signal comprises a continuous waveform representative of a sensor output;

retaining the continuous waveform in a memory of the ECU; and

isolating at least one of at least one characteristic and at least one period of the waveform and analyzing the at least one of at least one characteristic and at least one period and thereby determining an occurrence of a blade strike event using the ECU by determining a similarity measure between a reference period and an isolated period of the continuous waveform, and determining if the similarity measure exceeds a threshold, the similarity measure including at least one of a vector-time domain distance, a spectral distance, and a correlation distance.

2. The method of claim 1, wherein isolating at least one of at least one characteristic and at least one period of the waveform and analyzing the at least one of at least one characteristic and at least one period and thereby determining the occurrence of the blade strike event comprises comparing an isolated period from the continuous waveform against a reference period and determining the presence of the blade strike event based on the comparison.

3. A method for monitoring rotor blades comprising:

an electronic control unit (ECU) receiving a sensor signal from a sensor apparatus, wherein the sensor signal comprises a continuous waveform representative of a sensor output;

comparing a period of the received sensor signal to a reference period using the ECU and determining a similarity measure between the received period of the sensor signal and the reference period, the similarity measure including at least one of a vector-time domain distance, a spectral distance, and a correlation distance; and

determining a presence of a blade strike based on a difference between the reference period and the received waveform.

4. The method of claim 3, further comprising isolating a period corresponding to a single blade of a sensed rotor and generating a correlated set of sequential periods corresponding to the single blade.

5. The method of claim 3, wherein the reference period is one of a static period stored in a memory, a predicted period derived from one or more previous rotations of a corresponding rotor, a predicted period derived from one or more future periods of the corresponding rotor, and a predicted period derived from a combination of previous periods of the corresponding rotor and future periods of the corresponding rotor.

6. The method of claim 3, wherein the received period is a digitized sensor output.

7. The method of claim 3, wherein the received sensor signal is an analog sensor output.

8. The method of claim 3, wherein determining a presence of a blade strike based on a difference between the reference period and the received signal comprises determining that the similarity measure exceeds a threshold.

9. The method of claim 8, wherein the threshold is a dynamic threshold determined from derived characteristics of prior similarity measures.

10. The method of claim 3, further comprising validating the received sensor signal by comparing at least one characteristic of the received sensor signal against an expected value of the at least one characteristic.

11. The method of claim 3, wherein comparing a period of the received sensor signal to a reference period and determining a presence of a blade strike based on a difference between the reference period and the received signal are performed in real time.

12. A gas turbine engine comprising:

a compressor section;

a combustor section fluidly connected to the compressor section;

a turbine section fluidly connected to the combustor section;

wherein each of the compressor section and the turbine section includes a plurality of rotors, each rotor having a plurality of radially outward protruding rotor blades;

an engine case disposed about the compressor section, the combustor and the turbine section;

at least one sensing system disposed within sensing distance of a rotor; and

a controller connected to the sensing system and operable to receive a full waveform output from the sensing system;

wherein the controller further includes a memory operable to cause the controller and the sensing system to perform the steps of

receiving a sensor signal from the sensing system, wherein the sensor signal comprises a continuous waveform representative of a sensor output;

comparing the received sensor signal to at least a reference period using the controller and determining a similarity measure between the received period of the sensor signal and the reference period, the similarity measure including at least one of a vector-time domain distance, a spectral distance, and a correlation distance; and

determining a presence of a blade strike event based on a difference between the reference period and the received signal.

13. A gas turbine engine comprising:

a compressor section;

a combustor section fluidly connected to the compressor section;

a turbine section fluidly connected to the combustor section;

wherein each of the compressor section and the turbine section includes a plurality of rotors, each rotor having a plurality of radially outward protruding rotor blades;

an engine case disposed about the compressor section, the combustor and the turbine section;

at least one sensing system disposed within sensing distance of a rotor; and

a controller connected to the sensing system and operable to receive a full waveform output from the sensing system;

wherein the controller further includes a memory operable to cause the controller and the sensing system to perform the steps of

receiving a sensor signal from the sensing system, wherein the sensor signal comprises a continuous waveform representative of a sensor output;

comparing the received sensor signal to at least a reference period, wherein the reference period is one of a static period stored in a memory, a received period from a previous rotation of a corresponding rotor, a combination of a received period from at least two previous rotations of a corresponding rotor, a received period from a future rotation of the corresponding rotor, a combination of received periods from at least two future rotations of the corresponding rotor, and a combination of a received period from at least one previous rotation of the corresponding rotor and a received period from at least one future rotation of the corresponding rotor; and

determining a presence of a blade strike event based on a difference between the reference period and the received signal.

14. The gas turbine engine of claim 13, wherein the at least one sensing system comprises a plurality of sensors, and wherein each of the sensors is supported via the case within sensing distance of a corresponding rotor.