Reciprocating compressor and methods for monitoring operation of same

• US 8,807,959 B2
• Filed: 11/30/2010
• Issued: 08/19/2014
• Est. Priority Date: 11/30/2010
• Status: Active Grant

• Current Assignee: Baker Hughes, a GE Company, LLC (Baker Hughes Company)
• Original Assignee: General Electric Company
• Inventors: Grant, John Wesley, Howard, Brian Francis
• Primary Examiner(s): ZOLLINGER, NATHAN C
• Application Number:
  US12/955,987
• Publication Number:
  US 20120134850A1
• Time in Patent Office: 1,358 Days
• Field of Search: 417/63, 417/44.1, 731/68, 737/02, 702/54, 702/56, 702/98, 702/138, 702/1, 702/33, 702/34, 702/41, 702/43, 702/42, 702/44, 702/127, 702/140, 702/182, 340/500, 340/540, 340/679
• US Class Current: 417/63
• CPC Class Codes: F04B 2201/0802 Vibration
• CPC Class Codes: F04B 2205/03 Pressure in the compression chamber
• CPC Class Codes: F04B 39/00 Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
• CPC Class Codes: F04B 49/065 and making use of computers
• CPC Class Codes: F04B 49/10 Other safety measures
• CPC Class Codes: F04B 51/00 Testing machines, pumps, or pumping installations

Abstract

A condition monitoring system for use with a reciprocating device. The condition monitoring system includes at least one pressure sensor that is configured to sense a pressure within the reciprocating device. At least one vibration sensor is configured to sense a vibration of the reciprocating device. A protection system is communicatively coupled to the pressure sensor and the vibration sensor. The protection system is configured to calculate a stiffness value of the reciprocating device based on the sensed pressure within the reciprocating device and the sensed vibration of the reciprocating device.

Claims

1. A condition monitoring system for use with a reciprocating device, the condition monitoring system comprising:

at least one pressure sensor configured to sense a pressure within the reciprocating device;

at least one vibration sensor configured to sense a vibration of the reciprocating device; and

a protection system communicatively coupled to the pressure sensor and the vibration sensor, the protection system configured to calculate a stiffness value of the reciprocating device based on the sensed pressure within the reciprocating device and the sensed vibration of the reciprocating device.

2. The condition monitoring system in accordance with claim 1, further comprising a user computing device communicatively coupled to the protection system, the protection system configured to transmit a notification signal to the user computing device after determining that the calculated stiffness value is different than a predefined reciprocating device stiffness value.

3. The condition monitoring system in accordance with claim 1, wherein the protection system is configured to:

calculate a gas force based at least in part on the sensed pressure within the reciprocating device;

calculate a displacement value of the reciprocating device based at least in part on the sensed vibration of the reciprocating device; and

calculate the stiffness value based at least in part on the calculated gas force divided by the calculated displacement value.

4. The condition monitoring system in accordance with claim 3, wherein the reciprocating device comprises a crank shaft, the condition monitoring system further comprises at least one position sensor configured to sense a position of the crank shaft, the protection system communicatively coupled to the position sensor and configured to calculate a crank angle of the crank shaft based at least in part on the sensed position.

5. The condition monitoring system in accordance with claim 4, wherein the protection system is configured to:

calculate a stiffness value at a crank angle; and

transmit a notification signal to a user computing device after determining that the calculated stiffness value is different than a predefined stiffness value.

6. The condition monitoring system in accordance with claim 1, wherein the reciprocating device includes a cylinder assembly coupled to a frame, the condition monitoring system further comprises:

a first vibration sensor coupled to the cylinder assembly and configured to sense a vibration of the reciprocating device; and

a second vibration sensor coupled to the frame and configured to sense a vibration of the frame, the protection system configured to calculate a displacement value of the cylinder assembly based at least in part on the sensed vibration of the reciprocating device and the sensed vibration of the frame.

7. The condition monitoring system in accordance with claim 4, wherein the protection system is configured to:

calculate an array of gas force values at a plurality of calculated crank angles;

calculate an array of displacement values at the plurality of calculated crank angles; and

calculate an array of stiffness values within a predefined range of calculated crank angles based at least in part on the calculated array of gas force values divided by the calculated array of displacement values.

8. The condition monitoring system in accordance with claim 7, wherein the protection system is configured to:

calculate a stiffness spectra output based at least in part on the calculated array of gas force values divided by the calculated array of displacement values; and

transmit a notification signal to a user computing device after determining that the calculated stiffness spectra output is different than a predefined spectra stiffness output.

9. A reciprocating compressor comprising:

a compressor frame;

a crank shaft positioned within the compressor frame;

a cylinder assembly coupled to the compressor frame and to the crank shaft, the cylinder assembly extending outwardly from the compressor frame along a centerline axis;

at least one pressure sensor configured to sense a pressure within the reciprocating compressor;

at least one vibration sensor configured to sense a vibration of the reciprocating compressor; and

a protection system communicatively coupled to the pressure sensor and the vibration sensor, the protection system configured to calculate a stiffness value of the reciprocating compressor based on the sensed pressure within the reciprocating compressor and the sensed vibration of the reciprocating compressor.

10. The reciprocating compressor in accordance with claim 9, further comprising a user computing device communicatively coupled to the protection system, the protection system configured to transmit a notification signal to the user computing device after determining that the calculated stiffness value is different than a predefined reciprocating compressor stiffness value.

11. The reciprocating compressor in accordance with claim 9, wherein the protection system is configured to:

calculate a gas force based at least in part on the sensed pressure within the cylinder assembly;

calculate a displacement value of the reciprocating compressor based at least in part on the sensed vibration of the reciprocating compressor; and

calculate the stiffness value based at least in part on the calculated gas force divided by the calculated displacement value.

12. The reciprocating compressor in accordance with claim 11, further comprising at least one position sensor configured to sense a position of the crank shaft, the protection system communicatively coupled to the position sensor and configured to calculate a crank angle of the crank shaft based at least in part on the sensed position.

13. The reciprocating compressor in accordance with claim 12, wherein the protection system is configured to:

calculate a stiffness value at a crank angle; and

transmit a notification signal to a user computing device after determining that the calculated stiffness value is different than a predefined stiffness value.

14. The reciprocating compressor in accordance with claim 9, further comprising:

a first vibration sensor coupled to the cylinder assembly and configured to sense a vibration of the reciprocating compressor; and

a second vibration sensor coupled to the compressor frame and configured to sense a vibration of the compressor frame, the protection system configured to calculate a displacement value of the cylinder assembly based at least in part on the sensed vibration of the reciprocating compressor and the sensed vibration of the compressor frame.

15. The reciprocating compressor in accordance with claim 12, wherein the protection system is configured to:

calculate an array of gas force values;

calculate an array of displacement values;

calculate a stiffness spectra output based at least in part on the calculated array of gas force values divided by the calculated array of displacement values; and

transmit a notification signal to a user computing device after determining that the calculated stiffness spectra output is different than a predefined spectra stiffness output.

16. A method for monitoring a condition of a reciprocating compressor, the reciprocating compressor includes a cylinder assembly coupled to a frame, the method comprising:

transmitting, from a first sensor to a protection system, a first monitoring signal indicative of a pressure within the cylinder assembly of the reciprocating compressor;

transmitting, from at least a second sensor to the protection system, at least a second monitoring signal indicative of a vibration of the cylinder assembly; and

calculating, by the protection system, a stiffness value of the reciprocating compressor based at least in part on the first signal and the second signal, wherein the protection system is communicatively coupled to the first and second sensors.

17. The method in accordance with claim 16, further comprising transmitting a notification signal from the protection system to a user computing device after determining that the calculated stiffness value is different than a predefined stiffness value.

18. The method in accordance with claim 16, further comprising:

calculating a gas force value based at least in part on the sensed pressure within the cylinder assembly;

calculating a displacement value of the cylinder assembly based at least in part on the sensed vibration of the cylinder assembly; and

calculating a stiffness value of the reciprocating compressor based at least in part on the calculated gas force and the calculated displacement of the cylinder assembly.

19. The method in accordance with claim 16, wherein the reciprocating compressor includes a crank shaft rotatably coupled to a piston assembly, the method further comprising:

transmitting, from a third sensor to the protection system, a third monitoring signal indicative of a rotational position of the crank shaft;

calculating, by the protection system, a crank angle of the crank shaft based at least in part on the third monitoring signal;

calculating a first stiffness value at a calculated first crank angle in a first operating cycle;

calculating a second stiffness value at the calculated first crank angle in a second operating cycle;

transmitting a first notification signal from the protection system to a user computing device after determining that the calculated first stiffness value is different than the calculated second stiffness value; and

transmit a second notification signal from the protection system to the user computing device after determining that the calculated second stiffness value is less than a predefined stiffness value.

20. The method in accordance with claim 18, further comprising:

calculating a frequency of gas force values based at least in part on the calculated gas force value;

calculating a frequency of displacement values based at least in part on the calculated displacement value;

calculating a stiffness spectra output based at least in part on the calculated frequency of gas force values divided by the calculated frequency of displacement values; and

transmitting a notification signal from the protection system to the user computing device after determining that the calculated stiffness spectra output is different than a predefined spectra stiffness output.