Method and apparatus for the detection of reciprocating machine faults and failures

• US 5,592,386 A
• Filed: 07/07/1995
• Issued: 01/07/1997
• Est. Priority Date: 10/23/1992
• Status: Expired due to Fees

• Current Assignee: Noranda, Inc. (Glencore Plc)
• Original Assignee: Noranda, Inc. (Glencore Plc)
• Inventors: Gaultier, Philippe
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): LOUIS JACQUES, JACQUES H
• Application Number:
  US08/499,649
• Time in Patent Office: 550 Days
• Field of Search: 74/573 R, 74/604, 123/192.2, 123/436, 123/339.14, 123/192.2, 123/192.1, 123/416-417, 73/116, 73/117.3, 73/112, 73/115, 73/862, 73/119 R, 464/180, 364/431.08, 364/431.01, 364/431.04, 364/431.07, 364/550, 364/431.03, 364/551.01, 364/431.02
• US Class Current: 701/99
• CPC Class Codes: F02D 2200/1015 Engines misfires
• CPC Class Codes: G01M 15/046 by monitoring revolutions for detecting misfire G01M15/11
• CPC Class Codes: Y10T 74/2184 Vibration dampers

Abstract

In a method and apparatus for detection of reciprocating machine faults and failures, data representing velocity variation waveforms of a reciprocating machine having a plurality of cylinders is acquired. The acquired data is transformed using a computer to produce torque waveforms corresponding to the acquired velocity variation waveforms. An optimization algorithm is used to obtain a number of parameters corresponding to the number of cylinders of the machine for both compression and expansion cycles of the machine in an independent manner and for each cylinder. The optimized parameters and the transformed torque waveforms are then presented to the user to identify each cylinder'"'"'s condition.

Claims

1. A method for detection of reciprocating machine faults and failures, comprising the steps of:

a) acquiring data representing velocity variation waveforms of a reciprocating machine having a plurality of cylinders;

b) transforming said acquired data using a computer to produce torque waveforms corresponding to the acquired velocity variation waveforms;

c) using a model-based optimization algorithm to obtain;

(i) a coefficient corresponding to the compression cycle for each cylinder, and

(ii) a coefficient corresponding to the expansion cycle for each cylinder, wherein the coefficient corresponding to the expansion cycle is derived independently from the coefficient corresponding to the compression cycle;

d) presenting the compression coefficient, the expansion coefficient, and the transformed torque waveforms to a user to distinguish between compression faults and expansion faults for each cylinder; and

e) determining a reciprocating machine imbalance by detecting at least one of the compression fault and the expansion fault.

2. A method as defined in claim 1, wherein the data is filtered to remove systematic errors generated during data acquisition.

3. A method as defined in claim 1, wherein the coefficients are presented in a graphical format for interpretation by the user.

4. A method as defined in claim 1, wherein the torque waveform and the optimization coefficients for individual cylinders are presented for interpretation by the user.

5. A method according to claim 1, wherein the step of using a model-based optimization algorithm includes the step of using an algorithm to derive the compression cycle coefficient and the expansion cycle coefficient from torque values.

6. A method according to claim 1, wherein said optimization algorithm includes parameters corresponding to the mass of the reciprocating parts.

7. A method according to claim 1, wherein the sum of compression and expansion optimization coefficients for each cylinder are presented to the user.

8. A method according to claim 1, wherein said optimization algorithm is independent of engine type and number of cylinders.

9. A method according to claim 1, wherein the algorithm is optimized by running a plurality of iterations.

10. A method according to claim 1, wherein said step of using an optimization algorithm includes the step of iterating f_i^c and f_i '"'"' in the following equation to optimize ε

;

##EQU8## where ε

comprises a near-defined error constant between theoretical and test engine torque waveforms;

τ

(θ

) comprises torque from all cylinders superimposed;

τ

^c (θ

_i) comprises torque due to compression forces for each cylinder i;

f_i^c comprises the compression coefficient for each cylinder i;

τ

'"'"'(θ

_i) comprises torque due to expansion forces for each cylinder i;

f_i '"'"' comprises the expansion coefficient for each cylinder i; and

n comprises the cylinder number.

11. A method for detection of reciprocating machine faults and failures, comprising the steps of:

acquiring data representing velocity variation waveforms of a reciprocating machine having a plurality of cylinders;

transforming said acquired data using a computer to produce torque waveforms corresponding to the acquired velocity variation waveforms;

using a model-based optimization algorithm to obtain a compression coefficient for each cylinder and an expansion coefficient for each cylinder by iterating f_i^c and f_i '"'"' in the following equation to optimize ε

;

##EQU9## where ε

comprises a near-defined error constant between theoretical and test engine torque waveforms;

τ

(θ

) comprises torque from all cylinders superimposed;

τ

^c (θ

_i) comprises torque due to compression forces for each cylinder i;

f_i^c comprises the compression coefficient for each cylinder i;

τ

'"'"'(θ

_i) comprises torque due to expansion forces for each cylinder i;

f_i '"'"' comprises the expansion coefficient for each cylinder i; and

n comprises the cylinder number;

determining a reciprocating machine imbalance by detecting at least one of a compression fault and an expansion fault utilizing said compression coefficient and said expansion coefficient.

12. A method according to claim 11, wherein said optimization algorithm includes parameters corresponding to the mass of the reciprocating parts.

13. A method according to claim 11, wherein said optimization algorithm is independent of engine type and number of cylinders.

14. A method according to claim 11, further comprising the step of presenting in graphical form the compression coefficient for each cylinder and the expansion coefficient for each cylinder.

15. A system for detection of reciprocating machine faults and failures, comprising:

means for acquiring data representing velocity variation waveforms of a reciprocating machine having a plurality of cylinders; and

processing means for (i) transforming said acquired data to produce torque waveforms corresponding to the acquired velocity variation waveforms, (ii) using a model-based optimization algorithm to obtain;

a coefficient corresponding to the compression cycle for each cylinder, and

a coefficient corresponding to the expansion cycle for each cylinder, the coefficient corresponding to the expansion cycle being derived independently from the coefficient corresponding to the compression cycle, (iii) outputting a first signal corresponding to the compression coefficient, and a second signal corresponding to the expansion coefficient.

16. A system according to claim 15, wherein said processing means simultaneously displays the compression coefficient and the expansion coefficient in graphical form.

17. A system according to claim 15, wherein said processing means obtains the compression coefficient and the expansion coefficient according to the following equation:

##EQU10## where ε

comprises a near-defined error constant between theoretical and test engine torque waveforms;

τ

(θ

) comprises torque from all cylinders superimposed;

τ

^c (θ

_i) comprises torque due to compression forces for each cylinder i;

f_i^c comprises the compression coefficient for each cylinder i;

τ

'"'"'(θ

_i) comprises torque due to expansion forces for each cylinder i;

f_i '"'"' comprises the expansion coefficient for each cylinder i; and

n comprises the cylinder number.

18. A system according to claim 15, wherein said processing means uses the optimization algorithm by incorporating therein parameters corresponding to the mass of the reciprocating parts.

19. A system according to claim 15, wherein said processing means processes the optimization algorithm a plurality of times for each cylinder to optimize the compression coefficient and the expansion coefficient.

20. A system according to claim 15, wherein said processing means uses an optimization algorithm which is independent of engine type and number of cylinders.