IP Library Granted Patent US 11,613,999
Granted Patent B2
US 11,613,999 · App. 16/605,623 · Granted Mar 28, 2023

System and method for detecting deterioration of a control valve

Inventors: Michael Lev Tolmatsky (Des Moines, IA); Serge Staroselsky (Des Moines, IA); Paul Marvin Negley (Urbandale, IA); John Tse (West Des Moines, IA)
Assignee: Compressor Controls LLC
F01D21/14F16K37/0041F16K37/0083F16K37/0091G01M13/003F04D27/001F04D27/008
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Quick Facts
Patent No.
US 11,613,999
App. No.
16/605,623
Granted
Mar 28, 2023
Kind
B2
Abstract

Automatic testing for control valves is provided for diagnosing of actuators, including actuators not equipped with analog or discrete position transmitters. A valve controller confirms steady-state conditions for a turbo-compressor system that includes a control valve in a first position and sends, to an actuator for the control valve, a signal to initiate a partial valve stroke to move the control valve away from the first position. The valve controller receives feedback signals from sensors in the turbo-compressor system and monitors the feedback signals for a change from the steady-state conditions. When the monitoring detects a change from the steady-state conditions within a defined time period, the valve controller sends, to the actuator, a signal to return the control valve to the first position. When the monitoring does not detect a change from the steady-state conditions within the defined time period, the valve controller generates an alarm signal.

Claims (55)

1. A method of conducting a diagnostic test for a control valve, the method comprising:

confirming, by a control system, steady-state conditions for a turbo-compressor system that includes the control valve in a first position;

sending, by the control system and to an actuator for the control valve, a signal to initiate a partial valve stroke to move the control valve away from the first position;

receiving, by the control system and after sending the signal to initiate the partial valve stroke, feedback signals from sensors in the turbo-compressor system;

monitoring, by the control system, the feedback signals for a change from the steady-state conditions, wherein the monitoring comprises:

identifying a set number of different time intervals to apply,

calculating a derivative of each of the feedback signals using a first-order filter over the different time intervals, and

comparing each of the derivatives to a corresponding steady-state threshold;

sending, by the control system and to the actuator, a signal to return the control valve to the first position in response to the monitoring detecting a change from the steady-state conditions; and

generating, by the control system, an alarm signal in response to the monitoring not detecting a change from the steady-state conditions.

2. The method of claim 1 , wherein confirming the steady-state conditions includes receiving multiple feedback signals from different sources.

3. The method of claim 2 , wherein the multiple feedback signals include signals from one or more pressure sensors or one or more flow sensors, or variables calculated based on one or more of the multiple feedback signals.

4. The method of claim 3 , wherein the multiple feedback signals further include a valve position signal.

5. The method of claim 1 , wherein sending the signal to initiate the partial valve stroke includes sending instructions for a ramped valve movement, the instructions including a target valve movement distance and ramp rate.

6. The method of claim 1 , wherein sending the signal to initiate the partial valve stroke includes sending instructions for a step valve movement, the instructions including a step size for the valve movement that is less than a full valve stroke.

7. The method of claim 1 , wherein sending the signal to initiate the partial valve stroke includes sending instructions for a multi-step valve movement, the instructions including a step size, a number of steps, and a time interval between steps.

8. The method of claim 1 , wherein sending the signal to initiate the partial valve stroke includes sending instructions for one or more of a ramped valve movement or a step valve movement.

9. The method of claim 1 , wherein monitoring the feedback signals for the change from the steady-state conditions further comprises:

determining, prior to the comparing, an absolute value of each of the derivatives.

10. The method of claim 1 , wherein the different time intervals include two, three, or five different time intervals.

11. The method of claim 1 , wherein the signal to initiate the partial valve stroke to move the control valve away from the first position includes a second position with a maximum allowed distance that is configured to disrupt the steady-state conditions without disabling the turbo-compressor system.

12. The method of claim 1 , further comprising:

receiving, by the control system, a signal to initiate the diagnostic test, wherein the signal to initiate the diagnostic test is one of a manual start command or a periodic test command.

13. A valve control system, comprising:

a memory device for storing instructions; and

a processor configured to execute the instructions to:

confirm steady-state conditions for a turbo-compressor system that includes a control valve in a first position;

send, to an actuator for the control valve, a signal to initiate a partial valve stroke to move the control valve away from the first position;

receive, after sending the signal to initiate the partial valve stroke, feedback signals from sensors in the turbo-compressor system;

monitor the feedback signals for a change from the steady-state conditions,

wherein the monitoring comprises:

identifying a set number of different time intervals to apply,

calculating a derivative of each of the feedback signals using a first-order filter over the different time intervals, and

comparing each of the derivatives to a corresponding steady-state threshold;

send, to the actuator, a signal to return the control valve to the first position in response to the monitoring detecting a change from the steady-state conditions; and

generate an alarm signal in response to the monitoring not detecting a change from the steady-state conditions.

14. The valve control system of claim 13 , wherein, when comparing the derivatives, the processor is further configured to:

determine an absolute value of each of the derivatives.

15. The valve control system of claim 14 , wherein the different time intervals include two, three, or five different time intervals.

16. The valve control system of claim 13 , wherein the steady-state threshold represents a minimum amount of change required to indicate a disturbance from the steady-state conditions.

17. The valve control system of claim 13 , wherein, when confirming steady-state conditions, the processor is further configured to:

monitor the feedback signals for one or more of suction pressure, discharge pressure, or flow rate.

18. The valve control system of claim 13 , wherein the feedback signals include feedback signals from at least one sensor.

19. A non-transitory computer-readable medium containing instructions executable by at least one processor, the computer-readable medium comprising one or more instructions to:

confirm steady-state conditions for a turbo-compressor system that includes a control valve in a first position;

send, to an actuator for the control valve, a signal to initiate a partial valve stroke to move the control valve away from the first position;

receive, after sending the signal to initiate the partial valve stroke, feedback signals from sensors in the turbo-compressor system;

monitor the feedback signals for a change from the steady-state conditions, wherein the monitoring comprises:

identifying a set number of different time intervals to apply,

calculating a derivative of each of the feedback signals using a first-order filter over the different time intervals, and

comparing each of the derivatives to a corresponding steady-state threshold;

send, to the actuator, a signal to return the control valve to the first position in response to the monitoring detecting a change from the steady-state conditions; and

generate an alarm signal in response to the monitoring not detecting a change from the steady-state conditions.

20. The non-transitory computer-readable medium claim 19 , further comprising one or more instructions to:

receive a signal to initiate a diagnostic exercise, wherein confirming the steady-state conditions is performed in response to receiving the signal to initiate the diagnostic exercise.

Assignments (8)
CORRECTIVE ASSIGNMENT TO CORRECT THE PATENT NUMBER PREVIOUSLY RECORDED AT REEL: 61997 FRAME: 614. ASSIGNOR(S) HEREBY CONFIRMS THE SECURITY AGREEMENT. Recorded Nov 13, 2025
From: ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIA TRAN CORPORATION
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 073434/0453 →
RELEASE OF SECOND LIEN PATENT SECURITY INTERESTS Recorded May 30, 2025
From: ROYAL BANK OF CANADA
To: AGR INTERNATIONAL, INC.; ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIATRAN CORPORATION
Reel/Frame 071476/0346 →
PARTIAL 1ST LIEN RELEASE (REEL 061997 / FRAME 0614) Recorded Jul 4, 2023
From: UBS AG, STAMFORD BRANCH
To: COMPRESSOR CONTROLS LLC
Reel/Frame 064196/0203 →
PARTIAL 2ND LIEN RELEASE (REEL 062003 / FRAME 0566) Recorded Jul 4, 2023
From: ROYAL BANK OF CANADA
To: COMPRESSOR CONTROLS LLC
Reel/Frame 064196/0281 →
SECURITY AGREEMENT (FIRST LIEN) Recorded Nov 28, 2022
From: ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIATRAN CORPORATION
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 061997/0614 →
SECURITY AGREEMENT (SECOND LIEN) Recorded Nov 28, 2022
From: ALPHA TECHNOLOGIES SERVICES LLC; AMOT CONTROLS LLC; COMPRESSOR CONTROLS LLC; CORNELL PUMP COMPANY LLC; DYNISCO INSTRUMENTS LLC; HANSEN TECHNOLOGIES LLC; METRIX INSTRUMENT CO., L.P.; PETROLEUM ANALYZER COMPANY L.P.; ROPER HOLDINGS, LLC; ROPER INDUSTRIAL PRODUCTS INVESTMENT COMPANY LLC; ROPER PUMP COMPANY LLC; STRUERS LLC; VIATRAN CORPORATION
To: ROYL BANK OF CANADA, AS COLLATERAL AGENT
Reel/Frame 062003/0566 →
ENTITY CONVERSION Recorded Nov 3, 2022
From: COMPRESSOR CONTROLS CORPORATION
To: COMPRESSOR CONTROLS LLC
Reel/Frame 061880/0067 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 16, 2019
From: TOLMATSKY, MICHAEL LEV; STAROSELSKY, SERGE; NEGLEY, PAUL MARVIN; TSE, JOHN
To: COMPRESSOR CONTROLS CORPORATION
Reel/Frame 050734/0760 →
Continuity (2)
Provisional Application 62488188 · Apr 21, 2017
Related Publication 20200131927A1 · Apr 30, 2020