System and method for online monitoring of corrosion of gas turbine components

• US 8,475,110 B2
• Filed: 07/30/2009
• Issued: 07/02/2013
• Est. Priority Date: 07/30/2009
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Hefner, Rebecca, Czapiewski, Jeff P.
• Primary Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US12/512,618
• Publication Number:
  US 20110027063A1
• Time in Patent Office: 1,433 Days
• Field of Search: 415/1, 415/118, 415/116, 416/1, 416/61, 134/18, 134/22.1, 134/22.18, 134/2, 134/3, 134/34, 324/700, 204/404, 205/775.5, 205/776, 205/776.5, 205/777
• US Class Current: 415/1
• CPC Class Codes: G01N 17/02 Electrochemical measuring systems for weathering, corrosion or corrosion-protection measurement

Abstract

A system and method capable of performing online corrosion monitoring of a component installed in a gas turbine. A sensing device is located so that electrodes thereof are exposed to an operating environment within the gas turbine section containing the component. The electrodes are formed of a material so that the component and electrodes similarly respond to corrosive agents within the gas turbine section. The electrodes are electrically insulated from each other and each electrode is operable as an anodic electrode or a cathodic electrode, depending on the extent of corrosion thereat, so that each electrode has an electrical potential value, voltages exist across the electrodes, electric currents flow between the electrodes, and the electrical potential/current values correspond to corrosion behaviors at the anodic electrodes. During gas turbine operation, output signals are obtained from the sensing device and indications are provided as to when certain maintenance operations should be performed on the gas turbine.

Claims

1. A method for online monitoring of corrosion of a component installed in a section of a gas turbine, the method comprising:

locating a multi-electrode array sensing device on the gas turbine so that the sensing device is mounted in a wall of a second component of the gas turbine that is spaced apart from the first component, a face of the sensing device is substantially flush with a surface of the second component, and electrodes at the face of the sensing device are exposed to an operating environment within the section of the gas turbine, the electrodes being formed of an electrode material and the first component being formed of a component material that respond to at least one corrosive agent within the section of the gas turbine, the electrodes being electrically insulated from each other and each electrode being operable as an anodic electrode or a cathodic electrode depending on the extent of corrosion thereat so that each electrode has an electrical potential value, voltages exist across the electrodes, an electrical current flows from each anodic electrode to at least one of the cathodic electrodes, and the electrical potential values and the electric current values correspond to corrosion behaviors at the anodic electrodes that occur in response to the electrodes being exposed to the operating environment within the section of the gas turbine engine;

operating the gas turbine and, while the gas turbine is operating, obtaining output signals from the sensing device based on the electrical potential values and the electric current values;

monitoring corrosion characteristics based on the output signals of the sensing device, a first of the corrosion characteristics being pitting rate based on the electric current values and being monitored in relation to a pitting rate limit, a second of the corrosion characteristics being a pitting depth based on the electrical potential or electric current values and being monitored in relation to a pitting depth limit; and

indicating when a wash maintenance operation should be performed on the gas turbine in response to the pitting rate exceeding the pitting rate limit, and indicating when a shutdown maintenance operation of the gas turbine should be performed in response to the pitting depth exceeding the pitting depth limit.

2. The method according to claim 1, further comprising the step of performing the wash or shutdown maintenance operation following the indicating step.

3. The method according to claim 2, wherein the maintenance operation is the shutdown maintenance operation and comprises shutdown of the gas turbine and dismantling the first component from the section of the gas turbine.

4. The method according to claim 2, wherein the maintenance operation is the wash maintenance operation and comprises online washing of the section of the gas turbine while the gas turbine is operating.

5. The method according to claim 2, wherein the maintenance operation is the shutdown maintenance operation and comprises shutdown of the gas turbine and offline washing of the section of the gas turbine.

6. The method according to claim 1, wherein the electrode and component materials are the same so that the first component and the electrodes similarly respond to the at least one corrosive agent.

7. The method according to claim 1, wherein the electrode material is more sensitive to the at least one corrosive agent than is the component material.

8. The method according to claim 1, wherein the section of the gas turbine is the compressor section and the first component is a compressor blade.

9. The method according to claim 8, wherein the sensing component is a shell wall of the compressor section and is located in a sight hole port in the shell wall.

10. The method according to claim 1, wherein the monitoring step comprises:

monitoring the pitting rate as an average corrosion rate based on an average of the electrical currents between the anodic and cathodic electrodes; and

monitoring the pitting depth as a maximum or localized corrosion rate based on a fastest corroding of the electrodes.

11. A method for online monitoring of corrosion of a compressor blade installed in a compressor section of a gas turbine, the method comprising:

locating a multi-electrode array sensing device in the compressor section so that the sensing device is mounted in a shell wall of the compressor section, the shell wall is spaced apart from the blade, a face of the sensing device is substantially flush with an inner surface of the shell wall, and electrodes disposed at the face of the sensing device are exposed to an operating environment within the compressor section of the gas turbine, the electrodes being formed of an electrode material and the blade being formed of a blade material so that the blade and the electrodes similarly respond to corrosive agents within the compressor section of the gas turbine, the electrodes being electrically insulated from each other and each electrode being operable as an anodic electrode or a cathodic electrode depending on the extent of corrosion thereat so that each electrode has an electrical potential value, voltages exist across the electrodes, an electrical current flows from each anodic electrode to at least one of the cathodic electrodes, and the electrical potential values and the electric current values correspond to corrosion behaviors at the anodic electrodes that occur in response to the electrodes being exposed to the operating environment within the section of the gas turbine engine;

operating the gas turbine and, while the gas turbine is operating, obtaining output signals from the sensing device based on the electrical potential values and the electric current values;

monitoring corrosion characteristics based on the output signals of the sensing device, a first of the corrosion characteristics being pitting rate based on the electric current values and being monitored in relation to a pitting rate limit, a second of the corrosion characteristics being a pitting depth based on the electrical potential values and being monitored in relation to a pitting depth limit;

indicating when a wash maintenance operation should be performed on the gas turbine in response to the pitting rate based on the electric current values exceeding the pitting rate limit, and indicating when a shutdown maintenance operation of the gas turbine should be performed in response to the pitting depth based on the electrical potential values exceeding the pitting depth limit; and

performing the wash or shutdown maintenance operation based on the indicating step.