Wear monitoring system with embedded conductors

• US 7,270,890 B2
• Filed: 12/20/2004
• Issued: 09/18/2007
• Est. Priority Date: 09/23/2002
• Status: Expired due to Fees

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Power Generation, Inc.
• Inventors: Subramanian, Ramesh, Sabol, Stephen M.
• Primary Examiner(s): McNeil; Jennifer
• Assistant Examiner(s): Speer; Timothy M.
• Application Number:
  US11/018,816
• Publication Number:
  US 20050158511A1
• Time in Patent Office: 1,002 Days
• Field of Search: None
• US Class Current: 428/632
• CPC Class Codes: C23C 24/10 with intermediate formation of a liquid phase in the layer
• CPC Class Codes: C23C 4/18 After-treatment
• CPC Class Codes: F16D 66/02 Apparatus for indicating wear
• CPC Class Codes: F23M 11/00 Safety arrangements
• CPC Class Codes: F23M 5/00 Casings; Linings; Walls
• CPC Class Codes: F23R 3/007 constructed mainly of ceramic components
• CPC Class Codes: G01N 3/56 Investigating resistance to wear or abrasion
• CPC Class Codes: Y10T 428/12611 Oxide-containing component
• CPC Class Codes: Y10T 428/24273 including aperture

Abstract

Aspects of the invention relate to a system for monitoring the wear of a component. A conductor can be embedded in the component at a depth from a surface of the component. In one embodiment, the conductor can be operatively connected to a power source to form an electrical circuit. The resistance across the conductor can be measured. As the component contacts a second component, the component can begin to wear. Once the wear progresses to the conductor, changes in the measured resistance can result. Thus, an operator can be alerted that the component has worn to a certain point and that service may be needed. Alternatively, impedance can be measured across the conductor. Because the dielectric permeability of the material surrounding the conductor can affect impedance, changes in impedance can occur as the surface material of the component is worn away.

Claims

1. A wear monitoring system comprising:

a first component having a surface;

a second component;

a first conductor embedded in the first component at a predetermined depth beneath the surface and being electrically insulated from the first component;

a power source operatively connected to provide current to the first conductor, whereby an electrical circuit is formed; and

a measurement device operatively positioned to measure an electrical value across at least a portion of the first conductor,

wherein the second component contacts the surface of the first component such that at least the surface of the first component wears, whereby a user can monitor the measurement device for changes in the measured value indicating that the wear has progressed at least to the predetermined depth, wherein the current flows through the first conductor prior to the wear progressing to the predetermined depth.

2. The system of claim 1 wherein the first and second components are gas turbine engine components.

3. The system of claim 1 wherein the electrical value is one of resistance, current, voltage and impedance.

4. The system of claim 1 further including:

a second conductor embedded in the first component at a predetermined depth beneath the surface, wherein the second conductor is operatively connected to receive current from the power source, and wherein the measurement device is operatively positioned to measure the value across at least a portion of the second conductor.

5. The system of claim 4 wherein the first and second conductors we electrically insulated from each other and are separately operatively connected to the power source, whereby two isolated circuits are formed.

6. The system of claim 4 wherein the first and second conductors are provided in the first component at substantially the same depth beneath the surface of the first component.

7. The system of claim 4 wherein the first and second conductors are electrically connected in parallel.

8. The system of claim 4 wherein the first and second conductors are provided in the first component at different depths beneath the surface of the first component.

9. The system of claim 8 wherein the first conductor and the second conductor provide at least partially overlapping areas of coverage about the first component.

10. The system of claim 1 wherein the first component includes a base material with at least one layer of a coating thereon, wherein the first conductor is embedded within the coating.

11. A wear monitoring system comprising:

a first component having a fast surface;

a second component having a second surface, wherein at least a portion of the second surface of the second component is conductive;

a first conductor embedded in the first component at a predetermined depth beneath the first surface;

a second conductor embedded in the first component at another predetermined depth beneath the first surface, and

a power source operatively connected to the first conductor and to the conductive surface of the second component, wherein an initially open circuit is formed,

the second surface and the first surface being in contact such that at least the fast surface wears, wherein, when the first surface is sufficiently worn such that the second surface contacts the first conductor, the circuit is completed, whereby the completion of the circuit can alert a user that the wear has progressed to at least the predetermined depth,

wherein the second conductor is operatively connected to receive current from the power source such that an initially open circuit is formed,

wherein when the first surface is sufficiently worn such that the second surface contacts the second conductor, the circuit is completed, whereby the completion of the circuit can alert a user that the wear has progressed to at least the another predetermined depth,

wherein the first and second conductors are electrically insulated from each other and are separately operatively connected to the power source, whereby two isolated initially open circuits are formed, and

wherein the first and second conductors are provided in the first component at different depths beneath the first surface of the first component.

12. The system of claim 11 further including a measurement device operatively positioned to measure at least one of resistance, current, voltage and impedance across at least a portion of the first conductor and the conductive surface of the second component, whereby changes in the measured resistance, current, voltage and impedance indicate that a predetermined amount of wear has occurred.

13. The system of claim 11 wherein the first component is a gas turbine engine component.

14. The system of claim 11 wherein the first conductor and the second conductor provide at least partially overlapping areas of coverage about the first component.

15. The system of claim 11 wherein the first and second conductors are electrically connected in parallel.

16. The system of claim 11 wherein the first component includes a base material with at least one layer of a coating thereon, wherein the first conductor is embedded within the coating.