Corrosion sensor for internal structure of machine

Patent metadata

Field	Value
Publication number	US-9429510-B2
Application number	US-201414543989-A
Country	US
Kind code	B2
Filing date	Nov 18, 2014
Priority date	Nov 18, 2014
Publication date	Aug 30, 2016
Grant date	Aug 30, 2016

Abstract

A corrosion sensor for an internal structure of a machine is provided. The corrosion sensor may include a test cap having at least one of a material and a geometry configured to fail faster than a material of the internal structure due to a corrosive influence. A mount secures the test cap in position in an opening in a portion of the machine that defines an operational environment. A chamber is adjacent the test cap and in at least one of the test cap and the mount. A failure in the test cap creates an environmental change in the chamber that indicates exceeding a corrosion threshold and can be sensed by, for example, a temperature or pressure change.

First claim

What is claimed is:

1. A corrosion sensor and gas turbine compressor system, the system comprising:
a gas turbine compressor with an internal structure;
a test cap having at least one of a material and a geometry configured to fail faster than a material of the internal structure due to a corrosive influence;
a portion of the gas turbine compressor defining an opening and exposed to an operational environment at least similar to that of the internal structure;
a mount to secure the test cap in position in the opening in the portion of the gas turbine compressor whereby the test cap is exposed to an operational environment at least similar to that of the internal structure; and
a chamber adjacent the test cap and in at least one of the test cap and the mount,
wherein an environmental change in the chamber caused by a failure of the test cap indicates exceeding a corrosion threshold.

2. The system of claim 1 , wherein the test cap includes a first portion, a second portion, and a planar surface exposed to the operational environment, wherein the first portion has a thickness greater than the second portion.

3. The system of claim 2 , wherein the second portion surrounds the first portion.

4. The system of claim 1 , wherein the at least one of material and geometry is selected to create a predetermined time interval between failure of the test cap and failure of the internal structure based on an expected corrosion influence.

5. The system of claim 1 , wherein the test cap includes a planar surface that is co-planar with an internal surface of the portion of the gas turbine compressor that defines the operational environment.

6. The system of claim 1 , wherein the test cap and the mount are coupled by brazing.

7. The system of claim 1 , further comprising an environmental change sensor configured to identify the environmental change indicative of exceeding the corrosion threshold.

8. The system of claim 7 , wherein the environmental change sensor includes a thermocouple operably coupled with the chamber, wherein the environmental change includes a change in temperature measured by the thermocouple.

9. The system of claim 7 , wherein the environmental change sensor includes a pressure sensor operably coupled with the chamber, wherein the environmental change includes a change in pressure measured by the pressure sensor.

10. The system of claim 7 , wherein the environmental change sensor includes an electric gauge that measures a selected electrical parameter across the test cap, wherein the environmental change includes a change in the selected electrical parameter.

11. The system of claim 1 , wherein the test cap has a dimension greater than a dimension of the opening in the portion of the gas turbine compressor to create an interference fit such that the test cap is exposed to a compression stress greater than the internal structure.

12. The system of claim 1 , wherein the portion of the gas turbine compressor includes a threaded portion within the opening and the mount is threadably coupled in the opening.

13. A corrosion sensor and gas turbine compressor system, the system comprising:
a gas turbine compressor with an internal structure;
a test cap having at least one of a material and a geometry configured to fail faster than a material of the internal structure due to a corrosive influence;
a portion of the gas turbine compressor exposed to an operational environment at least similar to that of the internal structure and defining an opening;
a mount coupled to the test cap to threadably secure the test cap in position in the opening in the portion of the gas turbine compressor exposed to an operational environment at least similar to that of the internal structure; and
a chamber adjacent the test cap and in at least one of the test cap and the mount,
wherein an environmental change in the chamber caused by a failure of the test cap indicates exceeding a corrosion threshold,
wherein the mount positions the test cap in the position such that the test cap is exposed to a stress greater than the internal structure.

14. The system of claim 13 , wherein the test cap includes a first portion and a second portion, wherein the first portion has a thickness greater than the second portion and the second portion surrounds the first portion.

15. The system of claim 13 , wherein the test cap includes a planar surface exposed to the operational environment, and the planar surface is co-planar with an internal surface of the portion of the gas turbine compressor that defines the operational environment.

16. The system of claim 13 , further comprising an environmental change sensor configured to identify the environmental change indicative of exceeding the corrosion threshold.

17. The system of claim 16 , wherein the environmental change sensor includes a thermocouple operably coupled with the chamber, wherein the environmental change includes a change in temperature measured by the thermocouple.

18. The system of claim 16 , wherein the environmental change sensor includes a pressure sensor operably coupled with the chamber, wherein the environmental change includes a change in pressure measured by the pressure sensor.

19. The system of claim 16 , wherein the environmental change sensor includes an electric gauge that measures a selected electrical parameter across the test cap, wherein the environmental change includes a change in the selected electrical parameter.

Assignees

• Gen Electric

Inventors

• Belsom Keith Cletus
• Dimascio Paul Stephen

Classifications

• G01N17/04 Primary

  Corrosion probes · CPC title

• G01L7/00

  Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements ({G01L11/004 takes precedence;} transmitting or indicating the displacement of mechanical pressure-sensitive elements by electric {, e.g., photoelectric} or magnetic means G01L9/00; measuring differences of two or more pressure values G01L13/00; measuring two or more pressure values simultaneously G01L15/00) · CPC title

• G01N27/00

  Investigating or analysing materials by the use of electric, electrochemical, or magnetic means (G01N3/00 – G01N25/00 take precedence; measurement or testing of electric or magnetic variables or of electric or magnetic properties of materials G01R) · CPC title

• G01N25/00

  Investigating or analyzing materials by the use of thermal means (G01N3/00 - G01N23/00 take precedence) · CPC title