Method and apparatus of monitoring temperature and strain by using fiber bragg grating (FBG) sensors

• US 20050061058A1
• Filed: 10/20/2003
• Published: 03/24/2005
• Est. Priority Date: 09/24/2003
• Status: Active Grant

• Current Assignee: Siemens AG
• Original Assignee: Siemens AG
• Inventors: Sanjana, Zal, Bosselmann, Thomas, Willsch, Michael, Theune, Nils
• Granted Patent: US 6,923,048 B2
• Time in Patent Office: Days
• US Class Current: 73/23.320
• CPC Class Codes: G01K 11/32 using changes in transmittance, scattering or luminescence in optical fibres
• CPC Class Codes: G01L 1/246 using integrated gratings, e.g. Bragg gratings

Abstract

A method and apparatus for monitoring changes in temperature or strain, using fiber Bragg gratings (FBG). The Method and apparatus is advantageously useful for the measurement under harsh conditions, such as by combustion turbines. The invention uses the wavelength shift which is caused by temperature or strain changes at the FBG and the changing of the refraction index of the fiber.

Claims

1. A method of monitoring the condition of a thermal barrier coating within a turbine engine having an operating temperature in excess of 1200°

C., said method comprising;

embedding and thermally protecting a fiber lead into the thermal barrier coating;

embedding at least one fiber Bragg grating sensor into the thermal barrier coating such that the fiber Bragg grating is affected by a thermal or mechanical expansion of the thermal barrier coating; and

using the thermal or mechanical expansion of the thermal barrier coating or the changing of a refraction index of the fiber to determine changes in temperature or strain of the thermal barrier coating.

2. A method of monitoring according claim 1, wherein the fiber lead is thermally protected by placing into a thin stainless steel or Nickel tube.

3. A method of monitoring according claim 2, wherein the fiber Bragg grating is placed into the thin stainless steel or Nickel tube.

4. A method of monitoring according claim 2, wherein the thin stainless steel or Nickel tube is filled with air or a soft heat resistant filling material.

5. A method of monitoring according claim 1, wherein the fiber lead is placed into a thin hole of the substrate.

6. A method of monitoring according claim 3, wherein the fiber Bragg grating is placed loose in the tube.

7. A method of monitoring according claim 6, wherein the fiber Bragg grating is placed by a helical winding in the tube.

8. A method of monitoring according claim 6, wherein the fiber Bragg grating is placed meander like in the hole.

9. A method of monitoring according claim 5, wherein the fiber lead is placed loose in the hole.

10. A method of monitoring according claim 9, wherein the fiber lead is placed by a helical winding in the hole.

11. A method of monitoring according claim 10, wherein the fiber lead is placed meander like in the hole.

12. A method of monitoring according claim 1, wherein the fiber lead or the fiber Brag gratings are embedded inclined to the surface of the thermal barrier coating or a metal component to which the thermal barrier coating is attached.

13. A method of monitoring according claim 12, wherein the fiber lead or the fiber Brag gratings are embedded in the thermal barrier coating and a metal component to which the thermal barrier coating is attached.

14. A method of monitoring according claim 1, wherein the monitoring is performed real-time or near real-time.

15. A method of monitoring according claim 1, wherein the fiber Bragg grating sensor is mounted on or within a carrier.

16. A method of monitoring according claim 15, wherein the carrier is a ceramic carrier.

17. An apparatus for monitoring the condition of a metal component, said apparatus comprising:

a fiber lead embedded into the metal component;

at least one fiber Bragg grating sensor embedded into the metal component, such that the fiber Bragg grating is affected by a thermal or mechanical expansion of the metal component; and

a mechanism using the thermal or mechanical expansion of the metal component or the changing of a refraction index of the fiber to determine changes in temperature or strain.

18. An apparatus according claim 17, wherein the thermal barrier coating or the metal component are within a turbine engine.

19. An apparatus according claim 17, further comprising devices for real-time or near real-time measurement.

20. An apparatus according claim 17, further comprising a light source which provides an incident spectrum which covers all wavelengths of the sensors.

21. A metal component within a turbine engine, comprising:

a fiber lead embedded into said metal component;

at least one fiber Bragg grating sensor embedded into said metal component, wherein the fiber Bragg grating is affected by a thermal or mechanical expansion of the metal component;

a light source which provides an incident spectrum which covers all wavelengths of the sensors; and

a mechanism adopted to use the thermal or mechanical expansion of the metal component or the changing of a refraction index of the fiber to determine changes in temperature or strain of the metal component.

22. A metal component according claim 21, wherein the metal component is coated with a ceramic thermal barrier coating.