Phosphor thermometer with two waveguides

Patent metadata

Field	Value
Publication number	US-9696217-B2
Application number	US-201414301927-A
Country	US
Kind code	B2
Filing date	Jun 11, 2014
Priority date	Oct 30, 2013
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

A phosphor thermometer is disclosed. The phosphor thermometer may comprise a light source configured to emit an excitation light, and an input waveguide configured to transmit at least a portion of the excitation light from the light source to a temperature sensing end. A phosphor may be located at the temperature sensing end and it may be configured to emit a fluorescence signal upon absorption of at least a portion of the excitation light transmitted by the input waveguide. The phosphor thermometer may further comprise an output waveguide configured to transmit at least a portion of the fluorescence signal from the phosphor to a detector. The detector may determine a fluorescence decay constant from the time dependent decay of the fluorescence signal, and the fluorescence decay constant may be correlated with a temperature.

First claim

What is claimed:

1. A phosphor thermometer, comprising:
a light source configured to emit an excitation light;
an input waveguide configured to transmit at least a portion of the excitation light from the light source to a temperature sensing end;
a phosphor located at the temperature sensing end, the phosphor being configured to emit a fluorescence signal upon absorption of at least a portion of the excitation light; and
an output waveguide configured to transmit at least a portion of the fluorescence signal from the phosphor to a detector,
wherein the input waveguide comprises a transmitting end proximal to the phosphor and the output waveguide comprises a receiving end proximal to the phosphor, and
wherein the phosphor, a tip of the transmitting end, and a tip of the receiving end are encapsulated in an optically transmitting material.

2. The phosphor thermometer of claim 1 , wherein the tip of the transmitting end of the input waveguide comprises a surface extending at a 90° angle with respect to a longitudinal axis of the transmitting end, the surface being spaced from the phosphor by a distance along the longitudinal axis.

3. The phosphor thermometer of claim 1 , wherein the tip of the receiving end of the input waveguide comprises a surface extending at a 90° angle with respect to a longitudinal axis of the receiving end, the surface being spaced from the phosphor by a distance along the longitudinal axis.

4. The phosphor thermometer of claim 1 , wherein the tip of the transmitting end of the input waveguide comprises at least one surface extending at an angle other than 0° or 90° with respect to a longitudinal axis of the transmitting end, the tip being spaced from the phosphor by a distance.

5. The phosphor thermometer of claim 1 , wherein the tip of the receiving end of the input waveguide comprises at least one surface extending at an angle other than 0° or 90° with respect to a longitudinal axis of the receiving end, the tip being spaced from the phosphor by a distance.

6. The phosphor thermometer of claim 1 , wherein the phosphor, the tip of the transmitting end, the tip of the receiving end, and the optically transmitting material are further encapsulated in an opaque material.

7. The phosphor thermometer of claim 1 , wherein the phosphor comprises a hollow interior, and the tip of the transmitting end and the tip of the receiving end penetrate the hollow interior.

8. The phosphor thermometer of claim 7 , wherein the hollow interior is filled with an optically transmitting material.

9. The phosphor thermometer of claim 7 , wherein the phosphor, the tip of the transmitting end, and the tip of the receiving end are encapsulated in an opaque material.

10. A gas turbine engine, comprising: a fan section;
a low pressure compressor located downstream of the fan section;
a high pressure compressor located downstream of the low pressure compressor;
a combustor located downstream of the high pressure compressor; a high pressure turbine located downstream of the combustor;
a low pressure turbine located downstream of the high pressure turbine;
at least one phosphor thermometer located at at least one of an inlet of the low pressure compressor, an outlet of the low pressure compressor, an inlet of the high pressure compressor, an outlet of the high pressure compressor, an inlet of the combustor, an outlet of the combustor, an inlet of the high pressure turbine, an outlet of the high pressure turbine, an inlet of the low pressure turbine, and an outlet of the low pressure turbine, the at least one phosphor thermometer comprising
a light source configured to emit an excitation light,
an input waveguide configured to transmit at least a portion of the excitation light from the light source to a temperature sensing end,
a phosphor located at the temperature sensing end, the phosphor being configured to emit a fluorescence signal upon absorption of at least a portion of the excitation light,
an output waveguide configured to transmit at least a portion of the fluorescence signal from the phosphor to a detector, the detector being configured to determine a temperature from the fluorescence signal,
wherein the input waveguide comprises a transmitting end proximal to the phosphor and the output waveguide comprises a receiving end proximal to the phosphor, and
wherein the phosphor, a tip of the transmitting end, and a tip of the receiving end are encapsulated in an optically transmitting material.

11. The gas turbine engine of claim 10 , wherein the tip of the transmitting end of the input waveguide comprises a surface extending at a 90° angle with respect to a longitudinal axis of the transmitting end, the surface being spaced from the phosphor by a distance along the longitudinal axis.

12. The gas turbine engine of claim 10 , wherein the tip of the receiving end of the input waveguide comprises a surface extending at a 90° angle with respect to a longitudinal axis of the receiving end, the surface being spaced from the phosphor by a distance along the longitudinal axis.

13. The gas turbine engine of claim 10 , wherein the tip of the transmitting end of the input waveguide comprises a surface extending at an angle other than 0° or 90° with respect to a longitudinal axis of the transmitting end, the tip being spaced from the phosphor by a distance.

14. The gas turbine engine of claim 10 , wherein the tip of the receiving end of the input waveguide comprises a surface extending at an angle other than 0° or 90° with respect to a longitudinal axis of the receiving end, the tip being spaced from the phosphor by a distance.

15. The gas turbine engine of claim 10 , wherein the phosphor, the tip of the transmitting end, the tip of the receiving end, and the optically transmitting material are further encapsulated in an opaque material.

Assignees

• United Technologies Corp

Inventors

• Hockaday Bruce

Classifications

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• F05D2270/0831

  indirectly, at the exhaust · CPC title

• G01K11/3213

  using changes in luminescence, e.g. at the distal end of the fibres · CPC title

• G01K13/02 Primary

  for measuring temperature of moving fluids or granular materials capable of flow · CPC title

• F02C9/28

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title