Self-referencing microwave sensing system

Patent metadata

Field	Value
Publication number	US-11698348-B2
Application number	US-202017062998-A
Country	US
Kind code	B2
Filing date	Oct 5, 2020
Priority date	Oct 5, 2020
Publication date	Jul 11, 2023
Grant date	Jul 11, 2023

Abstract

A system of a machine includes a waveguide system and a radio frequency transceiver/detector coupled to the waveguide system and configured to emit a calibration signal in the waveguide system to establish a reference baseline between the radio frequency transceiver/detector and a calibration plane associated with an aperture of the waveguide system, emit a measurement signal in the waveguide system to transmit a radio frequency signal from the radio frequency transceiver/detector out of the aperture of the waveguide system, and detect a reflection of the measurement signal at the radio frequency transceiver/detector based on an interaction between the measurement signal and a component of the machine. A measurement result of the reflection of the measurement signal can be adjusted with respect to a reflection of the calibration signal.

First claim

What is claimed is:

1. A system of a machine, the system comprising:
a waveguide system; and
a radio frequency transceiver/detector coupled to the waveguide system and configured to:
emit a calibration signal in the waveguide system to establish a reference baseline between the radio frequency transceiver/detector and a calibration plane associated with an aperture of the waveguide system;
emit a measurement signal in the waveguide system to transmit a radio frequency signal from the radio frequency transceiver/detector out of the aperture of the waveguide system; and
detect a reflection of the measurement signal at the radio frequency transceiver/detector based on an interaction between the measurement signal and a component of the machine, wherein a measurement result of the reflection of the measurement signal is adjusted with respect to a reflection of the calibration signal;

wherein the waveguide system comprises a power-controlled switch configured to reflect the calibration signal and allow the measurement signal through the power-controlled switch based on a power difference between the calibration signal and the measurement signal.

2. The system of claim 1 , wherein the waveguide system comprises a ceramic window proximate to the aperture of the waveguide system.

3. The system of claim 2 , wherein the power-controlled switch is proximate to the ceramic window, wherein the measurement signal is allowed through the ceramic window based on the power difference between the calibration signal and the measurement signal.

4. The system of claim 1 , wherein the machine is a gas turbine engine.

5. The system of claim 4 , wherein the component of the machine is a rotating component of the gas turbine engine.

6. A system for a gas turbine engine, the system comprising:
a network of a plurality of nodes distributed throughout the gas turbine engine, each of the nodes associated with at least one sensor and/or actuator of the gas turbine engine and operable to communicate through one or more radio frequencies;
a controller of the gas turbine engine operable to communicate with the network of nodes through the one or more radio frequencies; and
a radio frequency sensing system coupled to the network of nodes, the radio frequency sensing system comprising a waveguide system and a radio frequency transceiver/detector coupled to the waveguide system and configured to:
emit a calibration signal in the waveguide system to establish a reference baseline between the radio frequency transceiver/detector and a calibration plane associated with an aperture of the waveguide system;
emit a measurement signal in the waveguide system to transmit a radio frequency signal from the radio frequency transceiver/detector out of the aperture of the waveguide system; and
detect a reflection of the measurement signal at the radio frequency transceiver/detector based on an interaction between the measurement signal and a component of the gas turbine engine, wherein a measurement result of the reflection of the measurement signal is adjusted with respect to a reflection of the calibration signal;

wherein the waveguide system comprises a power-controlled switch configured to reflect the calibration signal and allow the measurement signal through the power-controlled switch based on a power difference between the calibration signal and the measurement signal.

7. The system of claim 6 , wherein the waveguide system comprises a ceramic window proximate to the aperture of the waveguide system.

8. The system of claim 7 , wherein the power-controlled switch is proximate to the ceramic window, wherein the measurement signal is allowed through the ceramic window based on the power difference between the calibration signal and the measurement signal.

9. The system of claim 6 , wherein the component monitored by the radio frequency sensing system is a rotating component of the gas turbine engine.

10. A method of self-referencing radio frequency sensing in a machine, the method comprising:
emitting a calibration signal in a waveguide system to establish a reference baseline between a radio frequency transceiver/detector and a calibration plane associated with an aperture of the waveguide system in the machine;
emitting a measurement signal in the waveguide system to transmit a radio frequency signal from the radio frequency transceiver/detector out of the aperture of the waveguide system;
reflecting the calibration signal by a power-controlled switch;
allowing the measurement signal to pass through the power-controlled switch based on a power difference between the calibration signal and the measurement signal;
detecting a reflection of the measurement signal at the radio frequency transceiver/detector based on an interaction between the measurement signal and a component of the machine; and
determining a calibrated measurement result associated with the component of the machine based on adjusting a measurement result of the reflection of the measurement signal with respect to a reflection of the calibration signal.

11. The method of claim 10 , wherein the machine is a gas turbine engine.

12. The method of claim 11 , wherein the component of the machine is a rotating component of the gas turbine engine.

13. The method of claim 10 , wherein the waveguide system comprises a ceramic window proximate to the aperture of the waveguide system.

14. The method of claim 13 , wherein the power-controlled switch is proximate to the ceramic window.

15. The method of claim 14 , wherein the measurement signal is allowed through the ceramic window based on the power difference between the calibration signal and the measurement signal.

Assignees

• Raytheon Tech Corp

Inventors

• Gilson Jonathan
• Mantese Joseph V
• Gok Gurkan
• Djuknic Goran
• Wood Coy Bruce

Classifications

• G01M15/14

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• G01N22/00 Primary

  Investigating or analysing materials by the use of microwaves or radio waves, i.e. electromagnetic waves with a wavelength of one millimetre or more (G01N3/00 - G01N17/00, G01N24/00 take precedence) · CPC title

• F01D11/20 Primary

  Actively adjusting tip-clearance · CPC title

• F01D21/003

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F05D2270/802

  Calibration thereof · CPC title