Gas turbine engine health monitoring system with shaft-twist sensors

Patent metadata

Field	Value
Publication number	US-10316689-B2
Application number	US-201615243107-A
Country	US
Kind code	B2
Filing date	Aug 22, 2016
Priority date	Aug 22, 2016
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

A controller for a gas turbine engine is disclosed. The controller is configured to measure a first rotational speed of a shaft of the engine at a first end of the shaft and to measure a second rotational speed of the shaft at a second end. The first end may be coupled to a turbine of the engine and the second end may be coupled to a compressor of the engine. The controller is further configured to determine a shaft twist angle as a function of the first rotational speed and the second rotational speed, determine whether the shaft twist angle is within a predetermined shaft health monitoring range, and record the shaft twist angle. The controller may be configured to generate a maintenance alert in response to determining that the shaft twist angle is within the predetermined shaft health monitoring range.

First claim

What is claimed is:

1. A controller for gas turbine engine health monitoring, the controller comprising shaft twist monitoring logic configured to:
measure a first rotational speed of a shaft of a gas turbine engine at a first end of the shaft, wherein the first end of the shaft is coupled to a turbine of the gas turbine engine;
measure a second rotational speed of the shaft at a second end of the shaft, wherein the second end of the shaft is coupled to a compressor of the gas turbine engine;
determine a shaft twist angle of the shaft as a function of the first rotational speed and the second rotational speed;
determine whether the shaft twist angle is within a predetermined shaft health monitoring range, wherein to determine whether the shaft twist angle is within the shaft health monitoring range comprises to (i) determine whether the shaft twist angle has a first predetermined relationship to a predetermined maximum in-service twist angle and (ii) determine whether the shaft twist angle has a second predetermined relationship to a predetermined minimum shaft breakage twist angle; and
record the shaft twist angle in response to a determination of whether the shaft twist angle is within the predetermined shaft health monitoring range.

2. The controller of claim 1 , wherein the shaft twist monitoring logic is further configured to generate a maintenance alert in response to a determination that the shaft twist angle is within the predetermined shaft health monitoring range.

3. The controller of claim 1 , wherein the first predetermined relationship comprises is greater than and the second predetermined relationship comprises is less than.

4. The controller of claim 1 , wherein:
to measure the first rotational speed comprises to receive a first speed signal from a first speed sensor of the gas turbine engine; and
to measure the second rotational speed comprises to receive a second speed signal from a second speed sensor of the gas turbine engine.

5. The controller of claim 4 , wherein to determine the shaft twist angle comprises to determine a phase difference between the first speed signal and the second speed signal.

6. The controller of claim 1 , wherein the gas turbine engine comprises a multi-shaft turbine engine and the shaft is concentrically positioned within a second shaft.

7. A method for gas turbine engine health monitoring, the method comprising:
measuring, by a controller of a gas turbine engine, a first rotational speed of a shaft of the gas turbine engine at a first end of the shaft, wherein the first end of the shaft is coupled to a turbine of the gas turbine engine;
measuring, by the controller, a second rotational speed of the shaft at a second end of the shaft, wherein the second end of the shaft is coupled to a compressor of the gas turbine engine;
determining, by the controller, a shaft twist angle of the shaft as a function of the first rotational speed and the second rotational speed;
determining, by the controller, whether the shaft twist angle is within a predetermined shaft health monitoring range, wherein determining whether the shaft twist angle is within the shaft health monitoring range comprises (i) determining whether the shaft twist angle has a first predetermined relationship to a predetermined maximum in-service twist angle and (ii) determining whether the shaft twist angle has a second predetermined relationship to a predetermined minimum shaft breakage twist angle; and
recording, by the controller, the shaft twist angle in response to determining whether the shaft twist angle is within the predetermined shaft health monitoring range.

8. The method of claim 7 , further comprising generating, by the controller, a maintenance alert in response to determining that the shaft twist angle is within the predetermined shaft health monitoring range.

9. The method of claim 7 , wherein:
determining whether the shaft twist angle has the first predetermined relationship to the predetermined maximum in-service twist angle comprises determining whether the shaft twist angle is greater than the maximum in-service twist angle; and
determining whether the shaft twist angle has the second predetermined relationship to the predetermined minimum shaft breakage twist angle comprises determining whether the shaft twist angle is less than the minimum shaft breakage twist angle.

10. The method of claim 7 , wherein:
measuring the first rotational speed comprises receiving a first speed signal from a first speed sensor of the gas turbine engine; and
measuring the second rotational speed comprises receiving a second speed signal from a second speed sensor of the gas turbine engine.

11. The method of claim 10 , wherein determining the shaft twist angle comprises determining a phase difference between the first speed signal and the second speed signal.

12. One or more non-transitory, computer-readable storage media comprising a plurality of instructions that in response to being executed cause a controller of a gas turbine engine to:
measure a first rotational speed of a shaft of the gas turbine engine at a first end of the shaft, wherein the first end of the shaft is coupled to a turbine of the gas turbine engine;
measure a second rotational speed of the shaft at a second end of the shaft, wherein the second end of the shaft is coupled to a compressor of the gas turbine engine;
determine a shaft twist angle of the shaft as a function of the first rotational speed and the second rotational speed;
determine whether the shaft twist angle is within a predetermined shaft health monitoring range, wherein to determine whether the shaft twist angle is within the shaft health monitoring range comprises to (i) determine whether the shaft twist angle has a first predetermined relationship to a predetermined maximum in-service twist angle and (ii) determine whether the shaft twist angle has a second predetermined relationship to a predetermined minimum shaft breakage twist angle; and
record the shaft twist angle in response to determining whether the shaft twist angle is within the predetermined shaft health monitoring range.

13. The one or more non-transitory, computer-readable storage media of claim 12 , further comprising a plurality of instructions that in response to being executed cause the controller to generate a maintenance alert in response to determining that the shaft twist angle is within the predetermined shaft health monitoring range.

14. The one or more non-transitory, computer-readable storage media of claim 12 , wherein:
to determine whether the shaft twist angle has the first predetermined relationship to the predetermined maximum in-service twist angle comprises to determine whether the shaft twist angle is greater than the maximum in-service twist angle; and
to determine whether the shaft twist angle has the second predetermined relationship to the predetermined minimum shaft breakage twist angle comprises to determine whether the shaft twist angle is less than the minimum shaft breakage twist angle.

15. The one or more non-transitory, computer-readable storage media of claim 12 , wherein:
to measure the first rotational speed comprises to receive a first speed signal from a first speed sensor of the gas turbine engine; and
to measure the second rotational speed comprises to receive a second speed signal from a second speed sensor of the gas turbine engine.

16. The one or more non-transitory, computer-readable storage media of claim 15 , wherein to determine the shaft twist angle comprises to determine a phase difference between the first speed signal and

Assignees

• Rolls Royce Corp

Inventors

• Fletcher William S

Classifications

• F04D29/053

  Shafts · CPC title

• F04D25/045

  the pump wheel carrying the fluid driving means, e.g. turbine blades · CPC title

• F02C3/00

  Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C5/00) · CPC title

• F05D2240/60

  Shafts · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title