Turbine engine shaft shear detection

Patent metadata

Field	Value
Publication number	US-11761385-B2
Application number	US-202117372761-A
Country	US
Kind code	B2
Filing date	Jul 12, 2021
Priority date	Jul 12, 2021
Publication date	Sep 19, 2023
Grant date	Sep 19, 2023

Abstract

A method is provided involving a turbine engine. During this method, data is received indicative of twist of a shaft of the turbine engine. The data is monitored over time to identity one or more reversal events while the turbine engine is operating, where each of the reversal events corresponds to a reversal in a value sign of the data. Shaft shear is identified in the shaft based on occurrence of N number of the reversal events.

First claim

What is claimed is:

1. A method involving a turbine engine, comprising:
receiving data indicative of twist of a shaft of the turbine engine;
monitoring the data over time to identify one or more reversal events while the turbine engine is operating, wherein each of the reversal events corresponds to a reversal in a value sign of the data; and
identifying shaft shear in the shaft based on occurrence of N number of the reversal events.

2. The method of claim 1 , wherein the N number of the reversal events is one of the reversal events.

3. The method of claim 1 , wherein the N number of the reversal events is two or more of the reversal events.

4. The method of claim 1 , wherein the N number of the reversal events changes based on an operational parameter of the turbine engine.

5. The method of claim 4 , wherein the operational parameter comprises rotational speed of the shaft.

6. The method of claim 4 , wherein the operational parameter comprises power output of the turbine engine.

7. The method of claim 1 , wherein the identifying of the shaft shear in the shaft is further based on the N number of the reversal events occurring within a predetermined period.

8. The method of claim 7 , wherein the predetermined period changes based on an operational parameter of the turbine engine.

9. The method of claim 8 , wherein the operational parameter comprises rotational speed of the shaft.

10. The method of claim 8 , wherein the operational parameter comprises power output of the turbine engine.

11. The method of claim 1 , wherein the identifying of the shaft shear in the shaft is further based on a magnitude of at least one of the N number of the reversal events.

12. The method of claim 1 , further comprising shutting down the turbine engine when the shaft shear in the shaft is identified.

13. The method of claim 1 , wherein the occurrence of the N number of the reversal events is indicative of ringing of the data.

14. The method of claim 1 , wherein the data is further indicative of torque applied to the shaft.

15. The method of claim 1 , wherein a first of the reversal events corresponds to an operational parameter of the turbine engine having a positive value at a first point in time and a negative value at a second point in time.

16. A method involving a turbine engine, comprising:
providing data indicative of torque applied to a shaft of the turbine engine;
monitoring the data over a period to identify ringing in the monitored data while the turbine engine is operating, wherein the ringing in the monitored data indicates the torque applied to the shaft has a positive value at a first point in time and a negative value at a second point in time; and
identifying shaft shear in the shaft based on occurrence of the ringing in the monitored data.

17. The method of claim 16 , wherein
the ringing includes a plurality of reversal events in the monitored data; and
each of the reversal events corresponds to a reversal in a value sign of the monitored data.

18. An assembly for a turbine engine, comprising:
a shaft;
a sensor configured to provide sensor data indicative of a parameter of the shaft, the parameter comprising at least one of twist of the shaft or torque applied to the shaft; and
a controller configured to monitor the sensor data over time to identify one or more reversal events while the turbine engine is operating, each of the reversal events corresponding to a reversal in a value sign of the sensor data, and the controller further configured to identify shaft shear in the shaft based on occurrence of N number of the reversal events.

19. The assembly of claim 18 , further comprising:
a fuel system comprising a flow regulator;
the controller further configured to signal the flow regulator to stop fuel flow when the shaft shear in the shaft is identified.

20. The assembly of claim 18 , further comprising:
a load; and
a turbine rotor;
the shaft coupling the load to the turbine rotor.

Assignees

• Pratt & Whitney Canada

Inventors

• Mccarthy Sean
• Chahal Jasraj
• Beauchesne-Martel Philippe
• Tabar Roja

Classifications

• F01D21/02 Primary

  Shutting-down responsive to overspeed · CPC title

• F02C9/28 Primary

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

• F05D2270/021

  to prevent overspeed · CPC title

• F05D2270/091

  in particular sudden load loss · CPC title

• F05D2260/80

  Diagnostics · CPC title