Shaft break detection

• US 9,410,444 B2
• Filed: 11/02/2012
• Issued: 08/09/2016
• Est. Priority Date: 11/29/2011
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Bacic, Marko
• Primary Examiner(s): Edgar, Richard
• Assistant Examiner(s): Wolcott, Brian P
• Application Number:
  US13/667,220
• Publication Number:
  US 20130133333A1
• Time in Patent Office: 1,376 Days
• US Class Current: 1/1
• CPC Class Codes: F01D 17/04 responsive to load
• CPC Class Codes: F01D 17/06 responsive to speed
• CPC Class Codes: F01D 17/08 responsive to condition of working-fluid, e.g. pressure
• CPC Class Codes: F01D 17/085 to temperature
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F01D 21/04 responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
• CPC Class Codes: F01D 21/045 special arrangements in stators or in rotors dealing with breaking-off of part of rotor

Abstract

The present invention provides a method of detecting shaft break in a shaft system comprising a shaft coupled between two masses. The method comprises a number of steps. Firstly, to define a time-dependent rotational speed equation for the shaft in terms of system inertia for an engine transient event. Then to discretize the rotational speed equation in terms of a discrete time constant in the discrete domain. Then to recursively define the discretized equation to give a recursive equation and to solve the recursive equation to determine the discrete time constant. Then to define a threshold as a function of engine power and then to set a shaft break signal to TRUE if the discrete time constant is greater than the threshold. A shaft break detection system is also provided by the present invention.

Claims

1. A method of detecting shaft break in a shaft system comprising a shaft coupled between two masses, the method comprising steps to:

define a time-dependent rotational speed equation for the shaft in terms of system inertia for an engine transient event;

discretize the rotational speed equation in terms of a discrete time constant in a discrete domain;

recursively define the discretized equation to give a recursive equation;

solve the recursive equation to determine the discrete time constant;

define a threshold as a function of engine power, wherein the threshold is a value of the discrete time constant calculated as the function of engine power; and

set a shaft break detection signal to TRUE and reduce or stop a drive to the shaft if the discrete time constant is less than the threshold.

2. A method as claimed in claim 1 wherein the rotational speed equation is a first order linearised equation that approximates the shaft system.

3. A method as claimed in claim 1 wherein the rotational speed equation is exponential in terms of an inverse time constant of speed decay.

4. A method as claimed in claim 3 wherein the inverse time constant of speed decay is inversely proportional to an inertia of the shaft system, wherein the inertia of the shaft system is equal to the sum of the inertias of the masses.

5. A method as claimed in claim 1 wherein the recursive equation is solved using a recursive least squares method using a last n speed samples wherein n is in the range 4 to 20.

6. A method as claimed in claim 1 wherein the steps of solving the recursive equation, defining the threshold and setting the shaft break detection signal are performed iteratively.

7. A method as claimed in claim 1 further comprising a step of sampling a rotational speed of the shaft before the step of solving the recursive equation.

8. A method as claimed in claim 1 wherein the shaft system is a gas turbine engine shaft system.

9. A method as claimed in claim 8 wherein the two masses comprise a compressor and a turbine of a gas turbine engine.

10. A method as claimed in claim 1 wherein engine power is indicated by at least one engine parameter of the group comprising:

altitude, compressor exit pressure, another shaft speed, lagged compressor exit pressure, corrected shaft speed of another shaft.

11. A method as claimed in claim 1 wherein the engine transient event comprises engine surge.

12. A gas turbine engine comprising a method as claimed in claim 1.

13. A shaft break detection system comprising:

a shaft coupled between two masses;

at least one sensor to sample rotational speed of the shaft;

a processor to process the sampled speed to recursively solve a discretised rotational speed equation to determine a discrete time constant;

a processor to determine a threshold as a function of engine power, wherein the threshold is a value of the discrete time constant calculated as the function of engine power; and

a comparator to set a shaft break detection signal to TRUE in order to reduce or stop a drive to the shaft if the discrete time constant is less than the threshold.

14. A system as claimed in claim 13 further comprising a sensor to sense an engine power parameter of the group comprising:

altitude, compressor exit pressure, another shaft speed, lagged compressor exit pressure and corrected shaft speed of another shaft.

15. A system as claimed in claim 13 further comprising memory to store the last n speed samples.

16. A system as claimed in claim 13 wherein the two masses comprise a compressor and a turbine of a gas turbine engine.

17. A system as claimed in claim 13 wherein the two masses are a torque generator and a load.

18. A gas turbine engine comprising a system as claimed in claim 13.