Turbine blade monitoring

Patent metadata

Field	Value
Publication number	US-9995167-B2
Application number	US-201515329381-A
Country	US
Kind code	B2
Filing date	Jul 28, 2015
Priority date	Aug 1, 2014
Publication date	Jun 12, 2018
Grant date	Jun 12, 2018

Abstract

A blade monitoring system and method for a turbine assembly comprising rotating blades ( 14 ), the system comprising at least one sensor ( 10, 12 ) for transmitting a signal towards said rotating blades and detecting a time-varying return signal therefrom, and one or more processors ( 20 ) configured to calculate the time derivative of said return signal, generate a phase variation signal for said time derivative, determine minima points within said phase variation signal and measure said signal at said minima points so as to identify data representative of respective minimum path lengths, each said minimum path length corresponding to the returned signal as each respective blade passes said sensor, and generate, using said minimum path lengths, a time series of data representing the returned signal from individual blades as they pass the sensor.

First claim

What is claimed is:

1. A blade monitoring system for a turbine assembly comprising rotating blades, the system comprising at least one sensor for transmitting a signal towards said rotating blades and detecting a time-varying return signal therefrom, and one or more processors configured to calculate the time derivative of said return signal, generate a phase variation signal for said time derivative, determine minima points within said phase variation signal and measure said signal at said minima points so as to identify data representative of respective minimum path lengths, each said minimum path length corresponding to the returned signal as each respective blade passes said sensor, and generate, using said minimum path lengths, a time series of data representing the returned signal from individual blades as they pass the sensor.

2. The system according to claim 1 , wherein the transmitted signal is a wideband signal for enabling a return signal to be collected from substantially a complete blade and/or shaft to be collected.

3. The system, according to claim 1 , comprising a monostatic sensor, which is configured to transmit said signal towards said rotating blades and receive said returned signal.

4. The system according to claim 3 , wherein said at least one processor is configured to estimate and remove a DC component from said returned signal.

5. The system according to claim 1 , comprising a bistatic sensor arrangement comprising a first sensor for transmitting said signal towards said rotating blades, and a second sensor for receiving said returned signal.

6. The system according to claim 1 , wherein said one or more processor is configured to identify and remove a bias from the signal before generating said time series.

7. The system according to claim 1 , wherein said signal is a radar signal.

8. The system according to claim 7 , wherein said signal comprises a continuous wave radar signal.

9. The system according to claim 1 , wherein the or each sensor comprises a probe located within an existing boroscope or inspection hole or aperture in said turbine assembly.

10. A method of generating, in an engine health monitoring system for a turbine assembly comprising a plurality of rotating blades, a time series of data representative of a returned signal as individual blades pass a sensor, the method comprising obtaining a time-varying return signal from said rotating blades, calculating the time derivative of said return signal, generating a phase variation signal for said time derivative, determining minima points within said phase variation signal and measuring said signal at said minima points so as to identify data representative of respective minimum path lengths, each said minimum path length corresponding to the returned signal as each respective blade passes said sensor, and generating, using said minimum path lengths, a time series of data representing the returned signal from individual blades as they pass the sensor.

11. The method according to claim 10 , further comprising the step of estimating and removing a DC component from said return signal.

12. A program or plurality of programs arranged such that when executed by a computer system or one or more processors, it/they cause the computer system or the one or more processors to operate in accordance with the method of claim 10 .

13. A machine readable storage medium storing a program or at least one of the plurality of programs according to claim 12 .

14. An engine health monitoring system for a turbine assembly comprising a plurality of rotating blades, comprising a system according to claim 1 for generating a time series of data representing a returned signal from individual blades as they pass the sensor, and an analysis module configured, in use, to determine sequential blocks of said time series of data corresponding to the rotation rate of said rotating blades, and calculating in respect of each of a plurality of said blades data representative of at least one of blade clearance and blade vibration.

15. The engine health monitoring system according to claim 14 , wherein said analysis module is configured to calculate in respect of each of said plurality of blades data representative of blade clearance, the system further comprising a clearance control mechanism for controlling at least one operating parameter of said turbine assembly in response to said data representative of blade clearance.

Assignees

• Bae Systems Plc

Inventors

• Shepard David John

Classifications

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• G01S13/003

  Bistatic radar systems; Multistatic radar systems · CPC title

• G01S7/415

  Identification of targets based on measurements of movement associated with the target · CPC title

• B64D27/16

  of jet type · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title