System for sensing and locating delamination

Patent metadata

Field	Value
Publication number	US-10139376-B2
Application number	US-201615087416-A
Country	US
Kind code	B2
Filing date	Mar 31, 2016
Priority date	Mar 31, 2016
Publication date	Nov 27, 2018
Grant date	Nov 27, 2018

Abstract

A system to monitor a composite system component may include a plurality of sensors mounted proximate to the composite system component. A signal processing unit may receive, from each of the plurality of sensors, a series of sensed values associated with the composite system component and determine a kurtosis value for each series of sensed values. A threshold exceedance detector may detect if at least one of the kurtosis values exceeds a pre-determined threshold value. A delamination location estimation unit may calculate an estimated location of a composite system component delamination alert signal based on calculated time difference delay values of detected signal impulses in the series of sensed values using at least four of the plurality of sensors. A delamination alert output may then transmit a composite system component delamination alert signal, along with the estimated location, when at least one of the kurtosis values exceeds the pre-determined threshold.

First claim

The invention claimed is:

1. A system to monitor a composite system component, comprising:
a plurality of sensors mounted proximate to the composite system component;
a signal processing unit to receive, from each sensor, a series of sensed values associated with the composite system component and to determine a kurtosis value for each series of sensed values;
a threshold exceedance detector to detect if at least one of the kurtosis values exceeds a threshold value;
a delamination location estimation unit to calculate an estimated location of a composite system component associated with a delamination alert signal based on calculated time difference delay values of detected signal impulses in the series of sensed values using at least four of the plurality of sensors;
a delamination alert output to transmit a composite system component delamination alert signal, along with the estimation location, when at least one of the kurtosis values exceeds the threshold;
wherein the signal processing unit is associated with a digital twin of a twinned physical system, the twinned physical system including the composite system component;
wherein the digital twin comprises:
one or more digital twin sensors to sense values of one or more designated parameters of the twinned physical system;
a computer processor to receive data associated with the one or more digital twin sensors and programmed to:
for at least a selected portion of the twinned physical system, execute at least one of: (i) a monitoring process to monitor a condition of the selected portion of the twinned physical system based at least in part on the sensed values of the one or more designated parameters, and (ii) an assessing process to assess a remaining useful life of the selected portion of the twinned physical system based at least in part on the sensed values of the one or more designated parameters and
a communication port coupled to the computer processor to transmit information associated with a result generated by the computer processor,

wherein the one or more digital twin sensors are to sense values of the one or more designated parameters, and the computer processor is to execute at least one of the monitoring and assessing processes, when the twinned physical system is not operating.

2. The system of claim 1 , wherein the estimated location is calculated based at least in part on time differences of arrival.

3. The system of claim 1 , wherein at least one sensor is associated with at least one of: (i) an acoustic sensor, (ii) a seismic sensor, (iii) an accelerometer transducer sensor, and (iv) a multi-point transducer.

4. The system of claim 1 , wherein the composite system component delamination alert signal is responsive to at least one of: (i) a shock signal signature, (ii) a jerk signal signature, (iii) a crackling signal signature, (iv) a cracking signal signature, and (v) a relatively low speed, blunt impact to the composite system component.

5. The system of claim 1 , wherein at least one of the sensors is placed on or impregnated within the composite system component.

6. A computerized method to monitor a composite system component, comprising:
receiving by a signal processing unit a series of sensed values, associated with the composite system component, from each of a plurality of sensors mounted proximate to the composite system component;
determining by the signal processing unit a kurtosis value for each series of sensed values;
detecting, by a threshold exceedance detector, if at least one of the kurtosis values exceeds a threshold value;
calculating, by a delamination location estimation unit, an estimated location of a composite system component associated with a delamination alert signal based on calculated time difference delay values of detected signal impulses in the series of sensed values using at least four of the plurality of sensors;
transmitting, via a delamination alert output, a composite system component delamination alert signal, along with the estimated location, when the at least one of the kurtosis values exceeds the threshold;
wherein the signal processing unit is associated with a digital twin of a twinned physical system, the twinned physical system including the composite system component;
wherein the digital twin comprises:
one or more digital twin sensors to sense values of one or more designated parameters of the twinned physical system;
a computer processor to receive data associated with the one or more digital twin sensors and programmed to:
for at least a selected portion of the twinned physical system, execute at least one of: (i) a monitoring process to monitor a condition of the selected portion of the twinned physical system based at least in part on the sensed values of the one or more designated parameters, and (ii) an assessing process to assess a remaining useful life of the selected portion of the twinned physical system based at least in part on the sensed values of the one or more designated parameters and
a communication port coupled to the computer processor to transmit information associated with a result generated by the computer processor,

wherein the one or more digital twin sensors are to sense values of the one or more designated parameters, and the computer processor is to execute at least one of the monitoring and assessing processes, when the twinned physical system is not operating.

7. The method of claim 6 , wherein the estimated location is based at least in part on time differences of arrival.

8. The method of claim 7 , wherein at least one sensor is associated with at least one of: (i) an acoustic sensor, (ii) a seismic sensor, (iii) an accelerometer transducer sensor, and (iv) a multi-point transducer.

9. The method of claim 7 , wherein the composite system component alert signal is responsive to at least one of: (i) a shock signal signature, (ii) a jerk signal signature, (iii) a crackling signal signature, (iv) a cracking signal signature, and (v) a relatively low speed, blunt impact to the composite system component.

10. The method of claim 6 , wherein at least one of the sensors is placed on or impregnated within the composite system component.

11. A non-transitory, computer-readable medium storing instructions that, when executed by a computer processor, cause the computer processor to perform a method to monitor a composite system component, the method comprising:
receiving by a signal processing unit a series of sensed values, associated with the composite system component, from each of a plurality of sensors mounted proximate to the composite system component;
determining by the signal processing unit a kurtosis value for each series of sensed values;
detecting, by a threshold exceedance detector, if at least one of the kurtosis values exceeds a threshold value;
calculating, by a delamination location estimation unit, an estimated location of a composite system component associated with a delamination alert signal based on calculated time difference delay values of detected signal impulses in the series of sensed values using at least four of the plurality of sensors;
transmitting, via a delamination alert output, a composite system component delamination alert signal, along with the estimated location, when the at least one of the kurtosis values exceeds the threshold;
wherein the signal processing unit is associated with a digital twin of a twinned physical system, the twinned physical system including the composite system component;
wherein the digital twin comprises:
one or more digital twin sensors to sense values of one or more designated parameters of the twinned physical system;
a computer processor to receive da

Assignees

• Gen Electric

Inventors

• Hershey John Erik
• Wheeler Frederick Wilson

Classifications

• G01N2291/023

  Solids · CPC title

• G01P15/001

  by measuring acceleration changes by making use of a triple differentiation of a displacement signal · CPC title

• G01N29/449 Primary

  Statistical methods not provided for in G01N29/4409, e.g. averaging, smoothing and interpolation · CPC title

• G01N2291/0289

  Internal structure, e.g. defects, grain size, texture · CPC title

• G08B21/182

  Level alarms, e.g. alarms responsive to variables exceeding a threshold · CPC title