Structural health monitoring system

Patent metadata

Field	Value
Publication number	US-9719967-B2
Application number	US-201113226199-A
Country	US
Kind code	B2
Filing date	Sep 6, 2011
Priority date	Feb 8, 2011
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

The present invention relates to a structural health monitoring system, for example a system used in the non-destructive evaluation of an aircraft structure. The present invention provides a method and apparatus for evaluating one or more anomalies within a structure using a structural health monitoring system that includes at least three transducers arranged in operative contact with the structure such that no two transducers are aligned to be parallel. A transducer excites an elastic wave that propagates through the structure, and reflections from any anomalies within the structure are collected by the three transducers. These collected signals are analyzed to identify an anomaly within the structure. Time of flight techniques are used to determine the location of the anomaly.

First claim

The invention claimed is:

1. A method of evaluating damage within a structure using a structural health monitoring system comprising at least three receivers arranged in direct contact with the structure and a single transmitter arranged in direct contact with the structure and separate from the at least three receivers, the at least three receivers having corresponding longitudinal axes extending in different directions such that no two of the at least three receivers are aligned to be parallel, the method comprising:
propagating an elastic wave through the structure using the single transmitter;
collecting monitoring signals from the at least three receivers to monitor for reflections of the elastic wave from at least one anomaly within the structure; and
analysing the monitoring signals to identify the at least one anomaly.

2. The method of claim 1 , wherein analysing the monitoring signals comprises performing a differencing operation wherein, for each receiver of the at least three receivers, a corresponding reference signal is subtracted from corresponding monitoring signals collected by a corresponding receiver of the at least three receives, and wherein resultant differencing signals are used to identify the at least one anomaly within the structure.

3. The method of claim 2 , wherein the structure comprises an aircraft component and, further comprising:
collecting reference signals from the aircraft component for each receiver of the at least three receivers, after the aircraft component is deemed ready for operation of the aircraft.

4. The method of claim 1 , wherein analysing the monitoring signals to identify the at least one anomaly comprises calculating a corresponding time of flight of corresponding reflections received by each receiver of the at least three receivers.

5. The method of claim 4 , wherein analysing the monitoring signals comprises calculating corresponding distances from each of the corresponding time of flights and wherein a location of the at least one anomaly is determined from the corresponding distances.

6. The method of claim 5 , wherein determining the location of the at least one anomaly comprises identifying the location from the corresponding distances, a first known location of the single transmitter, and at least a second known location of at least one of the at least three receivers.

7. A method of evaluating damage within a structure using a structural health monitoring system comprising a first array of a first set of at least three receivers arranged in direct contact with the structure, the first set of at least three receivers having corresponding first longitudinal axes extending in different directions such that no two of the first set of at least three receivers are aligned to be parallel, the first array further comprising a first single transmitter arranged in direct contact with the structure in proximity to and separate from the first set of at least three receivers, and the structural health monitoring system further comprising a second array of a second set of at least three receivers arranged in direct contact with the structure, the second set of at least three receivers having corresponding second longitudinal axes extending in different directions such that no two of the second set of at least three receivers are aligned to be parallel, the second array further comprising a second single transmitter arranged in direct contact with the structure in proximity to and separate from the second set of at least three receivers, wherein the first and second arrays are spaced apart from each other, the method comprising:
propagating a first elastic wave through the structure using the first single transmitter of the first array;
collecting a first set of monitoring signals from the first set of at least three receivers of the first array to monitor for first reflections of the first elastic wave from at least one anomaly within the structure;
propagating a second elastic wave through the structure using the second single transmitter of the second array;
collecting a second set of monitoring signals from the second set of at least three receivers of the second array to monitor for second reflections of the second elastic wave from the at least one anomaly within the structure; and
analysing the first set of monitoring signals and the second set of monitoring signals to identify the at least one anomaly and to determine a first direction from the first array to the at least one anomaly and to determine a second direction from the second array to the at least one anomaly.

8. A structural health monitoring system for monitoring a structure, comprising:
a first set of at least three receivers in direct contact with the structure, the first set of at least three receivers having corresponding longitudinal axes extending in different directions such that no two of the first set of at least three receivers are aligned to be parallel;
a first single transmitter in direct contact with the structure in proximity to and separate from the first set of at least three receivers, wherein the first single transmitter is configured to excite a first elastic wave to propagate through the structure; and
a processor directly coupled to the first set of at least three receivers, the processor configured to collect a first set of corresponding monitoring signals from corresponding ones of the at least three receivers, wherein the processor is further configured to analyse the first set of corresponding monitoring signals to identify at least one anomaly within the structure.

9. The structural health monitoring system of claim 8 , wherein the processor is further configured to calculate a corresponding time of flight of corresponding reflections received by each receiver of the at least three receivers.

10. The structural health monitoring system of claim 9 , wherein the processor is further configured to calculate corresponding distances from each of the corresponding time of flights and wherein a location of the at least one anomaly is determined from the corresponding distances.

11. The structural health monitoring system of claim 10 , wherein the processor is further configured to determine the location of the at least one anomaly by identifying the location from the corresponding distances, a first known location of the single transmitter, and at least a second known location of at least one of the at least three receivers.

12. The structural health monitoring system of claim 8 further comprising:
a second set of at least three receivers in direct contact with the structure;
a second single transmitter in direct contact with the structure, wherein the second single transmitter is configured to excite a second elastic wave to propagate through the structure;
wherein the processor is directly coupled to the second set of at least three receivers, the processor configured to collect a second set of corresponding monitoring signals from corresponding ones of the second set of at least three receivers, wherein the processor is further configured to analyse both the first set of corresponding monitoring signals and the second set of corresponding monitoring signals to identify the at least one anomaly within the structure.

13. The structural health monitoring system of claim 12 wherein, for each receiver of the first set of at least three receives and for each receiver of the second set of at least three receivers, a corresponding receiver comprises a corresponding piezoelectric transducer with a corresponding longitudinal axis and a corresponding transverse axis, wherein each corresponding receiver is arranged such that no tw

Assignees

• Kawiecki Grzegorz Marian
• Rodriguez Rosa Maria
• Kudela Pawel
• Ostachowicz Wieslaw
• Boeing Co

Inventors

• Kawiecki Grzegorz Marian
• Rodriguez Rosa Maria
• Kudela Pawel
• Ostachowicz Wieslaw

Classifications

• G01N2291/2694

  Wings or other aircraft parts · CPC title

• G01N2291/103

  one emitter, two or more receivers · CPC title

• G01N2291/0258

  Structural degradation, e.g. fatigue of composites, ageing of oils · CPC title

• G01L1/183

  by measuring variations of frequency of vibrating piezo-resistive material · CPC title

• G01L1/16

  using properties of piezoelectric devices · CPC title