Impact detection and acoustic emission data processing

Patent metadata

Field	Value
Publication number	US-9500546-B2
Application number	US-201214240237-A
Country	US
Kind code	B2
Filing date	Aug 21, 2012
Priority date	Aug 22, 2011
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

A method and apparatus for processing measurements of an acoustic wave, the acoustic wave being within a member ( 12 ) made of a composite material and caused by an impact to the member ( 12 ), the method comprising: analyzing the measurements to detect an initial acoustic wave feature; analyzing the measurements to detect the presence of further acoustic wave features, the further features occurring after the initial feature; if there are no further acoustic wave features, determining that the impact to the member ( 12 ) has not changed the structure of the member ( 12 ); if there are further features, determining a value of a function of the further acoustic wave features; if the determined value satisfies certain criteria, determining that the impact has changed the structure of the member ( 12 ); and if the determined value does not satisfy the criteria, determining that the impact has not changed the structure of the member ( 12 ). By doing so, impact induced damage is detected and quantified by processing separately acoustic data generated by the impact from acoustic data generated by acoustic emission due to damage generation.

First claim

The invention claimed is:

1. A method of processing measurements of an acoustic wave, the acoustic wave being within a member and caused, at least in part, by an impact to the member, the member being made of a composite material, the method comprising:
analysing the measurements of the acoustic wave to detect an initial acoustic wave feature in the measured acoustic wave;
analysing the measurements of the acoustic wave to determine whether or not there is one or more further acoustic wave features present in the measured acoustic wave, each of the one or more further acoustic wave features occurring in the acoustic wave after the occurrence of the initial acoustic wave feature;
if there are no further acoustic wave features present in the measured acoustic wave, determining that the impact to the member has not changed a structure of the member;
if there is one or more further acoustic wave features present in the measured acoustic wave, determining a value of a function of one or more of the further acoustic wave features;
if the determined value satisfies one or more criteria, determining that the impact to the member has changed the structure of the member; and
if the determined value does not satisfy the one or more criteria, determining that the impact to the member has not changed the structure of the member.

2. A method according to claim 1 , the method further comprising:
filtering the measurements of the acoustic wave; wherein
the initial acoustic wave feature is a feature of the filtered measurements; and
each of the further acoustic wave features is a feature of the filtered measurements.

3. A method according to claim 1 , wherein:
the initial acoustic wave feature is a pulse having an absolute amplitude greater than a first threshold value; and
each of the further acoustic wave features is a further pulse having an absolute amplitude greater than the first threshold value.

4. A method according to claim 1 , wherein a time period between the initial acoustic wave feature occurring in the measured acoustic wave and each of the further acoustic wave features occurring in the measured acoustic wave is greater than a first threshold time-period.

5. A method according to claim 1 , wherein a time period between the initial acoustic wave feature occurring in the measured acoustic wave and each of the further acoustic wave features occurring in the measured acoustic wave is less than or equal to a second threshold time-period.

6. A method according to claim 1 , wherein the function of one or more of the further acoustic wave features is a ratio between an amplitude of the initial acoustic wave feature and an amplitude of at least one of the further acoustic wave features.

7. A method according to claim 1 , wherein the one or more criteria comprises a criterion that the determined value exceeds a second threshold value.

8. A method according to claim 1 , the method further comprising, using measurements of the acoustic wave measured at a plurality of different points on or in the member, determining a location of the impact on the member.

9. A method according to claim 1 , the method further comprising, if it is determined that the impact to the member has changed the structure of the member, outputting an indication that the structure of the member has changed.

10. A method according to claim 1 , wherein the method is performed, at least in part, on an unmanned aircraft.

11. Apparatus for use with a member, the member being made of a composite material, the apparatus comprising:
a sensor arranged to measure an acoustic wave, the acoustic wave being within the member and caused by an impact to the member; and
one or more processors arranged to:
analyse the measurements of the acoustic wave to detect an initial acoustic wave feature in the measured acoustic wave;
analyse the measurements of the acoustic wave to determine whether or not there is one or more further acoustic wave features present in the measured acoustic wave;
if there are no further acoustic wave features present in the measured acoustic wave, determine that the impact to the member has not changed a structure of the member;
if there is one or more further acoustic wave features present in the measured acoustic wave, determine a value of a function of one or more of the further acoustic wave features;
if the determined value satisfies one or more criteria, determine that the impact to the member has changed the structure of the member; and
if the determined value does not satisfy the one or more criteria, determine that the impact to the member has not changed the structure of the member.

12. Apparatus according to claim 11 , wherein:
the sensor is either a piezoelectric sensor or a fibre optic sensor; and
the sensor is either bonded to the member or embedded into the member.

13. An unmanned aircraft comprising:
the apparatus of claim 11 ; and further comprising:
the member being made of the composite material.

14. A non-transitory machine readable storage medium having instructions encoded thereon such that when executed by one or more processors cause the one or more processors to carry out a method of processing measurements of an acoustic wave, the acoustic wave being within a member made of a composite material and caused at least in part by an impact to the member, the method comprising:
analysing the measurements of the acoustic wave to detect an initial acoustic wave feature in the measured acoustic wave;
analysing the measurements of the acoustic wave to determine whether or not there is one or more further acoustic wave features present in the measured acoustic wave, each of the one or more further acoustic wave features occurring in the acoustic wave after the occurrence of the initial acoustic wave feature;
if there are no further acoustic wave features present in the measured acoustic wave, determining that the impact to the member has not changed a structure of the member;
if there is one or more further acoustic wave features present in the measured acoustic wave, determining a value of a function of one or more of the further acoustic wave features;
if the determined value satisfies one or more criteria, determining that the impact to the member has changed the structure of the member; and
if the determined value does not satisfy the one or more criteria, determining that the impact to the member has not changed the structure of the member.

15. A non-transitory machine readable storage medium according to claim 14 , the method further comprising:
filtering the measurements of the acoustic wave; wherein
the initial acoustic wave feature is a feature of the filtered measurements; and
each of the further acoustic wave features is a feature of the filtered measurements.

16. A non-transitory machine readable storage medium according to claim 14 , wherein:
the initial acoustic wave feature is a pulse having an absolute amplitude greater than a first threshold value; and
each of the further acoustic wave features is a further pulse having an absolute amplitude greater than the first threshold value.

17. A non-transitory machine readable storage medium according to claim 14 , wherein a time period between the initial acoustic wave feature occurring in the measured acoustic wave and each of the further acoustic wave features occurring in the measured acoustic wave is greater than a first threshold time-period.

18. A non-transitory machine readable storage medium according to claim 14 , the method further comprising, using measurements

Assignees

• Read Ian James
• John Ryan Nichols
• Macpherson William Neil
• Bae Systems Plc

Inventors

• Read Ian James
• John Ryan Nichols
• Macpherson William Neil

Classifications

• G01N2291/2694

  Wings or other aircraft parts · CPC title

• G01N2291/0231

  Composite or layered materials · CPC title

• G01N29/4427

  with stored values, e.g. threshold values · CPC title

• G01L5/0052 Primary

  measuring forces due to impact (G01L5/0061, G01L5/14 take precedence; impact testing of structures G01M7/08; impact testing of material G01N3/00) · CPC title

• G01N29/11 Primary

  by measuring attenuation of acoustic waves · CPC title