Thermographic system and method of operation thereof having composite implants

• US 20030219059A1
• Filed: 05/23/2002
• Published: 11/27/2003
• Est. Priority Date: 05/23/2002
• Status: Abandoned Application

• Current Assignee: The US of America As Represented By The Secretary of The Navy
• Original Assignee: The US of America As Represented By The Secretary of The Navy
• Inventors: Scott, William R.
• Application Number:
  US10/154,470
• Publication Number:
  US 20030219059A1
• Time in Patent Office: Days
• US Class Current: 374/5
• CPC Class Codes: G01N 25/72 Investigating presence of flaws

Abstract

A system employing thermographic techniques is provided for inspecting materials and detecting defects therein such as void, inclusions, interlaminar disbonds, or porosity. The system utilizes a composite material and a source of pulsed current which is delivered to conductive elements within the composite material which, in turn, heats the material being inspected allowing thermographic techniques to be employed to measure the temperature distributions related to the application of the heat source and indicative of the defects of the material being measured.

Claims

1. A system for inspecting materials having a surface, said system inspecting for defects in the materials and comprising:

a) a composite material placed in intimate contact with materials being inspected;

b) a network placed in intimate contact with said composite material and comprising at least one electrically conductive element having accessible electrical contacts;

c) a source of pulsed current connected to said electrical contacts of said electrically conductive element; and

d) instrumentation having the capability for mapping temperature distributions on said surface of said material being inspected.

2. The system according to claim 1, wherein said composite material is a material selected from the group consisting of laminated materials including graphite fiber reinforced plastics.

3. The system according to claim 1, wherein said electrically conductive element is selected from the group consisting of electrically conductive fibers and electrically conductive wires.

4. The system according to claim 3, wherein said electrically conductive wires carry an insulating coating.

5. The system according to claim 1, wherein said composite material is laminated.

6. The system according to claim 5, wherein said electrically conductive element is an electrically conductive fiber and is inserted in said laminated composite material.

7. The system according to claim 1, wherein said instrumentation for mapping temperature distribution on said surface is selected from the group consisting of a holographic camera, a thermographic camera, a thermocouple array, a thermistor array, and a strain gage array.

8. The system according to claim 1, wherein said composite material consists of reinforced fibers having a predetermined size and mechanical properties and said electrically conductive element consists of electrically conductive graphite fibers having parameters selected to substantially match said predetermined size and mechanical properties of said reinforcing fibers.

9. A method for inspecting materials having a surface, said method for detecting defects in the materials and comprising the steps of:

a) providing a composite material that is placed in intimate contact with the materials being inspected;

b) providing a network that is incorporated within said composite material and comprising at least one electrically conductive element having electrical contacts at each end;

c) providing a source of pulsed current which is connected to said conductive element with at least one electrically conductive element at both ends;

d) providing instrumentation having the capability for mapping temperature distributions on said surface;

e) energizing said source of pulsed current which is delivered to said electrically conductive element which, in turn, delivers the pulsed current to said composite material which, in turn, delivers the pulsed current inside said material being inspected; and

f) mapping the temperature distributions on said surface in response to said pulsed current to determine defects in said material being inspected.

10. The method according to claim 9, wherein said defects are represented by images indicative of defects of the group consisting of voids, inclusion, interlaminar disbonds, and porosity.

11. The method according to claim 9, wherein said instrumentation for mapping temperature distribution on said surface is selected from the group consisting of a holographic camera, a thermographic camera, a thermocouple array, a thermistor array and a strain gage array.

12. The method according to claim 10, wherein said source of current is energized on a repetitive basis and said instrumentation corresponding performs gated, synchronized image-averaging.

13. The method according to claim 10, wherein said source of current is energized on a repetitive basis and said instrumentation performs image subtraction.

14. The method according to claim 9, wherein said provided composite material consists of reinforcing fibers having a predetermined size and mechanical properties and said provided electrically conductive element consisting of electrically conductive graphite fibers having parameters selected to substantially match said predetermined size and mechanical properties of said reinforcing fibers.

15. The method according to claim 9, wherein said provided composite material is laminated.

16. The method according to claim 15, wherein said provided electrically conductive element is an electrically conductive fiber and is inserted in said laminated composite material.

17. The method according to claim 16, wherein said provided composite material is a graphite fiber reinforced plastic comprised of laminated epoxy impregnated tapes that are arranged from the group consisting of layers of tapes and adjacent tape layers.

18. The method according to claim 16, wherein said provided electrically conductive elements are selected from the group consisting of wires and fibers and said selected electrically conductive element is placed with said arranged tapes.