System and method for high speed FOD detection

Patent metadata

Field	Value
Publication number	US-10335838-B2
Application number	US-201715806380-A
Country	US
Kind code	B2
Filing date	Nov 8, 2017
Priority date	Feb 4, 2015
Publication date	Jul 2, 2019
Grant date	Jul 2, 2019

Abstract

A system for the detection of foreign object debris material on a surface of a composite part being manufactured. A platform is configured to move over the surface. A thermal excitation source is fixed to the platform and configured to direct infrared radiation across the surface. An infrared camera is also fixed to the platform and configured to scan the surface as the platform moves over the surface to detect and output a signal proportional to infrared radiation emitted by the surface and/or by any foreign object debris material on the surface in response to the infrared radiation from the excitation source. A controller is coupled to the excitation source and to the infrared camera and is configured to compare the signal from the infrared camera with a first predetermined threshold signal to detect if any foreign object debris material is located on the surface.

First claim

What is claimed is:

1. A system for detection of foreign object debris material on a surface, the system comprising:
a thermal excitation source configured to direct infrared radiation across the surface;
an infrared camera configured to scan the surface and output a first signal proportional to emitted infrared radiation emitted by at least one of the surface and a first type of foreign object debris material, the emitted infrared radiation responsive to the infrared radiation from the thermal excitation source;
a controller coupled to the thermal excitation source and to the infrared camera, the controller configured to compare the first signal from the infrared camera with a first threshold to detect presence of the first type of foreign object debris material; and
a controllable nozzle coupled to a high pressure gas source and coupled to the controller, wherein the controller, in response to detection of the first type of foreign object debris material on the surface, directs gas through the controllable nozzle at the first type of foreign object debris material.

2. The system of claim 1 , further comprising a layup machine to apply a layer of material to the surface, the layup machine configured to move along the surface, wherein the thermal excitation source, the infrared camera and the controllable nozzle are coupled to the layup machine.

3. The system of claim 1 , further comprising a terminal coupled to the controller, the terminal including a display, and wherein the controller is further configured to provide an indication on the display upon detection of foreign object debris material.

4. The system of claim 1 , further comprising:
an ultraviolet light source configured to direct ultraviolet light across the surface;
an ultraviolet light camera configured to scan the surface and output a second signal proportional to reflected ultraviolet light reflected by at least one of the surface and a second type of foreign object debris material, the reflected ultraviolet light responsive to the ultraviolet light from the ultraviolet light source; and
wherein the controller, in response to detection of the second type of foreign object debris material based on a comparison of the second signal to a second threshold, directs gas through the controllable nozzle at the second type of foreign object debris material.

5. The system of claim 4 , further comprising:
a visible light source configured to direct visible light across the surface;
a visible light camera configured to scan the surface and output a third signal proportional to reflected visible light reflected by at least one of the surface and a third type of foreign object debris material, the reflected visible light responsive to the visible light from the visible light source; and
wherein the controller, in response to detection of the third type of foreign object debris material based on a comparison of the third signal to a third threshold, directs gas through the controllable nozzle at the third type of foreign object debris material.

6. The system of claim 1 , further comprising:
a visible light source configured to direct visible light across the surface;
a visible light camera configured to scan the surface and output a second signal proportional to reflected visible light reflected by at least one of the surface and a second type of foreign object debris material, the reflected visible light responsive to the visible light from the visible light source; and
wherein the controller, in response to detection of the second type of foreign object debris material based on a comparison of the second signal to a second threshold, directs gas through the controllable nozzle at the second type of foreign object debris material.

7. The system of claim 1 , further comprising:
a conveyor to move the surface relative to a layup machine that applies a layer of material to the surface; and
a platform coupled to the thermal excitation source, the infrared camera, and the controllable nozzle.

8. The system of claim 1 , wherein the surface is an outer surface of a composite part being formed by a composite layup machine.

9. The system of claim 1 , further comprising:
a second infrared camera configured to scan the surface and output a second signal proportional to reflected infrared radiation reflected by at least one of the surface and a second type of foreign object debris material, the reflected infrared radiation responsive to the infrared radiation from the thermal excitation source; and
wherein the controller, in response to detection of the second type of foreign object debris material based on a comparison of the second signal to a second threshold, directs gas through the controllable nozzle at the second type of foreign object debris material.

10. A system for detection of foreign object debris material, the system comprising:
a thermal excitation source configured to direct infrared radiation across a surface, wherein the surface is an outer surface of a composite part being formed by a composite layup machine;
an infrared camera configured to scan the surface and output a first signal proportional to emitted infrared radiation emitted by at least one of the surface and a first type of foreign object debris material, the emitted infrared radiation responsive to the infrared radiation from the thermal excitation source; and
a controller coupled to the thermal excitation source and to the infrared camera, the controller configured to compare the first signal from the infrared camera with a first threshold to detect presence of the first type of foreign object debris material.

11. The system of claim 10 , further comprising a controllable nozzle coupled to an air source, the controllable nozzle directed at the surface, and wherein the controller is further configured to cause the controllable nozzle to direct air at the surface upon detection of foreign object debris material.

12. The system of claim 10 , further comprising a terminal coupled to the controller, the terminal including a display, and wherein the controller is further configured to provide an indication on the display upon detection of foreign object debris material.

13. The system of claim 10 , further comprising:
an ultraviolet light source configured to direct ultraviolet light across the surface;
an ultraviolet light camera configured to scan the surface and output a second signal proportional to reflected ultraviolet light reflected by at least one of the surface and a second type of foreign object debris material, the reflected ultraviolet light responsive to the ultraviolet light from the ultraviolet light source; and
wherein the controller is configured to compare the second signal from the ultraviolet light camera with a second threshold to detect presence of the second type of foreign object debris material.

14. The system of claim 13 , further comprising:
a visible light source configured to direct visible light across the surface;
a visible light camera configured to scan the surface and output a third signal proportional to reflected visible light reflected by at least one of the surface and a third type of foreign object debris material, the reflected visible light responsive to the visible light from the visible light source; and
wherein the controller is configured to compare the third signal from the visible light camera with a third threshold to detect presence of the third type of foreign object debris material.

15. The system of claim 10 , further comprising:
a visible light source configured to direct visible light across the surface;
a visible l

Assignees

• Boeing Co

Inventors

• Safai Morteza
• Thompson Jeffrey G

Classifications

• G01N2201/103

  Scanning by mechanical motion of stage · CPC title

• G01N21/8851

  Scan or image signal processing specially adapted therefor, e.g. for scan signal adjustment, for detecting different kinds of defects, for compensating for structures, markings, edges (G01N21/8806 and G01N21/93 - G01N21/95692 take precedence; optical measurement of dimensions G01B11/00; optical scanning G02B26/10; image transformation G06T3/00; computerised image enhancement G06T5/00; image processing per se for flaw detection G06T7/0002) · CPC title

• B08B5/02 Primary

  Cleaning by the force of jets, e.g. blowing-out cavities {(airguns or nozzles per se B05B1/005)} · CPC title

• G01N21/94

  Investigating contamination, e.g. dust (G01N21/85 takes precedence) · CPC title

• G01N2021/8472

  Investigation of composite materials · CPC title