In-process vision detection of flaw and FOD characteristics

• US 8,770,248 B2
• Filed: 09/14/2012
• Issued: 07/08/2014
• Est. Priority Date: 11/24/2004
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hannebaum, Reed, Pollock, Tim, Englebart, Roger W.
• Primary Examiner(s): KOCH, GEORGE R
• Application Number:
  US13/619,637
• Publication Number:
  US 20130010309A1
• Time in Patent Office: 662 Days
• Field of Search: 156/351, 156/361, 156/64, 356/237.1, 356/237.3, 356/238.3
• US Class Current: 156/351
• CPC Class Codes: B29C 70/38 Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns application heads for tyres B29D30/28
• CPC Class Codes: G01N 2021/8472 Investigation of composite materials
• CPC Class Codes: G01N 21/89 in moving material, e.g. running paper or textiles G01N21/90, G01N21/91, G01N21/94 take precedence

Abstract

An inspection system (9) includes an idler wheel (61) that is coupled to a fabrication system (8) and is in contact with a backing layer (65) of an applied material (64), A rotation sensor (63) monitors the idler wheel (61) and generates a rotational signal. A controller (24) is coupled to the rotation sensor (63) and determines a characteristic of one or more flaws and FOD (19) on a composite structure (12) in response to the rotation signal.

Claims

1. An inspection system comprising:

an idler wheel coupled to a fabrication system and contacting a backing layer of an applied material;

a rotation sensor configured to monitor the idler wheel and to generate a rotational signal;

an illumination device configured to illuminate a portion of a composite structure to produce an illumination;

a detector configured to detect at least one flaw and FOD (foreign objects and debris) based on the illumination, the detector further configured to generate a flaw and FOD detection signal; and

a controller coupled to said rotation sensor and configured to determine at least one characteristic of the at least one flaw and FOD on the composite structure in response to said rotation signal and the flaw and FOD detection signal.

2. An inspection system as in claim 1 wherein an idler wheel is a non-pressure applying wheel.

3. An inspection system as in claim 1 wherein said rotation sensor is at least one of an encoder, an infrared sensor, and a rotary potentiometer.

4. An inspection system as in claim 1 wherein said controller is further configured to determine a longitudinal position of said at least one flaw and FOD in response to said rotation signal.

5. An inspection system as in claim 1 wherein said controller is further configured to determine a lateral position of said at least one flaw and FOD in response to cessation of said idler wheel.

6. An inspection system as in claim 1, wherein said illumination device is selected from at least one of an incandescent light a light emitting diode, a noble gas arc lamp, a metal arc lamp, a strobe, a fluorescent light an infrared light and a laser.

7. An inspection system as in claim 1, wherein said detector is selected from at least one of a camera, an infrared sensor, a visible light sensor, a visible light sensor with infrared-pass filtration, and a charged-coupled device.

8. An inspection system as in claim 1, wherein said detector is configured to detect at least one flaw and at least one FOD simultaneously.

9. An inspection system as in claim 1 wherein said controller is further configured to determine at least one of size, location, type, density-per-unit area, and cumulative defect width-per-unit area.

10. An inspection system for determining characteristics of flaws and FOD (foreign objects and debris) during the fabrication of a composite structure comprising:

a material collection device coupled to the fabrication system;

a take-up sensor coupled to the material collection device, the take-up sensor configured to monitor translation of a backing layer of a composite material, and to generate a take-up signal;

an illumination device configured to illuminate a portion of said composite structure to produce an illumination;

a detector configured to detect said at least one flaw and FOD and to generate a flaw and FOD detection signal based on the illumination; and

a controller coupled to said take-up sensor and configured to determine at least one characteristic of at least one flaw or FOD on the composite structure in response to said take-up signal and said flaw and FOD detection signal.

11. An inspection system as in claim 10 wherein said material collection device is selected from at least one of a material collection wheel, a take-up reel, and a collection container.

12. An inspection system as in claim 10 wherein said backing layer is a backing paper.

13. An inspection system as in claim 10 wherein said controller is further configured to determine at least one of size, location, type, density-per-unit area, and cumulative defect width-per-unit area.