Monitoring composite manufacturing and repair processes using chromatic films

Patent metadata

Field	Value
Publication number	US-9656453-B2
Application number	US-201615173718-A
Country	US
Kind code	B2
Filing date	Jun 6, 2016
Priority date	May 5, 2011
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

A composite structure is processed using heat and pressure. A chromatic film is placed in proximity to the composite structure and is used to monitor at least one of the temperature of the heat and the pressure during processing.

First claim

What is claimed is:

1. Apparatus for curing, via heat and pressure, a composite structure, such that the apparatus comprises:
a radiation source, a camera, and an image processor;
a tool adapted to receive a composite structure layup; and,
a chromatic film that comprises a size, configured to lay adjacent to an entire surface area of the composite structure layup, and structured to continuously monitor at least one of heat and pressure, to which the composite structure layup is subjected, such that the chromatic film comprises a dye integrated throughout the chromatic film that comprises a fluorescent characteristic that indicates:
responsive to an illumination from the radiation source, a fluorescent shift in the chromatic film mapped on an image from the image processor of a backscatter of the illumination from the chromatic film, such that the camera receives the backscatter and the image processor maps in real-time each change of temperature, across a tailored range of temperature, and each change of pressure, across a tailored range of pressure, in the chromatic film; and
in the image from the image processor, a value of at least one of: a heat, and a pressure, as being outside a range of preselected values during the curing of the composite structure layup.

2. The apparatus of claim 1 , wherein the chromatic film includes at least one of a thermochromatic dye, and a mechanochromatic dye.

3. The apparatus of claim 1 , wherein the chromatic film overlies and substantially covers an entire area of the composite structure.

4. The apparatus of claim 1 , wherein the chromatic film substantially surrounds a periphery of the composite structure.

5. The apparatus of claim 1 , further comprising
a vacuum bag adapted to be sealed over the composite structure layup for applying compaction pressure to the composite structure layup during curing, and
wherein the chromatic film is integrated with the vacuum bag.

6. The apparatus of claim 1 , further comprising:
a source of illumination for illuminating the chromatic film with light; and,
a camera for recording an image of the chromatic film.

7. A device, used in vacuum bag processing of a composite part to monitor a temperature and at least one additional process parameter, such that the device comprises:
a radiation source, a camera, and an image processor;
a chromatic film that comprises a dye integrated throughout the chromatic film that comprises a fluorescent characteristic and a size configured to:
lay adjacent to an entire surface area of a composite layup; and
indicate in an image from the image processor:
a backscatter from illumination from the radiation source that is received by the camera and indicates a fluorescent shift in the chromatic film; and
each change, across a tailored range of the temperature and a tailored range of the at least one additional process parameter, in the temperature and the at least one additional process parameter; and
whether, during the vacuum bag processing, at least one of: the temperature, and the at least one additional process parameter, outlays a preselected range of values.

8. The device of claim 7 , wherein the at least one additional process parameter comprises a pressure.

9. The device of claim 7 , wherein the chromatic film includes at least one of a thermochromatic dye, and a mechanochromatic dye respectively tailored to exhibit fluorescent shifts outside of preselected ranges of temperature and pressure.

10. The device of claim 7 , further comprising:
a vacuum bag, and
the chromatic film is bonded to the vacuum bag.

11. A manufacture configured to monitor, in real-time, at least one of: a pressure and a temperature of a composite layup throughout a curing the composite layup, such that the manufacture comprises:
a radiation source, a camera, and an image processor, and a material;
at least one of: a thermochromatic dye, and a mechanochromatic dye, integrated into an entire area of the material, such that the material covers an area, in proximity to an entire surface of the composite layup, and comprises a fluorescent characteristic configured to indicate in real-time;
each change, across the area, in the temperature of the material, via a fluorescent shift in the material in response to each change, across a tailored range of temperatures,
an image from the image processor of a backscatter from at least one of: an ultraviolet, and an infrared, illumination by the radiation source that is received by the camera of any thermochromatic dye integrated into the material, such that the image maps each change of the backscatter of the temperature and the pressure, of the composite layup during the curing.

12. The manufacture of claim 11 , further comprising a sheet of the material located over the entire area of the composite layup.

13. The manufacture of claim 11 , further comprising-at least one of: the temperature, and the pressure, comprising a desired range during curing of the composite layup.

14. The manufacture of claim 11 , further comprising the material connected to an entirety of a perimeter of the composite layup.

15. The manufacture of claim 11 , further comprising the material comprises at least one of: a caul sheet, a vacuum bag, and a coating.

16. The manufacture of claim 11 , further comprising a surface of the composite layup comprising at least one: a concave, and a convex shape.

17. The manufacture of claim 11 , further comprising:
the composite layup comprising a repair patch; and
a periphery of the repair patch covered with the material.

18. The manufacture of claim 11 , further comprising the material comprising at least one of: paper and plastic.

19. The manufacture of claim 11 , further comprising further comprising a caul sheet comprising the material.

Assignees

• Boeing Co

Inventors

• Georgeson Gary Ernest
• Bossi Richard H

Classifications

• G01M5/0091

  by using electromagnetic excitation or detection · CPC title

• B64F5/40

  Maintaining or repairing aircraft · CPC title

• G01L5/00

  Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes · CPC title

• B29C2035/0827

  using UV radiation · CPC title

• B32B33/00

  Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class · CPC title