Heated double diaphragm tool for decorative laminate application

• US 10,525,683 B2
• Filed: 11/08/2016
• Issued: 01/07/2020
• Est. Priority Date: 11/08/2016
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Cysewski, Sean Richard, Prudnick, Steven
• Primary Examiner(s): Schatz, Christopher T
• Assistant Examiner(s): Schaller, Cynthia L
• Application Number:
  US15/346,371
• Publication Number:
  US 20180126715A1
• Time in Patent Office: 1,155 Days
• CPC Class Codes: B32B 2607/00 Walls, panels
• CPC Class Codes: B32B 37/06 characterised by the heating method
• CPC Class Codes: B32B 37/1018 using only vacuum
• CPC Class Codes: B32B 37/12 characterised by using adhesives

Abstract

A panel laminator includes a first frame defining an outer boundary, the first frame operable to support a panel to be laminated and a first flexible diaphragm supported by the first frame to cover the outer boundary. The laminator includes a second frame sized and shaped to conform to the first frame along the outer boundary and a second flexible diaphragm supported by the second frame to match the outer boundary. The laminator includes a passage fluidly connected to the space between the first and second flexible diaphragms, with the passage configured to be coupled to a vacuum system in order to remove air from the space between the first and second flexible diaphragms during a lamination process. The first frame and the second frame are configured to rotate as a unit between a first, generally horizontal, orientation and a second, generally vertical, orientation.

Claims

1. A panel laminator comprising:

a first frame defining an outer boundary, the first frame operable to support a panel to be laminated;

a first flexible diaphragm supported by the first frame to cover the outer boundary;

a second frame sized and shaped to conform to the first frame along the outer boundary;

a second flexible diaphragm supported by the second frame to match the outer boundary;

a first heating blanket attached to the first frame distal from the first flexible diaphragm to create an isolated heated environment between the first heating blanket and the first flexible diaphragm, and enclosed by the first frame wherein the first flexible diaphragm and the first heating blanket are separated by a plurality of support bars spanning between first and second lateral portions of the first frame;

a second heating blanket attached to the second frame distal from the second flexible diaphragm to create an isolated heated environment between the second heating blanket and the second flexible diaphragm, and enclosed by the second frame;

a permeable layer positioned between the first flexible diaphragm and the second flexible diaphragm; and

a vacuum port operable to connect a vacuum source to the permeable layer between the first flexible diaphragm and the second flexible diaphragm.

2. The panel laminator of claim 1, further comprising:

a first insulating layer positioned so that the first heating blanket is positioned between the first insulating layer and the first flexible diaphragm; and

a second insulating layer positioned so that the second heating blanket is positioned between the second insulating layer and the second flexible diaphragm.

3. The panel laminator of claim 1, wherein the second frame is coupled to the first frame to provide for angular separation of the second frame relative to the first frame.

4. The panel laminator of claim 1, further comprising:

a first rotatable connection on a first edge portion of the first frame; and

a second rotatable connection on a second edge portion of the first frame;

wherein the first rotatable connection and the second rotatable connection are configured so that the first frame and the second frame are configured to rotate as a unit when secured to one another between a first, generally horizontal, orientation and a second, generally vertical, orientation.

5. The panel laminator of claim 1, wherein the panel has a non-planar shape, the first frame has a three-dimensional shape which corresponds to the non-planar shape of the panel, the second frame has a three-dimensional shape which corresponds to the non-planar shape of the panel, and the three-dimensional shape of the first frame is complementary to the three-dimensional shape of the second frame.

6. The panel laminator of claim 5, further comprising:

a first coupler attached to a first edge portion of the first frame at a first connection point located a first distance away from a rotation axis of the panel laminator; and

a second coupler attached to a second edge portion of the first frame at a second connection point located a second distance away from the rotation axis of the panel laminator.

7. The panel laminator of claim 1, wherein the first heating blanket is at least partially retained by a plurality of slats spanning lateral portions of a first insulation layer.

8. The panel laminator of claim 1, wherein at least one of the plurality of support bars is oriented at a different angle relative to another of the plurality of support bars corresponding to different planar sections of the panel.

9. The panel laminator of claim 7, wherein each support bar of the plurality of support bars is aligned with a slat of the plurality of slats.

10. An apparatus for laminating a panel, the apparatus comprising:

a first flexible diaphragm;

a first frame bound to the first flexible diaphragm;

a second flexible diaphragm;

a second frame bound to the second flexible diaphragm, the second frame configured to be coupled to the first frame so that the first flexible diaphragm is proximate the second flexible diaphragm, thereby creating a space between the first flexible diaphragm and the second flexible diaphragm;

a passage fluidly connected to the space between the first flexible diaphragm and the second flexible diaphragm, the passage configured to be coupled to a vacuum system in order to remove air from the space between the first flexible diaphragm and the second flexible diaphragm during a lamination process; and

a diaphragm support configured to (a) provide support for the first flexible diaphragm against gravity prior to activation of the vacuum system and (b) be spaced from the first flexible diaphragm after activation of the vacuum system and during the lamination process, wherein the diaphragm support includes a plurality of support bars spanning between first and second lateral portions of the first frame and wherein at least one of the support bars has a three-dimensional shape configured to correspond to a non-planar shape of a panel to be received in a space between the first flexible diaphragm and the second flexible diaphragm;

wherein the first frame and the second frame are configured to rotate as a unit between a first, generally horizontal, orientation and a second, generally vertical, orientation.

11. The apparatus of claim 10, further comprising:

a first heating blanket attached to the first frame distal from the first flexible diaphragm to create an isolated heated environment between the first heating blanket and the first flexible diaphragm, and enclosed by the first frame; and

a second heating blanket attached to the second frame distal from the second flexible diaphragm to create an isolated heated environment between the second heating blanket and the second flexible diaphragm, and enclosed by the second frame.

12. The apparatus of claim 10, wherein the first flexible diaphragm is configured to exert a force on a first major face of a panel disposed in the space between the first flexible diaphragm and the second flexible diaphragm and the second flexible diaphragm is configured to exert a force on a second major face of the panel when air has been removed from the space between the first flexible diaphragm and the second flexible diaphragm during the lamination process.

13. The apparatus of claim 10, wherein the diaphragm support spans an area enclosed by the first frame.

14. A method of laminating a panel, the method comprising:

providing a panel and a laminate to be applied to the panel;

providing a first flexible diaphragm bound to a first frame and a second flexible diaphragm bound to a second frame;

securing the first frame to the second frame so that the panel and the laminate to be applied to the panel are enclosed within a space between the first flexible diaphragm and the second flexible diaphragm;

evacuating air from the space between the first flexible diaphragm and the second flexible diaphragm; and

heating an ambient environment around the first flexible diaphragm and the second flexible diaphragm, the panel, and the laminate by activating a first heating blanket attached to the first frame distal from the first flexible diaphragm and a second heating blanket attached to the second frame distal from the second flexible diaphragm, wherein the first flexible diaphragm and the first heating blanket are separated by a plurality of support bars spanning between first and second lateral portions of the first frame.

15. The method of claim 14, wherein providing a panel and a laminate to be applied to the panel includes providing a first laminate to be applied to a first major face of the panel and providing a second laminate to be applied to a second major face of the panel.

16. The method of claim 14, wherein heating an ambient environment around the first flexible diaphragm and the second flexible diaphragm, the panel, and the laminate includes heating a first isolated environment between the first heating blanket and the first flexible diaphragm and heating a second isolated environment between the second heating blanket and the second flexible diaphragm.

17. The method of claim 14, wherein providing a first flexible diaphragm bound to a first frame includes supporting the first flexible diaphragm against gravity by a diaphragm support coupled to the first frame, the diaphragm support configured to support the first flexible diaphragm against gravity prior to evacuating air from the space between the first flexible diaphragm and the second flexible diaphragm.

18. The method of claim 17, wherein the diaphragm support is configured to be spaced apart from the first flexible diaphragm after evacuating air from the space between the first flexible diaphragm and the second flexible diaphragm.

19. The method of claim 14, further comprising:

reducing a footprint of the first frame and the second frame by rotating the first frame and the second frame as secured to one another about a generally horizontal rotation axis.

20. The method of claim 19, wherein reducing a footprint of the first frame and the second frame includes coupling a first edge portion of the first frame to an apparatus support and coupling a second edge portion of the first frame to an apparatus support, the second edge portion opposite the first edge portion, and wherein the first edge portion includes a first connection point spaced a first distance away from the generally horizontal rotation axis and the second edge portion includes a second connection point spaced a second distance away from the generally horizontal rotation axis, the second distance different than the first distance.