IP Library Granted Patent US 7,691,222
Granted Patent B2
US 7,691,222 · App. 12/128,328 · Granted Apr 6, 2010

Flexible tooling method and apparatus

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 7,691,222
App. No.
12/128,328
Granted
Apr 6, 2010
Kind
B2
Abstract

A molding apparatus comprises an upper molding box, a lower mold box, an upper flexible membrane covering an opening of the upper mold box, a lower flexible membrane covering an opening of the lower mold box, a heating system located in the upper mold box, a set of ports located between the upper flexible membrane and the lower flexible membrane capable of being used to draw a vacuum between the upper flexible membrane and the lower flexible membrane, and a displacement system located in the lower mold box under the lower flexible membrane.

Claims (40)

1. A method for processing parts, the method comprising:

placing a master part between an upper flexible membrane and a lower flexible membrane in a molding apparatus;

applying a vacuum between the upper flexible membrane and the lower flexible membrane;

displacing a support material located under the lower flexible membrane to conform to a shape of the master part to form a conformed surface; and

stiffening the support material after the support material has conformed to the shape of the master part to form the conformed surface such that the support material and the lower flexible membrane substantially maintain the conformed surface;

compacting the support material such that the support material and the lower flexible membrane substantially maintain the conformed surface by applying a second vacuum to the support material.

2. The method of claim 1 further comprising:

applying pressure to the upper flexible membrane.

3. The method of claim 1 further comprising:

removing the master part.

4. The method of claim 3 further comprising:

placing a preform on the conformed surface;

placing a layer over the preform; and

applying the vacuum between the preform and the layer, wherein the layer conforms to a surface of the preform.

5. The method of claim 4 , further comprising:

placing a layer of a heat activated adhesive on the surface of the preform; and

applying heat to the heat activated adhesive.

6. The method of claim 5 further comprising:

releasing the vacuum applied between the preform and the layer after the heat activated adhesive has attached the layer to the preform.

7. The method of claim 4 , wherein the layer is a decorative layer.

8. The method of claim 1 , wherein the displacing step comprises:

agitating the support material; and

inflating a bladder located under the support material.

9. The method of claim 1 , wherein the support material comprises a plurality of spheres.

10. A method for processing aircraft parts, the method comprising:

placing a master part between an upper flexible membrane and a lower flexible membrane in a molding apparatus;

applying a vacuum between the upper flexible membrane and the lower flexible membrane to conform the upper flexible membrane and the lower flexible membrane to a mold shape of the master part;

displacing a support material located under the lower flexible membrane to conform to the mold shape of the master part to form a conformed surface by agitating the support material and inflating a bladder located under the support material the support material comprising a plurality of spheres;

applying pressure to the upper flexible membrane;

stiffening the support material after the support material has conformed to the mold shape of the master part to form the conformed surface by applying a second vacuum to the support material in which the second vacuum compacts the support material such that the support material and the lower flexible membrane substantially maintain the conformed surface;

removing the master part after the conformed surface has been formed and the support material has been stiffened;

placing a layer of a heat activated adhesive on the surface of a preform;

placing the preform on the conformed surface;

placing a decorative layer over the preform;

applying the vacuum between the preform and the decorative layer, wherein the decorative layer conforms to a surface of the preform;

applying heat to the heat activated adhesive; and

releasing the vacuum applied between the preform and the decorative layer after the heat activated adhesive has attached the decorative layer to the preform.

11. The method of claim 1 , wherein the molding apparatus is used to process parts.

12. The method of claim 1 , wherein the molding apparatus is used to conform layers to parts.

13. The method of claim 1 , wherein the upper flexible membrane and the lower flexible membrane conform to the shape of the master part.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 28, 2008
From: KUNTZ, MICHAEL P.; YOUNIE, MARK L.
To: THE BOEING COMPANY
Reel/Frame 021010/0278 →
Continuity (1)
Related Publication 20090295015A1 · Dec 3, 2009