Mandrel forming for discrete wing skin stiffeners

Patent metadata

Field	Value
Publication number	US-9701070-B2
Application number	US-201414534747-A
Country	US
Kind code	B2
Filing date	Nov 6, 2014
Priority date	Nov 6, 2014
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

In one embodiment, a stiffener may be formed by inserting a plurality of flexible mandrels into a channel of a tool having a three-dimensional contour, placing a vacuum bag over the flexible mandrels and the tool, with the mandrels disposed between the vacuum bag and the tool, and applying vacuum pressure between the vacuum bag and the tool. A hardening substance may be inserted into each of the plurality of flexible mandrels and then may be hardened while the plurality of mandrels are inserted in the one or more channels of the tool. Finally, the mandrels may be wrapped with a stiffener material with stiffeners being formed from the stiffener material.

First claim

What is claimed is:

1. A method for forming panel stiffeners, comprising:
inserting one or more flexible mandrels into each of one or more channels of a tool having a three-dimensional contour, the one or more flexible mandrels being composed of silicone rubber;
hardening the flexible mandrels while inserted in the one or more channels of the tool; and
forming stiffeners using the hardened one or more mandrels.

2. The method of claim 1 , wherein hardening the flexible mandrels while inserted in the one or more channels comprises inserting a hardening substance into the flexible mandrels.

3. The method of claim 2 , wherein inserting a hardening substance into the flexible mandrels comprises applying vacuum pressure at one end of the flexible mandrels to draw the hardening substance into the mandrel.

4. A method for forming panel stiffeners, comprising:
inserting one or more flexible mandrels into each of one or more channels of a tool having a three-dimensional contour, wherein the tool is composed of foam;
hardening the flexible mandrels while inserted in the one or more channels of the tool; and
forming stiffeners using the hardened one or more mandrels.

5. The method of claim 1 , wherein forming stiffeners using the hardened one or more mandrels comprises:
wrapping the mandrels with a stiffener material; and
forming the stiffener material into a stiffener shape.

6. The method of claim 5 , wherein the stiffener shape is selected from the group consisting of an I-stiffener, a J-stiffener, and a blade stiffener.

7. The method of claim 1 , further comprising:
placing a vacuum bag over the flexible mandrels and the tool, wherein the mandrels are disposed between the vacuum bag and the tool; and
applying vacuum pressure between the vacuum bag and the tool.

8. The method of claim 7 , further comprising placing a breathable material over the flexible mandrels, wherein the breathable material is disposed between the flexible mandrels and the vacuum bag.

9. The method of claim 1 , wherein the tool is formed using a panel having a three-dimensional contour, and the method further comprises coupling the stiffeners to the panel.

10. The method of claim 4 , wherein hardening the flexible mandrels while inserted in the one or more channels comprises inserting a hardening substance into the flexible mandrels.

11. The method of claim 10 , wherein inserting a hardening substance into the flexible mandrels comprises applying vacuum pressure at one end of the flexible mandrels to draw the hardening substance into the mandrel.

12. The method of claim 4 , wherein forming stiffeners using the hardened one or more mandrels comprises:
wrapping the mandrels with a stiffener material; and
forming the stiffener material into a stiffener shape.

13. The method of claim 12 , wherein the stiffener shape is selected from the group consisting of an I-stiffener, a J-stiffener, and a blade stiffener.

14. The method of claim 4 , further comprising:
placing a vacuum bag over the flexible mandrels and the tool, wherein the mandrels are disposed between the vacuum bag and the tool; and
applying vacuum pressure between the vacuum bag and the tool.

15. The method of claim 14 , further comprising placing a breathable material over the flexible mandrels, wherein the breathable material is disposed between the flexible mandrels and the vacuum bag.

16. The method of claim 4 , wherein the tool is formed using a panel having a three-dimensional contour, and the method further comprises coupling the stiffeners to the panel.

Assignees

• Huddleston Nicholas Lee
• Ballester Jaime
• Lockheed Corp

Inventors

• Huddleston Nicholas Lee
• Ballester Jaime

Classifications

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B29L2031/001

  Profiled members, e.g. beams, sections · CPC title

• B29K2683/00

  Use of polymers having silicon, with or without sulfur, nitrogen, oxygen or carbon only, in the main chain, for preformed parts, e.g. for inserts · CPC title

• B29K2309/08

  Glass · CPC title

• B29C70/70 Primary

  Completely encapsulating inserts {(B29C70/86 takes precedence)} · CPC title