Mandrel forming for discrete wing skin stiffeners

Patent metadata

Field	Value
Publication number	US-10611101-B2
Application number	US-201715644906-A
Country	US
Kind code	B2
Filing date	Jul 10, 2017
Priority date	Nov 6, 2014
Publication date	Apr 7, 2020
Grant date	Apr 7, 2020

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 of forming a stiffener, comprising:
inserting one or more flexible mandrels into a channel of a tool having a three-dimensional contour;
placing a vacuum bag over the one or more flexible mandrels and the tool, wherein the one or more flexible mandrels are disposed between the vacuum hag and the tool;
applying vacuum pressure between the vacuum bag and the tool;
inserting a hardening substance into each of the one or more flexible mandrels;
creating one or more hardened mandrels by hardening the hardening substance while the one or more flexible mandrels are inserted in the one or more channels of the tool;
wrapping the one or more hardened mandrels at least partially with a material; and
forming the material into a stiffener.

2. The method of claim 1 , wherein the stiffener comprises a shape selected from the group consisting of an I-stiffener, a J-stiffener, and a blade stiffener.

3. The method of claim 1 , further comprising coupling the stiffener to a structure having a corresponding shape to the tool.

4. The method of claim 3 , wherein the stiffener is coupled to the structure with the one or more hardened mandrels remaining in place within the stiffener.

5. The method of claim 1 , further comprising placing a breathable material over the one or more flexible mandrels, wherein the breathable material is disposed between the one or more flexible mandrels and the vacuum bag.

6. The method of claim 1 , wherein the material that is wrapped around at least part of the one or more hardened mandrels comprises aluminum or a carbon composite material.

7. A method of forming a stiffener, comprising:
inserting one or more flexible mandrels into a channel of a tool having a three-dimensional contour;
placing a vacuum bag over the one or more flexible mandrels and the tool, wherein the one or more flexible mandrels are disposed between the vacuum bag and the tool;
applying vacuum pressure between the vacuum bag and the tool;
creating one or more hardened mandrels by hardening the one or more flexible mandrels while the one or more flexible mandrels are inserted in the one or more channels of the tool;
wrapping the one or more hardened mandrels at least partially with a material; and
forming the material into a stiffener.

8. The method of claim 7 , wherein the stiffener comprises a shape selected from the group consisting of an I-stiffener, a J-stiffener, and a blade stiffener.

9. The method of claim 7 , further comprising coupling the stiffener to a structure having a corresponding shape to the tool.

10. The method of claim 9 , wherein the stiffener is coupled to the structure with the one or more hardened mandrels remaining in place within the stiffener.

11. The method of claim 9 , further comprising placing a breathable material over the one or more flexible mandrels, wherein the breathable material is disposed between the one or more flexible mandrels and the vacuum bag.

12. The method of claim 7 , wherein creating the one or more hardened mandrels by hardening the one or more flexible mandrels comprises:
inserting a hardening substance either directly into cavities of the one or more flexible mandrels or inserting the hardening substance into a tube inserted in the cavities of the one or more flexible mandrels; and
hardening the hardening substance.

13. The method of claim 12 , wherein:
the one or more flexible mandrels are formed from a material that hardens through a heating process; and
creating the one or more hardened mandrels by hardening the one or more flexible mandrels comprises heating the one or more flexible mandrels.

14. A method comprising:
inserting one or more flexible mandrels into a channel of a tool, the tool comprising a three-dimensional contour corresponding to a structure;
securing the one or more flexible mandrels into the channel of the tool;
creating one or more hardened mandrels by hardening the one or more flexible mandrels while the one or more flexible mandrels are secured in the channel of the tool;
wrapping the one or more hardened mandrels at least partially with a material; and
forming the material into a stiffener.

15. The method of claim 14 , wherein the stiffener comprises a shape selected from the group consisting of an I-stiffener, J-stiffener, and a blade stiffener.

16. The method of claim 14 , further comprising coupling the stiffener to the structure.

17. The method of claim 16 , wherein the stiffener is coupled to the structure with the one or more hardened mandrels remaining in place within the stiffener.

18. The method of claim 14 , wherein creating, the one or more hardened mandrels by hardening the one or more flexible mandrels comprises:
inserting a hardening substance either directly into cavities of the one or more flexible mandrels or inserting the hardening substance into a tube inserted in the cavities of the one or more flexible mandrels; and
hardening the hardening substance.

19. The method of claim 14 , wherein:
the one or more flexible mandrels are formed from a material that hardens through a heating process; and
creating the one or more hardened mandrels by hardening the one or more flexible mandrels comprises heating the one or more flexible mandrels.

20. The method of claim 14 , wherein securing the one or more flexible mandrels into the channel of the tool comprises:
utilizing vacuum pressure to secure the one or more flexible mandrels into the channel of the tool; or
coupling the one or more flexible mandrels into the channel of the tool using an adhesive.

Assignees

• Lockheed Corp

Inventors

• Huddleston Nicholas Lee
• Ballester Jaime

Classifications

• B29K2309/08

  Glass · CPC title

• B29C70/70 Primary

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

• B64F5/10

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

• B29L2031/001

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