IP Library Granted Patent US 7,293,737
Granted Patent B2
US 7,293,737 · App. 10/830,291 · Granted Nov 13, 2007

Co-cured stringers and associated mandrel and fabrication method

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 7,293,737
App. No.
10/830,291
Granted
Nov 13, 2007
Kind
B2
Abstract

A co-cured composite stringer and associated apparatus and method are provided. The co-cured composite stringer includes a stringer and a mandrel positioned within a channel defined in the stringer. A plurality of strips are positioned within an opening of the mandrel, and a substrate layer, such as aircraft skin, is positioned adjacent to the stringer. During application of the substrate layer to the stringer, the mandrel and plurality of strips support the stringer.

Claims (11)

1. A collapsible lay-up mandrel assembly comprising:

an elastic mandrel defining an opening therethrough, wherein the mandrel is configured to be deformed and return to its original shape; and

a plurality of strips positioned within the opening of the mandrel, wherein the plurality of strips are configured to be slidably positioned within, and removed from, the opening of the mandrel.

2. A collapsible lay-up mandrel assembly according to claim 1 , wherein the plurality of strips are stacked horizontally and vertically within the opening of the mandrel.

3. A collapsible lay-up mandrel assembly according to claim 1 , wherein the plurality of strips are positioned within the opening of the mandrel such that the strips substantially conform to the shape of the mandrel.

4. A collapsible lay-up mandrel assembly according to claim 1 , wherein the plurality of strips are pliable such that the strips are capable of bending to a desired contour and returning to their original shape.

5. A collapsible lay-up mandrel assembly according to claim 1 , wherein the each of the plurality of strips is rectangular in shape.

6. A collapsible lay-up mandrel assembly according to claim 1 , wherein the plurality of strips comprise a polymeric material.

7. A collapsible lay-up mandrel assembly according to claim 6 , wherein the plurality of strips comprise nylon.

8. A collapsible lay-up mandrel assembly according to claim 1 , wherein the mandrel and plurality of strips are capable of withstanding at least 90 psi of head pressure.

9. A collapsible lay-up mandrel assembly according to claim 1 , wherein the mandrel comprises an elastomeric material.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 22, 2004
From: ENGWALL, DWIGHT L.; MORROW, CHRISTOPHER J.
To: BOEING COMPANY, THE
Reel/Frame 015260/0133 →
Continuity (1)
Related Publication 20050230552A1 · Oct 20, 2005