Composite structure and methods of forming thereof

Patent metadata

Field	Value
Publication number	US-9856008-B2
Application number	US-201414281456-A
Country	US
Kind code	B2
Filing date	May 19, 2014
Priority date	May 19, 2014
Publication date	Jan 2, 2018
Grant date	Jan 2, 2018

Abstract

A composite structure is provided. The composite structure includes a first stiffener, a second stiffener, and an intermediate structure positioned between the first and second stiffeners such that the first stiffener is coupled to a first side of the intermediate structure, and such that the second stiffener is coupled to a second opposing side of the intermediate structure. A first radius gap is defined at least partially between the first stiffener and the intermediate structure, and a second radius gap is defined at least partially between the second stiffener and the intermediate structure.

First claim

What is claimed is:

1. A composite structure comprising:
a first stiffener;
a second stiffener;
an intermediate structure positioned between said first and second stiffeners such that said first stiffener is coupled to a first side of said intermediate structure, and such that said second stiffener is coupled to a second opposing side of said intermediate structure;
a first radius gap defined at least partially between said first stiffener and said intermediate structure; and
a second radius gap defined at least partially between said second stiffener and said intermediate structure,
wherein said intermediate structure comprises a base portion positioned adjacent said first and second radius gaps and an elongated portion extending away from said base portion, said base portion and said elongated portion having different weights such that an uneven weight distribution is formed along a length of said first and second stiffeners.

2. The composite structure in accordance with claim 1 further comprising a filler structure positioned within each of said first and second radius gaps, wherein said filler structure has a cross-sectional shape that substantially corresponds to a cross-sectional shape of each said first and second radius gaps.

3. The composite structure in accordance with claim 2 , wherein said filler structure is integrally formed with said intermediate structure.

4. The composite structure in accordance with claim 1 , wherein said base portion comprises an internal cavity extending therethrough.

5. The composite structure in accordance with claim 1 , wherein said base portion is fabricated from a first material and said elongated portion is fabricated from a second material different from the first material.

6. The composite structure in accordance with claim 1 , wherein said base portion comprises at least one protrusion extending from an outer surface of said base portion, said at least one protrusion restricting movement of said intermediate structure relative to said first and second stiffeners.

7. An intermediate structure for use in defining a first radius gap and a second radius gap between stiffeners in a composite structure, said intermediate structure comprising:
a base portion coupled adjacent the first and second radius gaps within the composite structure, said base portion positioned to separate the first radius gap from the second radius gap; and
an elongated portion coupled to said base portion, said elongated portion extending away from said base portion to facilitate modifying a moment of inertia of the composite structure, and said base portion and said elongated portion having different weights such that an uneven weight distribution is formed along the composite structure.

8. The intermediate structure in accordance with claim 7 further comprising a filler structure positioned within each of the first and second radius gaps, wherein said filler structure has a cross-sectional shape that substantially corresponds to a cross-sectional shape of each the first and second radius gaps.

9. The intermediate structure in accordance with claim 8 , wherein said filler structure is integrally formed with said base portion.

10. The intermediate structure in accordance with claim 7 , wherein said base portion comprises an internal cavity extending therethrough.

11. The intermediate structure in accordance with claim 7 , wherein said base portion is fabricated from a first material and said elongated portion is fabricated from a second material different from the first material.

12. The intermediate structure in accordance with claim 7 , wherein said base portion comprises at least one protrusion extending from an outer surface of said base portion, said at least one protrusion restricting movement of said intermediate structure relative to the stiffeners.

13. A method of forming a composite structure, said method comprising:
coupling a first stiffener to a base structure of the composite structure;
coupling a second stiffener to the base structure; and
positioning an intermediate structure between the first and second stiffeners such that the intermediate structure separates a first radius gap defined at least partially between the first stiffener and the intermediate structure from a second radius gap defined at least partially between the second stiffener and the intermediate structure, wherein the intermediate structure includes a base portion positioned adjacent the first and second radius gaps and an elongated portion extending away from the base portion, the base portion and the elongated portion having different weights such that an uneven weight distribution is formed along a length of the first and second stiffeners.

14. The method in accordance with claim 13 further comprising positioning a filler structure within each of the first and second radius gaps.

15. The method in accordance with claim 14 , wherein positioning a filler structure comprises integrally forming the filler structure with the intermediate structure.

16. The method in accordance with claim 13 further comprising extending at least one protrusion from an outer surface of the intermediate structure, the at least one protrusion restricting movement of the intermediate structure relative to the first and second stiffeners.

17. The method in accordance with claim 13 further comprising defining an internal cavity that extends through the base portion.

18. The method in accordance with claim 13 further comprising:
forming the base portion from a first material; and
forming the elongated portion from a second material different from the first material.

19. The method in accordance with claim 13 , wherein positioning an intermediate structure comprises forming the intermediate structure from a two-piece assembly including the base portion and the elongated portion.

20. The composite structure in accordance with claim 1 , wherein said intermediate structure is a two-piece assembly comprising said base portion and said elongated portion.

Assignees

• Boeing Co

Inventors

• Cheng Jiangtian
• Vetter Derek Paul
• Woodard Patrick Alan
• Behzadpour Forouzan

Classifications

• B29C70/342

  using isostatic pressure · CPC title

• B29C70/865

  completely encapsulated · CPC title

• B29K2705/00

  Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts · CPC title

• B29C37/0082

  Mechanical anchoring (B29C66/303 takes precedence) · CPC title

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title