IP Library Granted Patent US 11,534,986
Granted Patent B2
US 11,534,986 · App. 16/179,324 · Granted Dec 27, 2022

Composite structures constructed of wound tubular braiding

Inventor: Amol Ogale (Munich, DE)
Assignee: The Boeing Company
B29C70/222B29C53/005B29C53/566B29C53/60B29C53/824B29C53/84B29C70/347B29C70/443B29C70/462B29C70/465B29K2063/00B29K2071/00B29K2101/00B29K2105/0827B29K2105/0872B29K2307/04B29L2031/3076
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Quick Facts
Patent No.
US 11,534,986
App. No.
16/179,324
Granted
Dec 27, 2022
Kind
B2
Abstract

A system for constructing a composite structure includes a braiding machine, a winding tool and a forming machine. The composite structure is constructed of a wound tubular braiding. The wound tubular braiding is constructed of a biaxial or triaxial tubular braid of unidirectional tape.

Claims (25)

1. A method of forming a composite structure, the method comprising:

winding a tubular braiding around an outer surface of a winding tool to form a wound tubular braiding having stacked turns, the tubular braiding defining a central bore extending along a length therethrough; and

forming the wound tubular braiding into the composite structure by consolidating the stacked turns of the wound tubular braiding into flattened plies having a solid cross-section thereby eliminating the central bore.

2. The method of claim 1 , further comprising fabricating the tubular braiding from materials selected from the group consisting of: a unidirectional tape and a unidirectional tow.

3. The method of claim 2 , wherein the unidirectional tape is constructed from unidirectional fibers.

4. The method of claim 1 , further comprising winding the tubular braiding into a spiral pattern around the winding tool.

5. The method of claim 1 , further comprising slipping the unidirectional tape relative to one another without bending when the tubular braiding is wound around the winding tool.

6. The method of claim 1 , further comprising pre-impregnating the wound tubular braiding with a resin.

7. The method of claim 1 , further comprising applying heat while consolidating the wound tubular braiding.

8. The method of claim 7 , wherein the wound tubular braiding is heated to a resin melt temperature.

9. The method of claim 1 , wherein the unidirectional tape shear relative to one another without bending when consolidating the wound tubular braiding.

10. The method of claim 1 , wherein the tubular braiding has a biaxial braid.

11. The method of claim 1 , wherein the tubular braiding has a triaxial braid.

12. The method of claim 1 , further comprising winding the tubular braiding into a helical pattern around the winding tool.

13. The method of claim 1 , wherein the tubular braiding has a first free end and a second free end.

14. The method of claim 13 , wherein the first free end overlaps the second free end when the tubular braiding is wound around the winding tool.

15. The wound tubular braiding of claim 1 , wherein the tubular braiding wound around the winding tool is formed of a single length of the tubular braiding.

16. The method of claim 1 , wherein forming the wound tubular braiding into the composite structure includes placing the wound tubular braiding and the winding tool into a mold and consolidating the wound tubular braiding using heat and pressure.

17. A method of forming a composite structure, the method comprising:

winding a tubular braiding around an outer surface of a winding tool to form a wound tubular braiding having stacked turns, the tubular braiding defining a central bore extending along a length therethrough;

placing the wound tubular braiding and the winding tool into a mold; and

consolidating, using heat and pressure, the stacked turns of the wound tubular braiding within the mold into flattened plies having a solid cross-section thereby eliminating the central bore, to form the composite structure.

18. The method of claim 17 , wherein the winding tool includes an axis, and the tubular braiding is wound about the axis.

19. The method of claim 18 , wherein consolidating the wound tubular braiding on the winding tool to form the composite structure includes compacting the wound tubular braiding flat in a direction parallel to the axis.

20. The method of claim 19 , further comprising winding the tubular braiding into a helical pattern around the winding tool.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 5, 2018
From: OGALE, AMOL
To: THE BOEING COMPANY
Reel/Frame 047410/0602 →
Continuity (1)
Related Publication 20200139643A1 · May 7, 2020