Composite laminated structures and methods for manufacturing and using the same

Patent metadata

Field	Value
Publication number	US-9296174-B2
Application number	US-201113272139-A
Country	US
Kind code	B2
Filing date	Oct 12, 2011
Priority date	Jan 12, 2011
Publication date	Mar 29, 2016
Grant date	Mar 29, 2016

Abstract

Variously configured sub-laminate modules are provided, which comprise at least a first ply and a second ply, the first ply comprising fibers extending in a first orientation, the second ply comprising fibers extending in a second orientation. The second orientation is offset relative to the first orientation, which offset defines an acute angle between the two orientations. The acute angle is less than 90 degrees and in at least one embodiment, the acute angle is approximately 25°. In certain embodiments, the acute angle further defines an unbalanced structure of the sub-laminate module. In certain embodiments, the first and second plies may be further secured relative to one another in a non-crimped configuration. Composite laminated structures formed from various embodiments of the sub-laminate modules are also provided, at least some of which may be homogenized. Various methods of manufacturing the sub-laminate modules and the composite laminated structures are also provided.

First claim

That which is claimed:

1. A sub-laminate module for use in forming a composite laminated structure, the sub-laminate module consisting of:
a primary longitudinal axis corresponding to a primary load-bearing axis of the sub-laminate module;
a first ply comprising fibers extending in a first orientation;
a second ply comprising fibers extending in a second orientation, the second orientation being offset relative to the first orientation; and
an acute angle defined by the relative offset between the first orientation and the second orientation, the acute angle being less than 90° and defining an unbalanced structure of the sub-laminate module,
wherein:
the first orientation is aligned with the primary longitudinal axis of the sub-laminate module such that the first ply is aligned with the primary load-bearing axis of the sub-laminate module;
the second orientation is offset relative to the first orientation and the primary longitudinal axis such that the relative offset corresponds to the acute angle and defines the unbalanced structure of the sub-laminate module; and
the first ply and the second ply are secured relative to one another via a plurality of transversely oriented stitches, the plurality of transverse stitches being oriented substantially perpendicular relative to the primary longitudinal axis of the sub-laminate module so as to at least in part define a non-crimped configuration.

2. The sub-laminate module of claim 1 , wherein the acute angle is less than 45°.

3. The sub-laminate module of claim 1 , wherein the acute angle is within a range from about 10° to about 40°.

4. The sub-laminate module of claim 3 , wherein the acute angle is within a range of from about 15° to about 30°.

5. The sub-laminate module of claim 4 , wherein the acute angle is approximately 25°.

6. The sub-laminate module of claim 1 , wherein the fibers of the first and second plies comprise carbon fibers.

7. The sub-laminate module of claim 1 , wherein the fibers of the first ply comprise carbon fibers and the fibers of the second ply comprise glass fibers, so as to form a hybrid composition.

8. The sub-laminate module of claim 1 , wherein the sub-laminate module is folded in half on itself, relative to an axis extending in the second orientation, such that:
the first ply forms a first and a fourth ply layer; and
the second ply forms a second and a third ply layer,
wherein the fourth ply layer comprises fibers extending in the first orientation and the third ply layer comprises fibers extending in a third orientation, the third orientation being opposite that of the second orientation relative to the primary load-bearing axis of the sub-laminate module.

9. The sub-laminate module of claim 1 , wherein at least the first ply has a thickness within a range of from about 0.020 millimeters to about 0.080 millimeters.

10. The sub-laminate module of claim 1 , wherein at least the first ply has a thickness of approximately 0.0625 millimeters and a weight of approximately 75 g/m 2 .

11. A sub-laminate module for use in forming a composite laminate, the sub-laminate module consisting of:
a primary longitudinal axis corresponding to a primary load-bearing axis of the sub-laminate module;
a first ply comprising fibers extending in a first orientation, the fibers of the first ply comprising a plurality of spread tows lying adjacent to each other;
a second ply comprising fibers extending in a second orientation, the fibers of the second ply comprising a plurality of spread tows lying adjacent to each other, the second orientation being offset relative to the first orientation; and
an acute angle defined by the relative offset between the first and the second orientations, the acute angle being less than 90° and defining an unbalanced structure of the sub-laminate layer,
wherein:
the first orientation is aligned with the primary longitudinal axis of the sub-laminate module such that the first ply is aligned with the primary load-bearing axis of the sub-laminate module;
the second orientation is offset relative to the first orientation and the primary longitudinal axis such that the relative offset corresponds to the acute angle and defines the unbalanced structure of the sub-laminate module; and
the fibers of the first and the second plies are secured relative to one another via a plurality of stitches.

12. The sub-laminate module of claim 11 , wherein the acute angle is within a range of from about 10° to about 40°.

13. The sub-laminate module of claim 12 , wherein the acute angle is approximately 25°.

14. The sub-laminate module of claim 11 , wherein the fibers of the first and second plies comprise carbon fibers.

15. The sub-laminate module of claim 14 , wherein the fibers of the first ply comprise carbon fibers and the fibers of the second ply comprise glass fibers, so as to form a hybrid composition.

16. The sub-laminate module of claim 11 , wherein the sub-laminate module is folded in half on itself, relative to an axis extending in the second orientation, such that:
the first ply forms a first and a fourth ply layer, the fourth ply layer comprising a plurality of spread tows lying adjacent to each other; and
the second ply forms a second and a third ply layer, the third ply layer comprising a plurality of spread tows lying adjacent to each other,
wherein the fourth ply layer comprises fibers extending in the first orientation and the third ply layer comprises fibers extending in a third orientation, the third orientation being opposite that of the second orientation relative to the primary load-bearing axis of the sub-laminate module.

17. The sub-laminate module of claim 11 , wherein at least the first ply has a thickness of approximately 0.0625 millimeters and a weight of approximately 75 g/m 2 .

18. A composite laminated structure, the composite laminated structure comprising:
a plurality of sub-laminate modules, each module consisting of:
a primary longitudinal axis corresponding to a primary load-bearing axis of the sub-laminate module;
a first ply comprising fibers extending in a first orientation;
a second ply comprising fibers extending in a second orientation, the second orientation being offset relative to the first orientation; and
an acute angle defined by the relative offset between the first orientation and the second orientation, the acute angle being less than 90° and defining an unbalanced structure of the sub-laminate module,
wherein;
the first orientation is aligned with the primary longitudinal axis of the sub-laminate module such that the first ply is aligned with the primary load-bearing axis of the sub-laminate module;
the second orientation is offset relative to the first orientation and the primary longitudinal axis such that the relative offset corresponds to the acute angle and defines the unbalanced structure of the sub-laminate module; and
the first ply and the second ply are secured relative to one another via a plurality of transversely oriented stitches, the plurality of transverse stitches being oriented substantially perpendicular relative to the primary longitudinal axis of the sub-laminate module so as to at least in part define a non-crimped configuration.

19. The composite laminated structure of claim 18 , wherein each of the plurality of sub-laminate modules has a thickness within a range of from about 0.040 millimeters to about 0.080 millimeters.

20. The composite laminated structure of claim 18 , wherein the structure comprises at least sixteen sub-laminate modul

Assignees

• Tsai Steven W
• Cognet Michel
• Sanial Philippe
• Cie Chomarat
• Univ Leland Stanford Junior

Inventors

• Tsai Steven W
• Cognet Michel
• Sanial Philippe

Classifications

• B29K2105/0881

  unidirectional · CPC title

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title

• Y10T428/24124

  Fibers · CPC title

• B29K2307/04

  Carbon · CPC title

• B32B5/28

  impregnated with or embedded in a plastic substance {(not used)} · CPC title