IP Library › Granted Patent US 9,592,650
Granted Patent B2
US 9,592,650 · App. 14/252,764 · Granted Mar 14, 2017

Composite laminate including beta-reinforcing fibers

Inventor: Max U. Kismarton (Renton, WA)
Assignee: The Boeing Company
B32B5/12B29C65/562B29C65/564B29C66/474B29C66/524B29C66/721B29C66/72141B29C70/202B29C70/207B29C70/228B29C70/30B32B1/00B32B5/26B32B5/28B64C1/064B64C1/12B64C3/182B64C3/26B29C66/7212B29K2101/00B29K2307/00B29K2707/04B29L2031/3076B32B2250/20B32B2260/023B32B2260/046B32B2262/106B64C2001/0072Y02T50/433Y10T428/24124
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Quick Facts
Patent No.
US 9,592,650
App. No.
14/252,764
Granted
Mar 14, 2017
Kind
B2
Abstract

A composite laminate comprises a plurality of plies of reinforcing fibers. At least some of the plies have reinforcing fibers oriented at ±α with respect to an axis of primary loading, where α is between 2 and 12 degrees. At least some of the plies have reinforcing fibers oriented at ±β with respect to the axis of primary loading, where β is between 50 and 85 degrees.

Claims (20)

1. A composite laminate comprising a plurality of plies of reinforcing fibers; at least some of the plies having reinforcing fibers oriented at ±α with respect to an axis of primary loading, where α is between 2 and 12 degrees; at least some of the plies having reinforcing fibers oriented at ±β with respect to the axis of primary loading, where β is between 50 and 85 degrees.

2. The laminate of claim 1 , wherein α is between 2 and 8 degrees.

3. The laminate of claim 1 , wherein α is between 3 and 5 degrees.

4. The laminate of claim 1 , wherein the reinforcing fibers oriented at ±α constitute at least 50% of the total number of fibers.

5. The laminate of claim 1 , further comprising a polymer matrix, wherein the fibers include carbon fibers in a polymer matrix.

6. The laminate of claim 1 , wherein all fibers in the laminate consist of the fibers oriented at ±α and ±β; and wherein 20-30% of the total fibers are oriented at ±β to reach bearing strength levels similar to traditional 0/+45/−45/90 degree hard laminates.

7. A system comprising the laminate of claim 1 .

8. A composite beam comprising plies of α-reinforcing fibers oriented at ±α with respect to an axis of primary loading, where α is between 2 and 12 degrees; and plies having β-reinforcing fibers oriented at ±β with respect to the axis of primary loading, where β is between 50 and 85 degrees.

9. The beam of claim 8 , including a base and a web, at least one of the base and web including the plies of the α-reinforcing and the plies of the β-reinforcing fibers, at least 50% of the reinforcing fibers being the α-reinforcing fibers.

10. The beam of claim 8 , wherein the base has fastener apertures, whereby the α-reinforcing fibers in the base are oriented at ±α degrees to suppress or delay splitting caused by the fastener apertures.

11. The beam of claim 8 , wherein α is between 2 and 8 degrees.

12. The beam of claim 8 , wherein α is between 3 and 5 degrees.

13. The beam of claim 9 , wherein the β-reinforcing fibers are biased towards outer surfaces of the webs to increase stiffness in buckling and transverse bending.

14. The beam of claim 8 , further comprising a polymer matrix; wherein the α-reinforcing and the β-reinforcing fibers include carbon fibers embedded in the polymer matrix.

15. A system comprising the beam of claim 8 .

16. A system comprising a beam including a base and a web, the web including plies of reinforcing fibers for providing strength in tension and compression along an axis of primary loading, the web also including plies of reinforcing fibers oriented at ±β degrees with respect to the axis of primary loading, where β is between 50 and 85 degrees, wherein the fibers oriented at ±β degrees are biased towards outer surfaces of the web to increase stiffness in buckling and transverse loading.

17. The system of claim 16 , wherein the reinforcing fibers for providing strength in tension and compression are oriented at ±α with respect to the axis of primary loading, where α is between 2 and 12 degrees.

18. The system of claim 16 , wherein the reinforcing fibers are carbon fibers embedded in a polymer matrix.

19. The system of claim 16 , wherein the reinforcing fibers oriented at ±β degrees are biased towards an outer surface of the web to increase stiffness in buckling and transverse bending.

20. The system of claim 16 , wherein α is between 3 and 5 degrees.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2017
From: KISMARTON, MAX U.
To: THE BOEING COMPANY
Reel/Frame 041121/0432 →
Continuity (5)
Continuation 12897742 · Oct 4, 2010
Continuation In Part 11118594 · Apr 28, 2005
Continuation In Part 12340631 · Dec 19, 2008
Continuation In Part 11096727 · Mar 31, 2005
Related Publication 20140227479A1 · Aug 14, 2014