IP Library › Granted Patent US 11,141,927
Granted Patent B2
US 11,141,927 · App. 16/458,582 · Granted Oct 12, 2021

Hybrid braided composite parts

Inventors: Amol Ogale (Munich, DE); Karl R Bernetich (Wilmington, DE)
Assignee: The Boeing Company
B29C65/3636B29C65/3656B29C66/73752D04C1/02D04C1/06D04C3/48B29C66/434
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Quick Facts
Patent No.
US 11,141,927
App. No.
16/458,582
Granted
Oct 12, 2021
Kind
B2
Abstract

Systems and methods are provided for fabricating a hybrid composite part. A method includes braiding a first set of fibers to form a weave having a closed cross-sectional shape, braiding a second set of fibers into the weave that are chemically distinct from the first set of fibers, impregnating the weave with a resin, and hardening the resin within the weave to form a hybrid composite part.

Claims (47)

1. A method for induction welding a composite part, the method comprising:

acquiring a first composite part that includes fibers impregnated with a thermoplastic;

acquiring a second composite part that includes braided electrically conductive fibers and braided electrically insulating fibers impregnated with the thermoplastic;

placing the first composite part in contact with the second composite part at a location occupied by the electrically conductive fibers; and

induction welding the first composite part to the second composite part at the location.

2. The method of claim 1 wherein:

the first composite part comprises a tube having a first diameter, and the second composite part comprises a tube having a second diameter larger than the first diameter.

3. The method of claim 2 wherein:

the placing comprises nesting the first composite part within the second composite part, such that a circumference of the first composite part contacts the second composite part.

4. The method of claim 1 wherein:

the first composite part comprises a tube having a first diameter, and the second composite part comprises a tube having a second diameter smaller than the first diameter.

5. The method of claim 4 wherein:

the placing comprises nesting the second composite part within the first composite part, such that a circumference of the second composite part contacts the first composite part.

6. The method of claim 1 wherein:

the induction welding is performed by orbiting an induction coil around the second composite part.

7. The method of claim 1 wherein:

the induction welding is performed by rotating the second composite part.

8. The method of claim 1 wherein:

induction welding comprises exposing electrically conductive fibers arranged at an exterior of the second composite part to a magnetic field.

9. The method of claim 1 wherein:

induction welding comprises exposing electrically conductive fibers, arranged at an inner surface of the second composite part that defines a hollow portion, to a magnetic field.

10. The method of claim 1 wherein:

the insulating fibers comprise glass fibers.

11. The method of claim 1 wherein:

the electrically conductive fibers comprise carbon fibers.

12. The method of claim 1 wherein:

the electrically conductive fibers form a portion of a Faraday cage.

13. The method of claim 1 wherein:

induction welding the first composite part to the second composite part comprises commingling thermoplastic in the first composite part with thermoplastic in the second composite part.

14. A method for fabrication comprising:

providing a first composite part that includes fibers impregnated with a thermoplastic;

providing a second composite part that includes braided electrically conductive fibers and braided electrically insulating fibers impregnated with the thermoplastic;

holding the second composite part in contact with the first composite part at a location occupied by the electrically conductive fibers;

orbiting an induction coil around the second composite part; and

generating a magnetic field at the induction coil while the induction coil is orbiting.

15. The method of claim 14 wherein:

the first composite part comprises a tube having a first diameter, the second composite part comprises a tube having a second diameter larger than the first diameter, and the first composite part is nested within the second composite part.

16. The method of claim 14 wherein:

the first composite part comprises a tube having a first diameter, the second composite part comprises a tube having a second diameter smaller than the first diameter, and the second composite part is nested within the first composite part.

17. The method of claim 14 wherein:

the first composite part and the second composite part form a longitudinal lap splice.

18. The method of claim 14 wherein:

the electrically insulating fibers comprise glass fibers.

19. The method of claim 14 wherein:

the electrically conductive fibers comprise carbon fibers.

20. The method of claim 14 wherein:

the electrically conductive fibers form a portion of a Faraday cage.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 1, 2019
From: OGALE, AMOL; BERNETICH, KARL R
To: THE BOEING COMPANY
Reel/Frame 049641/0241 →
Continuity (1)
Related Publication 20210001564A1 · Jan 7, 2021