IP Library Granted Patent US 10,357,924
Granted Patent B2
US 10,357,924 · App. 14/835,323 · Granted Jul 23, 2019

Composite feedstock strips for additive manufacturing and methods of forming thereof

Inventors: John C. Waldrop, III (St. Peters, MO); Michael W. Hayes (Belleville, IL); Gregory James Schoepen Hickman (University City, MO)
Assignee: The Boeing Company
B29C70/545B29C70/20B29C70/504B29C64/106B29K2071/00B29K2081/06B29K2105/106B29K2105/253B29L2031/3076B33Y10/00B33Y70/00
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Quick Facts
Patent No.
US 10,357,924
App. No.
14/835,323
Granted
Jul 23, 2019
Kind
B2
Abstract

Provided are composite feedstock strips for additive manufacturing and methods of forming such strips. A strip may include continuous fibers extending parallel to the principal axis of the strip. The cross-sectional distribution of these continuous fibers may be uneven. Specifically, the fibers may be concentrated near the center of the strip and may be positioned away from at least some portions of the strip surface. A strip may be formed by laminating a layup of one or more fiber-containing plies and one or more of resin plies. The position of the different types of plies in the layup is used to control distribution of the fibers and other materials within the strip. The laminated sheet is slit into multiple strips in a direction parallel to the continuous fibers. The cross-sectional profile of the slit strips may be later changed without disturbing orientation of the continuous fibers.

Claims (35)

1. A method of forming composite feedstock strips for additive manufacturing, the method comprising:

forming a layup, comprising one or more fiber containing plies and one or more of resin plies,

all of continuous fibers in all of the one or more fiber containing plies, forming the layup, being parallel to each other,

forming the layup comprises varying a volumetric fraction of the continuous fibers within the layup throughout a thickness of the layup;

laminating the layup thereby forming a laminated sheet, a volumetric fraction of the continuous fibers within the laminated sheet being greater at a center of the laminated sheet along the thickness than at one of surfaces of the laminated sheet; and

slitting the laminated sheet into the composite feedstock strips, slitting being performed along a direction parallel to all of the continuous fibers within the laminated sheet thereby preserving continuity of a majority of the continuous fibers along a full length of the composite feedstock strips.

2. The method of claim 1 , wherein a portion of the laminated sheet forming the one of the surfaces of the laminated sheet is free from the continuous fibers.

3. The method of claim 1 , wherein a cross-sectional profile of each of the composite feedstock strips is a square.

4. The method of claim 1 , wherein all of continuous fibers in each of the composite feedstock strips are parallel to a primary axis of that composite feedstock strip.

5. The method of claim 1 , further comprising changing a cross-sectional profile of each of the composite feedstock strips.

6. A method of forming composite feedstock strips for additive manufacturing, the method comprising:

forming a layup, comprising one or more fiber containing plies and one or more of resin plies,

all of continuous fibers in all of the one or more fiber containing plies, forming the layup, being parallel to each other;

laminating the layup thereby forming a laminated sheet; and

slitting the laminated sheet into the composite feedstock strips,

slitting being performed along a direction parallel to all of the continuous fibers within the laminated sheet thereby preserving continuity of a majority of the continuous fibers along a full length of the composite feedstock strips; and

changing a cross-sectional profile of each of the composite feedstock strips, wherein the cross-sectional profile of each of the composite feedstock strips is changed to a circle.

7. The method of claim 6 , wherein changing the cross-sectional profile of each of the composite feedstock strips comprises heating each of the composite feedstock strips and redistributing a material away from corners of the cross-sectional profile.

8. The method of claim 7 , wherein position of the continuous fibers within each of the composite feedstock strips is retained while redistributing the material away from the corners of the cross-sectional profile.

9. The method of claim 1 , wherein at least one outer ply of the layup is one of the one or more resin plies.

10. The method of claim 1 , wherein the one or more resin plies comprise one or more materials selected from the group consisting of polyethersulfone (PES), polyphenylsulfone (PPS), polyetheretherketone (PEEK), polyetherketoneketone (PEKK), polyetherimide (PEI), and thermoplastic polyimide (TPI).

11. The method of claim 1 , wherein the one or more resin plies comprise polyethersulfone (PES).

12. The method of claim 1 , wherein the one or more fiber containing plies comprise one or more materials selected from the group consisting of polyethersulfone (PES), polyphenylsulfone (PPS), polyetheretherketone (PEEK), polyetherketoneketone (PEKK), and polyetherimide (PEI).

13. A method of forming composite feedstock strips for additive manufacturing, the method comprising:

forming a layup, comprising one or more fiber containing plies and one or more of resin plies,

all of continuous fibers in all of the one or more fiber containing plies, forming the layup, being parallel to each other,

the one or more fiber containing plies comprising polyetherketoneketone (PEKK);

laminating the layup thereby forming a laminated sheet; and

slitting the laminated sheet into the composite feedstock strips,

slitting being performed along a direction parallel to all of the continuous fibers within the laminated sheet thereby preserving continuity of a majority of the continuous fibers along a full length of the composite feedstock strips.

14. The method of claim 1 , wherein the composite feedstock strips have a principal cross-sectional dimension of less than about 0.050 inches.

15. The method of claim 1 , wherein forming layup and laminating sheet is performed in a roll-to-roll process.

16. The method of claim 1 , wherein slitting the laminated sheet into the composite feedstock strips is performed in a roll-to-roll process.

17. The method of claim 1 , wherein the volumetric fraction of the continuous fibers within the laminated sheet is greater at the center of the laminated sheet than both surfaces of the laminated sheet.

18. The method of claim 17 , wherein a profile of the volumetric fraction of the continuous fibers within the laminated sheet is symmetric with respect to the center of the laminated sheet.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 25, 2015
From: WALDROP, JOHN C., III; HAYES, MICHAEL W.; SCHOEPEN HICKMAN, GREGORY JAMES
To: THE BOEING COMPANY
Reel/Frame 036457/0197 →
Continuity (1)
Related Publication 20170057165A1 · Mar 2, 2017
Cited By (2)
US 12,242,911 US 12,389,551