Granted Patent B2

US 12,195,895 · App. 18/048,701 · Granted Jan 14, 2025

Inventors: Jacquelynn Xueting Tian (Melbourne, AU); Christopher Alan Howe (Albert Park, AU); Adrian Paul Mouritz (Melbourne, AU); Michelle Louise Gee (Bundoora, AU); Stuart Arthur Bateman (Melbourne, AU)

Assignee: The Boeing Company

D04C1/02D10B2101/12D10B2505/12

Abstract

Claims (39)

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

forming a braided carbon structure by braiding together carbon filaments and thermoplastic filaments;

forming and stabilizing a braided carbon preform by softening the thermoplastic filaments and reducing a thickness of the braided carbon structure, by applying heat and pressure to the braided carbon structure;

subsequently, infusing the braided carbon preform with a thermoset resin; and

forming the braided composite product by melting a portion of the thermoplastic filaments while curing the thermoset resin within the braided carbon preform to form the braided composite product.

2. The method of claim 1 wherein braiding together carbon filaments and thermoplastic filaments comprises braiding axial tows and braid tows into the braided carbon structure, at least one of the axial tows or the braid tows comprising the thermoplastic filaments.

3. The method of claim 2 , wherein the axial tows or the braid tows comprises 10% by volume of the thermoplastic filaments.

4. The method of claim 1 , further comprising repeating applying heat and pressure repeatedly until the braided carbon preform has a desired per-ply thickness.

5. The method of claim 1 , wherein the braided carbon preform comprises less than 20% by volume of the thermoplastic filaments.

6. The method of claim 5 , wherein partially melting the thermoplastic filaments and mixes thermoplastic material with the thermoset resin and increases a fracture toughness of the braided composite product.

7. The method of claim 5 , wherein the braided carbon preform has a smaller per-ply thickness than a per-ply thickness of the braided carbon structure.

8. A method of forming a braided composite product, the method comprising:

coating axial tows and braid tows with a thermoplastic material;

braiding the axial tows and the braid tows into a braided carbon structure, at least one of the axial tows or the braid tows comprising thermoplastic filaments, the thermoplastic filaments comprising less than 40% by volume in each of the at least one of the axial tows or the braid tows;

forming and stabilizing a braided carbon preform by softening the thermoplastic filaments and reducing a thickness of the braided carbon structure, by applying heat and pressure to the braided carbon structure;

subsequently, infusing the braided carbon preform with a thermoset resin; and

curing the thermoset resin within the braided carbon preform to form the braided composite product.

9. The method of claim 8 , further comprising:

repeating applying heat and pressure to a per-ply thickness of the braided carbon structure.

10. A method of improving material characteristics of braided carbon materials, the method comprising:

reducing a per-ply thickness of a braided carbon structure comprising tows comprising less than 40% by volume of thermoplastic filament by applying heat and pressure to the braided carbon structure and forming a braided carbon preform;

subsequently, infusing the braided carbon preform with a thermoset resin; and

forming a braided composite product by partially melting a portion of the thermoplastic filaments while curing the thermoset resin within the braided carbon preform.

11. The method of claim 10 further comprising applying the heat and pressure more than once to tailor the per-ply thickness of the braided carbon structure.

12. The method of claim 11 , wherein applying the heat and pressure to the braided carbon structure to reduce the per-ply thickness of the braided carbon structure improves in-plane mechanical properties of the braided carbon preform.

13. A method of improving material characteristics of braided carbon materials, the method comprising:

infusing a braided carbon preform comprising less than 40% by volume of thermoplastic fibers with a thermoset resin; and

increasing a fracture toughness of a product of the braided carbon preform by applying a heat and pressure during curing the thermoset resin within the braided carbon preform that softens and mixes a portion of the thermoplastic fibers with the thermoset resin infused within the braided carbon preform.

14. A method of forming a braided composite product:

braiding together carbon filaments and thermoplastic filaments to form a braided carbon structure comprising less than 20% thermoplastic filaments by volume;

reducing a thickness of the braided carbon structure by applying heat and pressure to the braided carbon structure and forming a braided carbon preform;

infusing the braided carbon preform with a thermoset resin; and

forming a toughened braided composite product by applying a heat melting a portion of the thermoplastic filaments and curing the braided carbon preform.

15. The method of claim 8 wherein the braid tows comprise 10% by volume of the thermoplastic filaments.

16. The method of claim 10 , further comprising braiding axial tows and braid tows into the braided carbon structure, at least one of the axial tows or the braid tows comprising the thermoplastic filaments.

17. The method of claim 10 , wherein the tows comprise braid tows comprising 10% by volume of the respective thermoplastic filaments.

18. The method of claim 10 , further comprising repeating applying heat and pressure repeatedly until the braided carbon preform has a desired per-ply thickness.

19. The method of claim 10 , wherein the braided carbon preform comprises less than 20% by volume of the thermoplastic filaments.

20. The method of claim 19 , wherein partially melting the thermoplastic filaments and mixes thermoplastic material with the thermoset resin and increases a fracture toughness of the braided composite product.

Assignments (1)

Continuity (2)

References Cited (29)