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US 2026/0249585 A1Published application
Systems and methods for forming a composite layered assembly including a non-woven carbon fiber material
AssigneeThe Boeing Company
InventorsDavis Tran, Brian H. Chien, Brenna Catherine Doll
Life of this patent
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Abstract
A system and method of forming a composite layered assembly includes arranging a first fiberglass layer between a non-woven carbon fiber layer and a decorative layer. The decorative layer, the first fiberglass layer, and the non-woven carbon fiber layer are exposed to one or more curing conditions to form a composite layered assembly.
Claims20
A method, comprising:
- arranging a first fiberglass layer between a non-woven carbon fiber layer and a decorative layer;
- and
- exposing the decorative layer, the first fiberglass layer, and the non-woven carbon fiber layer to one or more curing conditions to form a composite layered assembly.
A composite layered assembly, comprising:
- a non-woven carbon fiber layer;
- a first fiberglass layer having a bottom surface configured to be operably coupled with a top surface of the non-woven carbon fiber layer;
- and
- a decorative layer configured to be operably coupled with a top surface of the first fiberglass layer,
- wherein the decorative layer, the first fiberglass layer, and the non-woven carbon fiber layer are configured to be exposed to one or more curing conditions to form a composite layered assembly.
2 more elements
A method for forming a composite layered assembly, comprising:
- arranging a bottom surface of a first fiberglass layer facing toward to a top surface of a recycled carbon fiber layer, the recycled carbon fiber layer configured to be manufactured of a non-woven carbon fiber material;
- arranging a top surface of a second fiberglass layer facing toward to a bottom surface of the recycled carbon fiber layer;
- arranging a decorative layer relative to a top surface of the first fiberglass layer;
- and
- exposing the decorative layer, the first fiberglass layer, the recycled carbon fiber layer, and the second fiberglass layer to one or more curing conditions to form a composite layered assembly.
2 more elements
Dependencies are inferred from the claim text.