Composite vehicle body

Patent metadata

Field	Value
Publication number	US-10766595-B2
Application number	US-201715682844-A
Country	US
Kind code	B2
Filing date	Aug 22, 2017
Priority date	Nov 3, 2016
Publication date	Sep 8, 2020
Grant date	Sep 8, 2020

Abstract

A vehicle body may have an internal skeleton forming a wing shape and a fuselage shape, and a skin fabricated in-situ over the internal skeleton. The skin may include a matrix material, and a plurality of continuous fibers at least partially coated with the matrix material. The plurality of continuous fibers may extend from the wing shape over the fuselage shape.

First claim

What is claimed is:

1. A vehicle body, comprising:
an internal skeleton forming a wing shape and a fuselage shape; and
a skin fabricated in-situ over the internal skeleton and including:
a matrix material; and
plurality of continuous fibers at least partially coated with the matrix material, the plurality of continuous fibers extending from the wing shape over the fuselage shape,

wherein:
the plurality of continuous fibers includes:
a first plurality of continuous fibers arranged into a first layer that is generally parallel to an outer surface of the vehicle body; and
a second plurality of continuous fibers arranged into a second layer overlapping the first layer; and

the first plurality of continuous fibers extend normal to the outer surface from the first layer into the second layer to interlock the first and second layers.

2. The vehicle body of claim 1 , wherein:
the wing shape is a first wing shape;
the internal skeleton further forms a second wing shape; and
the plurality of continuous fibers in the skin on the first wing shape extend over the fuselage shape and into the skin on the second wing shape.

3. The vehicle body of claim 1 , wherein:
the internal skeleton includes at least one of ribs, spars, trusses, stringers, longerons, and bulkheads fabricated from the matrix material and a plurality of continuous fibers encased in the matrix material; and
at least some of the plurality of continuous fibers of the at least one of ribs, spars, trusses, stringers, longerons, and bulkheads extend into and form a portion of the skin.

4. The vehicle body of claim 1 , wherein the second plurality of continuous fibers pass orthogonally between adjacent fibers of the second plurality of continuous fibers.

5. The vehicle body of claim 1 , wherein a density of the plurality of continuous fibers varies along a length of the wing shape.

6. The vehicle body of claim 1 , wherein the matrix material includes multiple resins deposited at strategic locations in the skin.

7. The vehicle body of claim 6 , wherein the multiple resins includes:
a flexible resin at a trailing edge of the wing shape; and
a stiffer resin away from the trailing edge.

8. The vehicle body of claim 6 , wherein the multiple resins includes:
a pyrolized resin at a leading edge of the wing shape; and
an acrylated resin away from the leading edge.

9. A vehicle body, comprising:
an internal skeleton having at least one of ribs, spars, trusses, stringers, longerons, and bulkheads that together make a fuselage shape and a wing shape from a matrix material and a plurality of continuous fibers at least partially coated with the matrix material; and
a skin fabricated in-situ over the internal skeleton,
wherein the plurality of continuous fibers extends from the internal skeleton into the skin.

10. The vehicle body of claim 9 , wherein the plurality of continuous fibers includes:
a first plurality of continuous fibers arranged in generally parallel layers; and
a second plurality of continuous fibers that extend normal to the generally parallel layers to interlock the generally parallel layers.

11. The vehicle body of claim 10 , wherein the second plurality of continuous fibers pass orthogonally between adjacent fibers of the second plurality of continuous fibers.

12. The vehicle body of claim 9 , wherein a density of the plurality of continuous fibers varies along a length of the wing shape.

13. The vehicle body of claim 9 , wherein the matrix material includes multiple resins deposited at strategic locations in the skin.

14. The vehicle body of claim 13 , wherein the multiple resins includes:
a flexible resin at a trailing edge of the wing shape; and
a stiffer resin away from the trailing edge.

15. The vehicle body of claim 13 , wherein the multiple resins includes:
a pyrolized resin at a leading edge of the wing shape; and
an acrylated resin away from the leading edge.

16. A vehicle body, comprising:
an internal skeleton including matrix material and plurality of continuous fibers at least partially coated with the matrix material; and
a skin fabricated in-situ over the internal skeleton, wherein:
the plurality of continuous fibers includes:
a first plurality of continuous fibers arranged into a first layer that is generally parallel to an outer surface of the vehicle body; and
a second plurality of continuous fibers arranged into a second layer overlapping the first layer; and

the first plurality of continuous fibers extend normal to the outer surface from the first layer into the second layer to interlock the first and second layers.

17. The vehicle body of claim 16 , wherein the second plurality of continuous fibers pass orthogonally between adjacent fibers of the second plurality of continuous fibers.

18. The vehicle body of claim 16 , wherein a density of the plurality of continuous fibers varies along a length of the skin.

19. The vehicle body of claim 16 , wherein the matrix material includes multiple resins deposited at strategic locations in the skin.

Assignees

• Cc3D Llc
• Continuous Composites Inc

Inventors

• Stockett Ryan C
• Tyler Kenneth L

Classifications

• B29C70/302

  Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination · CPC title

• B29L2031/3082

  Fuselages · CPC title

• B64C3/18

  Spars; Ribs; Stringers · CPC title

• B29C70/0035

  comprising two or more matrix materials · CPC title

• B29C70/16

  using fibres of substantial or continuous length {(non-woven fabrics per se D04H3/00)} · CPC title