Radially extending composite structures

Patent metadata

Field	Value
Publication number	US-10668672-B2
Application number	US-201715604493-A
Country	US
Kind code	B2
Filing date	May 24, 2017
Priority date	Nov 10, 2009
Publication date	Jun 2, 2020
Grant date	Jun 2, 2020

Abstract

A composite structure having at least one radially extending part is provided. The composite structure is formed with ply layers. At least one of the ply layers used to form the radially extending part has fibers oriented at an angle offset from an edge of the at least one ply layer.

First claim

What is claimed is:

1. A method of forming a composite structure having a radially extending portion in an at least partially automated process, the method comprising:
applying ply layers one at a time on a forming surface of a tool configured to form a composite structure, the tool having an annular portion extending in an axial direction around a centerline and comprising a cylinder and at least one radially extending part extending outward from the annular portion in a direction about an axis transverse to the centerline of the annular portion, wherein at least one ply layer of the ply layers each individually, and before being applied to the composite structure, comprises a plurality of flags of fiber-reinforced material, the plurality of flags each being positioned proximate another flag of the plurality of flags in a substantially end to end configuration to define a major length of the at least one ply layer having fibers in at least some matrix material oriented at a common angle offset from an edge of the at least one ply layer, the plurality of flags of the at least one ply layer each being adhered to a common removable backing material;
extending the at least one ply layer over the forming surface of the tool from the annular portion, through an interface between the annular portion and the at least one radially extending part, and radially outward over the at least one radially extending part;
conforming the ply layers over the forming surface of the tool; and
curing the conformed ply layers to form the composite structure.

2. The method of claim 1 , further comprising orienting the fibers in the at least one ply layer of the ply layers at 17.5 to 27.5 degrees in relation to an edge of the at least one ply layer.

3. The method of claim 1 , further comprising orienting the fibers in the at least one ply layer of the ply layers at 62.5 to 72.5 degrees in relation to an edge of the at least one ply layer.

4. The method of claim 1 , further comprising producing material for the at least one ply layer by applying the plurality of flags on a removable backing material.

5. The method of claim 4 , wherein producing the material, further comprises:
pattern cutting the plurality of flags from a stock supply of material to achieve a desired fiber orientation;
placing the plurality of flags end to end; and
splicing the plurality of flags together to form the at least one ply layer having the desired fiber orientation.

6. The method of claim 5 , further comprising overlapping ends of the plurality of flags when splicing the plurality of flags together.

7. The method of claim 1 , wherein applying the ply layers to the tool further comprises applying the at least one ply layer over the forming surface of the tool so that spliced ends of flags of adjacent ply layers do not align.

8. The method of claim 1 , further comprising butt-splicing at least one flag of the plurality of flags with at least one adjacent flag of the plurality of flags.

9. The method of claim 1 , further comprising gradually increasing and expanding spacing between the fibers in a portion of the at least one ply layer on the at least one radially extending part as the at least one ply layer extends toward a radially outer edge of the at least one radially extending part.

10. The method of claim 1 , further comprising angularly offsetting fiber orientations of the at least one ply layer with at least one other ply layers in the ply layers.

11. The method of claim 1 , further comprising extending the at least one ply layer continuously along the annular portion and the at least one radially extending part without an area within outer edges of each flag of the plurality of flags of the at least one ply layer having been cut before or during layup of the at least one ply layer.

12. The method of claim 1 , further comprising selecting the at least one ply layer to comprise a dry fiber material.

13. A method of forming a composite structure having a radially extending portion, the method comprising:
applying ply layers in an at least partially automated process on a forming surface of a tool configured to form a composite structure, the tool having a first portion comprising a cylinder extending in a direction along a centerline and at least one radially extending part extending outward from the first portion in a direction along an axis transverse to the centerline of the first portion, wherein at least one ply layer of the ply layers comprises, before being applied to the forming surface of the tool, a plurality of flags of fiber-reinforced material, the plurality of flags each being positioned proximate another flag of the plurality of flags to define the at least one ply layer having fibers in at least some matrix material oriented at an angle offset from an edge of the at least one ply layer;
extending the at least one ply layer over the forming surface of the tool from the first portion, through an interface between the first portion and the at least one radially extending part, and radially outward over the at least one radially extending part; and
consolidating the ply layers to form the composite structure.

14. The method of claim 13 , wherein applying the ply layers comprises laying up a plurality of dry fiber materials.

15. The method of claim 13 , further comprising fabricating the at least one ply layer of the ply layers prior to the at least one ply layer being applied to the tool, comprising:
pattern cutting the plurality of flags of fiber-reinforced material from a stock supply of material to achieve a desired fiber orientation; and
placing the plurality of flags end to end on a backing material to form the at least one ply layer having the desired fiber orientation.

16. The method of claim 13 , further comprising extending another ply layer of the ply layers over a second radially extending part of the tool.

17. The method of claim 13 , further comprising staggering splices between flags of adjacent ply layers on the tool.

18. A method of forming a composite structure having a radially extending portion, the method comprising:
applying ply layers in an at least partially automated process on a forming surface of a tool configured to form a composite structure, the tool having a body portion extending in a direction along a longitudinal axis and at least one radially extending part extending outward from the body portion in a direction along an axis transverse to the longitudinal axis of the body portion, wherein at least one ply layer of the ply layers comprises a fiber-reinforced material having fibers oriented at an angle offset from an edge of the at least one ply layer;
selecting the at least one ply layer of the ply layers to comprise a plurality of flags of fiber-reinforced material, the plurality of flags each being positioned proximate another flag of the plurality of flags and adhered to common backing material to define an individual length the at least one ply layer; and
extending the at least one ply layer over the forming surface of the tool from a body portion, through an interface between the body portion and the at least one radially extending part, and radially outward over the at least one radially extending part.

19. The method of claim 18 , further comprising extending another ply layer of the ply layers from the body portion to and over a second radially extending part of the tool.

Assignees

• Northrop Grumman Innovation Systems Inc

Inventors

• Madsen Christopher J
• Mcnabb Eric
• Healey John B
• Rosevear Todd

Classifications

• B64C3/182

  Stringers, longerons · CPC title

• Y10T428/13

  Hollow or container type article [e.g., tube, vase, etc.] · CPC title

• B29C53/585

  the cross-section varying along their axis, e.g. tapered, with ribs, or threads, with socket-ends · CPC title

• B29C70/32 Primary

  on a rotating mould, former or core · CPC title

• B64C1/064

  Stringers; Longerons · CPC title