Composite lay up and method of forming

• US 9,545,757 B1
• Filed: 01/10/2014
• Issued: 01/17/2017
• Est. Priority Date: 02/08/2012
• Status: Active Grant

• Current Assignee: Textron Innovations Incorporated (Textron Inc)
• Original Assignee: Textron Innovations Incorporated (Textron Inc)
• Inventors: Boone, Richard, De Putter, Benjamin
• Primary Examiner(s): DANIELS, MATTHEW J
• Application Number:
  US14/152,532
• Time in Patent Office: 1,103 Days
• US Class Current: 1/1
• CPC Class Codes: B29C 70/302 Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
• CPC Class Codes: B29C 70/345 using matched moulds
• CPC Class Codes: B29C 70/545 Perforating, cutting or machining during or after moulding
• CPC Class Codes: B32B 3/28 characterised by a layer comprising a deformed thin sheet , i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled B32B29/08 takes precedence
• CPC Class Codes: B32B 5/12 characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other

Abstract

A fiber reinforced composite structure includes multiple plies of pre-impregnated fiber reinforced material. Consecutive plies are layered such that the fibers of one ply are at 90 degrees relative to the fibers of a proximate ply, and such that the fibers of each ply are oriented at positive or negative 45 degrees with respect to a reference plane of the fiber reinforced composite structure. In a method for fabricating a fiber reinforced composite structure, pre-impregnated fiber reinforced composite plies are layered into a tool layup. Each ply is cut on the bias at either plus 45 degrees or minus 45 degrees. The bias angles of the layered plies alternate one relative to the next. The layered plies are cured after layering.

Claims

1. A method for fabricating a curved fiber reinforced composite structure, the method comprising the steps of:

a) forming a straight charge having a longitudinal axis and a plurality of cut-out features along an edge of the straight charge, wherein the plurality of cut-out features are each separated by a first spacing, and comprising a plurality of full-width prepreg fiber reinforced composite plies, a characteristic fiber orientation of each full-width ply of the straight charge being from 30 to 60 degrees or from −

30 to −

60 degrees with respect to the longitudinal axis of the straight charge and the sign of the characteristic fiber orientation of each full width ply of the straight charge alternating with respect to the sign of the characteristic fiber orientation of each neighboring ply;

b) forming a curved composite layup by placing the straight charge of step a) into a tool layup comprising a bond tool, the bond tool comprising a curved longitudinal or circumferential axis and a mold, the mold having a curved shape and comprising structural features each separated by a second spacing greater than the first spacing which engage the plurality of cut-out features of the straight charge and the straight charge being reshaped to conform to the plurality of structural features of the mold such that the characteristic fiber orientation of each full-width ply is reshaped to be relative to the curved longitudinal or circumferential axis of the bond tool; and

c) curing the curved composite layup of step b), thereby forming a curved fiber reinforced composite structure.

2. The method of claim 1, wherein the characteristic fiber orientation of each full-width ply of the straight charge is from 40 to 50 degrees or from −

40 to −

50 degrees with respect to the longitudinal axis of the straight charge.

3. The method of claim 2, wherein the characteristic fiber orientation of each full width ply of the straight charge forms an angle of 80 to 100 degrees with respect to the characteristic fiber orientation of each neighboring ply.

4. The method of claim 3, wherein the straight charge further comprises a plurality of full-width plies of woven fibers.

5. The method of claim 1, wherein the straight charge comprises a plurality of full-width plies of unidirectionally oriented fibers.

6. The method of claim 1, wherein the straight charge further comprises a plurality of partial plies of unidirectionally oriented fibers, an edge of each partial ply aligning with an edge of the straight charge and the characteristic fiber orientation of each of the partial plies of the straight charge being aligned with the longitudinal axis of the straight charge.

7. The method of claim 1, wherein a plurality of straight charges are layered into the tool layup prior to step c).

8. The method of claim 1, wherein the radius of curvature of the bond tool axis is 60 inches or greater.

9. The method of claim 1 wherein the mold comprises a surface comprising a planar substantially horizontal portion and being curved so that the radius of curvature lies in the plane of the surface.

10. The method of claim 9, wherein each full width ply of the composite layup comprises a characteristic fiber orientation in a plane parallel to the planar substantially horizontal portion of the surface of the mold that is from 30 to 60 degrees or from −

30 to −

60 degrees with respect to the bond tool axis and the sign of the characteristic fiber orientation of each full width ply in a plane parallel to the planar substantially horizontal portion of the surface of the mold alternates with respect to the sign of characteristic fiber orientation of each neighboring ply.