Formation of complex composite structures using laminate templates

• US 10,005,267 B1
• Filed: 09/22/2015
• Issued: 06/26/2018
• Est. Priority Date: 09/22/2015
• 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): Gross, Carson
• Application Number:
  US14/861,641
• Time in Patent Office: 1,008 Days
• Field of Search: 1563071, 1563077
• CPC Class Codes: B29C 70/30 Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
• CPC Class Codes: B29C 70/86 Incorporated in coherent impregnated reinforcing layers, e.g. by winding
• CPC Class Codes: B29D 24/00 Producing articles with hollow walls B29D99/0028 takes precedence
• CPC Class Codes: B29D 99/0003 Producing profiled members, e.g. beams
• CPC Class Codes: B32B 2305/076 Prepregs
• CPC Class Codes: B32B 2305/72 Cured, e.g. vulcanised, cross-linked
• CPC Class Codes: B32B 2305/74 Partially cured
• CPC Class Codes: B32B 2309/105 Thickness
• CPC Class Codes: B32B 2605/18 Aircraft blades, propellers B32B2603/00
• CPC Class Codes: B32B 38/1866 conforming the layers or laminate to a convex or concave profile
• CPC Class Codes: B64C 3/182 Stringers, longerons
• CPC Class Codes: B64C 3/185 Spars
• CPC Class Codes: B64C 3/187 Ribs
• CPC Class Codes: B64F 5/10 Manufacturing or assembling aircraft, e.g. jigs therefor
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

Embodiments of a method to fabricate complex structures include making a pre-cured laminate template. The laminate template is first cured to the required shape, then surface prepared for joining to additional composite lamina. The laminate templates are used to position composite lamina in contact with one another. The composite lamina are then co-cured together to form one monolithic composite structure lacking bond lines or bonded joints. The laminate template supports additional composite lamina for formation of complex structures and replaces template tools from conventional methods.

Claims

1. A method to fabricate a composite structure, comprising:

providing a laminate template including a first template surface having a bend;

providing a first prepreg layup including a first side and a second side opposing the first side;

securing at least a portion of the first side of the first prepreg layup to the first template surface including the bend to form a laminate template-prepreg, wherein the portion of the first prepreg layup secured to the laminate template substantially adopts the shape of the first template surface;

providing a tool having a second template surface;

providing a second prepreg layup including a first side and a second side opposing the first side;

placing at least a portion of the first side of the second prepreg layup in contact with the second template surface of the tool such that the second prepreg layup substantially adopts the shape of the second template surface of the tool;

positioning the laminate template-prepreg with respect to the second prepreg layup such that at least a portion of the second side of the first prepreg layup contacts the second side of the second prepreg layup, wherein the portion of the first prepreg layup including the bend is offset from the second prepreg layup to define a cavity between the first prepreg layup and the second prepreg layup; and

co-curing the laminate template-prepreg and the second prepreg layup together after said positioning of the laminate template-prepreg to form a composite structure.

2. The method of claim 1, wherein the bend of the laminate template possesses an internal radius of curvature less than 0.25 inch.

3. The method of claim 1, wherein the thickness of the laminate template is about one third of the laminate template-prepreg thickness.

4. The method of claim 1, wherein securing the first side of the first prepreg layup to the first surface of the laminate template further comprises partially curing the first prepreg layup with the laminate template.

5. The method of claim 1, wherein the portion of the second side of the first prepreg layup contacting the second prepreg layup does not include the bend.

6. The method of claim 1, further comprising co-curing together the laminate template-prepreg with the second prepreg layup, while the second prepreg layup remains in contact with the tool, wherein at least a portion of the cavity is retained within the resulting composite structure.

7. The method of claim 1, wherein the first surface of the laminate template includes at least two bends.

8. The method of claim 1, wherein the second template surface of the tool includes one or more bends.

9. The method of claim 1, wherein providing the laminate template includes forming the laminate template, comprising:

providing a template-forming tool with a third template surface having the bend;

providing a third prepreg layup having a first side and a second side opposing the first side;

placing the first side of the third prepreg layup in contact with the first surface of the template-forming tool, wherein the third prepreg layup substantially adopts the shape of the third template surface including the bend;

curing the third prepreg layup while contacting the template-forming tool to form the laminate template; and

removing the cured laminate template from the template-forming tool.

10. The method of claim 9, further comprising:

imparting a roughness to a first surface of the laminate template to form the first template surface of the laminate template.