Forming Composite Features Using Steered Discontinuous Fiber Pre-Preg

a discontinuous fiber and composite technology, applied in the direction of process and machine control, instruments, mechanical control devices, etc., can solve the problems of inability to control local thickness/fiber orientation, inability to achieve close control of thickness and/or fiber orientation in local areas with tight contours, and inability to achieve local thickness/fiber orientation. control, the effect of optimizing the structural properties of the lamina

Inactive Publication Date: 2014-09-11
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0007]The disclosed embodiments provide a method and apparatus for fabricating composite features of laminates which provide increased control over feature thickness and/or fiber orientation in local areas of a laminate structure, such as in tight contours and

Problems solved by technology

The ability to control local thickness/fiber orientation is limited using current fabrication processes.
For example, automated fiber placement equipment may be used to steer continuous tows onto the substrate, but the radius of curvature that can be achieved is limited, thus making control of fibe

Method used

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  • Forming Composite Features Using Steered Discontinuous Fiber Pre-Preg
  • Forming Composite Features Using Steered Discontinuous Fiber Pre-Preg
  • Forming Composite Features Using Steered Discontinuous Fiber Pre-Preg

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Embodiment Construction

[0050]The disclosed embodiments provide a method and apparatus for fabricating fiber reinforced resin laminates which provide increased control over laminate thickness, contour, width, cross-sectional profile and / or fiber orientation in local areas of a laminate structure. Referring to FIG. 1, a composite feature 30 comprises discontinuous, resin infused fibers which may be in the form of chopped fiber pre-preg segments 32 having unidirectional reinforcing fibers 25. Each of the fiber pre-preg segments 32 is elongate, having a length L that is greater than its width W. Each of the fiber pre-preg segments 32 may have an aspect ratio (L / W) in the range of approximately 6:1, however this particular ratio is merely illustrative. The fiber pre-preg segments 32 may have other aspect ratios that are selected and / or optimized for the application, including structural requirements and the equipment used to position or place the segments 32. In some embodiments, the fiber pre-preg segments 32...

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Abstract

Interlaminar features of a composite structure are laid up by placing and steering individual chopped fiber pre-preg segments onto a substrate.

Description

BACKGROUND INFORMATION[0001]1. Field[0002]The present disclosure generally relates to fabrication of composite laminate structures using fiber pre-preg, and deals more particularly with a method and apparatus for forming composite structural features by steering discontinuous fiber pre-preg onto a substrate with desired fiber orientations.[0003]2. Background[0004]The strength, stiffness and load transfer characteristics of a composite laminate structure may be optimized through control of fiber orientation during the layup process. Conventional composite laminates may be laid up using pre-preg tapes, tows or broad goods, employing either automated fiber placement equipment or hand placement techniques to layup the material. Generally, the resulting composite structure exhibits substantially consistent structural properties throughout. In some cases, however, it may be necessary or desirable to control the thickness and / or fiber orientation in local areas of a composite laminate in o...

Claims

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Application Information

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IPC IPC(8): B29C70/02B32B5/32
CPCB32B5/32B29C70/021B29K2105/14B29C70/38B29C70/14B29K2105/26B29K2105/0872Y10T428/24132Y10T156/1322B29C2793/0081B29C2793/0072B29C70/545
Inventor GRIESS, KENNETH H.VETTER, DEREK PAULGRAVES, MICHAEL JEFFREY
Owner THE BOEING CO
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