Method and system of forming a composite laminate
AssigneeThe Boeing Company
InventorsDoan Dinh Pham, William Brent Harlow
Life of this patent
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Abstract
A method and associated system for forming composite materials is presented, including providing a composite charge having applied release films to top and bottom surfaces and positioned on a contoured forming tool such that a portion of the composite charge over hangs a second upper surface of forming tool. A fairing bar abuts the forming tool that has an uppermost surface positioned above the second upper surface of the forming tool. The combination of the positioning of the fairing bar and the use of release film in contact with the composite charge allows the composite charge to conform to the contoured forming tool without bridging or wrinkling the composite charge when a forming membrane and applied vacuum are used.
Claims8
A method for forming composite materials, the method comprising:
- providing a composite charge to a lay-up system, where the composite charge comprises upper and lower surfaces;
- applying release film to the upper and lower surfaces of the composite charge;
- positioning a first portion of the composite charge across a first upper surface of a forming tool having a first height measured from the first upper surface to a bottom surface;
- overhanging a second portion of the composite charge over a second upper surface of the forming tool, wherein the second upper surface has a second height that is less than the first height;
- positioning a fairing bar to abut the forming tool, wherein the fairing bar has an uppermost surface, wherein the fairing bar is positioned relative to the forming tool such that the uppermost surface is above the second upper surface of the forming tool;
- applying a forming membrane over the composite charge, the release film, the forming tool, and the fairing bar;
- sealing the forming membrane around a peripheral edge of the lay-up system;
- causing, via applying a vacuum to the lay-up system, a first portion of the forming membrane to conform to the forming tool such that a portion of the second portion of the composite charge is brought into contact with a surface of the forming tool located between the first and second upper surfaces, and
- causing, via the applied vacuum, a remaining portion of the second portion of the composite charge to contact and slide along the second upper surface,
- wherein a second portion of the forming membrane (1) overhangs the forming tool and the fairing bar and (2) remains separated from the composite charge, the forming tool, and the fairing bar after the first portion of the forming membrane is conformed to the forming tool such that the portion of the second portion of the composite charge is brought into contact with the surface of the forming tool located between the first and second upper surfaces.
Dependencies are inferred from the claim text.