Adhesive fillets and method and apparatus for making same
Methods of forming shaped adhesive fillets are disclosed. The adhesive fillets may be made by stacking multiple layers of adhesive sheets, consolidating the stacked layers, cutting strips from the consolidated layers, and forming the strips into adhesive fillets having desired cross sectional shapes. The fillets may be formed by feeding the strips through an apparatus comprising opposing rollers and a catcher, which facilitates release of the adhesive fillets from the rollers. The formed adhesive fillets are useful for applications such as stiffened panels for aircraft.
1. A formed adhesive fillet comprising multiple stacked and consolidated adhesive layers, wherein the consolidated adhesive layers consist essentially of epoxy adhesive and do not include fibers.
2. The formed adhesive fillet of claim 1 , wherein the fillet comprises from 5 to 8 of the stacked adhesive layers.
3. The formed adhesive fillet of claim 1 , wherein the fillet has a cross section including two arms oriented at an angle of from about 90 to about 120 degrees with respect to each other.
4. The formed adhesive fillet of claim 2 , wherein each of the arms has a length of from about 0.1 to about 0.5 inch.
5. The formed adhesive fillet of claim 1 , wherein the fillet comprises a concave portion having a radius of curvature of from about 0.1 to about 2 inches.
6. The formed adhesive fillet of claim 5 , wherein the fillet comprises two arms and has a chord length measured between tips of the arms of from about 0.2 to about 0.8 inch.
7. A stiffened panel comprising:
a panel;
a stiffening member attached to the panel; and
at least one formed adhesive fillet attached to the panel and the stiffening member, wherein the at least one formed adhesive fillet comprises multiple stacked and consolidated adhesive layers, wherein the consolidated adhesive layers consist essentially of epoxy adhesive and do not include fibers.
8. The stiffened panel of claim 7 , wherein the fillet comprises a 5 to 8 of the stacked adhesive layers.
9. The stiffened panel of claim 7 , wherein the panel comprises an aircraft panel having a thickness of from about 0.1 to about 0.2 inch.
10. The stiffened panel of claim 9 , wherein the panel comprises a graphite/epoxy composite.
11. The stiffened panel of claim 7 , wherein the stiffening member comprises a substantially hat-shaped cross-section.
12. The stiffened panel of claim 11 , wherein the stiffening member has a thickness of from about 0.1 to about 0.2 inch, a width of from about 2 to about 5 inches, and a height of from about 0.5 to about 1.5 inches.
13. The stiffened panel of claim 11 , wherein the adhesive fillets are attached at interior corners where the stiffener meets the panel.