Method of molding complex composite parts using pre-plied multi-directional continuous fiber laminate
View Patent ↗Layers of unidirectional (UD) fiber prepreg are formed into a pre-plied, multi-directional, continuous fiber laminate that is used as a molding compound to form three dimensional structures. Cut-outs from the laminate are slotted and folded along fold lines to provide near-net-shaped preforms that may be compression molded to form fiber-reinforced composite structures having complex shapes.
1. A method for forming an uncured fiber-reinforced preform comprising the steps of:
providing a multi-layered, pre-plied, multi-directional planar laminate comprising an interior and an edge, said laminate comprising at least a first layer of prepreg and a second layer of prepreg wherein each of said prepreg layers comprises an uncured resin matrix and unidirectional fibers and wherein the direction of said unidirectional fibers in said first prepreg layer is different from the direction of said unidirectional fibers in said second prepreg layer and wherein said laminate comprises a first tab portion and a second tab portion, said laminate further comprising a linear slot located between said first tab portion and said second tab portion such that said linear slot defines an edge of said first tab portion and an edge of said second tab portion, said linear slot having an open end and a bottom end, said laminate comprising a collinear fold line that extends from the bottom of said linear slot and a first fold line that extends from the bottom of said linear slot and is transverse to said collinear fold line, said first fold line forming an end of said first tab portion, said laminate further comprising a second fold line that extends from the bottom of said linear slot and is transverse to said collinear fold line, said second fold line forming an end of said second tab portion;
folding said multi-layered laminate at said collinear fold line, said first fold line and said second fold line so that the edge of said first tab is aligned with said second fold line and the edge of said second tab is aligned with said first fold line wherein said first and second tab portions overlap each other; and
pushing the overlapped tab portions together to form a portion of said preform.
2. A method for forming a preform according to claim 1 wherein said linear slot extends from an intersection of said fold lines to the edge of said multi-layered laminate.
3. A method for forming a preform according to claim 1 wherein at least one of said fold lines is heated prior to folding said multi-layered laminate to form said folded laminate.
4. A method according to claim 1 which includes the additional step of curing said preform to form a composite structure wherein the portion of said preform that is formed by said first and second tab portions is cured to form a cured portion of said composite structure.
5. A method according to claim 2 which includes the additional step of curing said preform to form a composite structure wherein the portion of said preform that is formed by said first and second tab portions is cured to form a cured portion of said composite structure.
6. A method according to claim 3 which includes the additional step of curing said preform to form a composite structure wherein the portion of said preform that is formed by said first and second tab portions is cured to form a cured portion of said composite structure.
7. A method for forming a preform according to claim 1 wherein said collinear fold line extends from the bottom of said linear slot to an edge of said multi-layered laminate.
8. A method for forming a preform according to claim 1 wherein said first fold line extends from the bottom of said linear slot to an edge of said multi-layered laminate.
9. A method for forming a preform according to claim 1 wherein said second fold line extends from the bottom of said linear slot to an edge of said multi-layered laminate.
10. A method according to claim 7 which includes the additional step of curing said preform to form a composite structure wherein the portion of said preform that is formed by said first and second tab portions is cured to form a cured portion of said composite structure.
11. A method according to claim 8 which includes the additional step of curing said preform to form a composite structure wherein the portion of said preform that is formed by said first and second tab portions is cured to form a cured portion of said composite structure.
12. A method according to claim 9 which includes the additional step of curing said preform to form a composite structure wherein the portion of said preform that is formed by said first and second tab portions is cured to form a cured portion of said composite structure.