Apparatus and method for roll forming thermoplastic composites
An apparatus for roll forming thermoplastic composites comprises a plurality of thermoplastic composite material spools, a plurality of thermoplastic composite material rollers, a plurality of sheet metal spools, a plurality of welding rollers, an oven, a forming roller, a pair of pinch rollers. The thermoplastic composite material spools retain plies of thermoplastic composite material. The plies flow through the thermoplastic composite material rollers to form a layup. The sheet metal spools retain metal sheets. The metal sheets and the layup flow through the welding rollers to form a metal composite material laminate. The oven heats the metal composite material laminate. The forming roller imparts a curvature to the metal composite material laminate. The pinch rollers receive the metal composite material laminate from the forming roller, pull the metal composite material laminate, and output the metal composite material laminate in a heated and compressed state.
1 . A method for roll forming thermoplastic composite parts, the method comprising:
forming a composite material layup including a plurality of thermoplastic composite material plies positioned one on another to create a stack:
forming a metal composite material laminate including a first metal sheet positioned in contact with an upper surface of the composite material layup and a second metal sheet positioned in contact with a lower surface of the composite material layup;
heating the metal composite material laminate to create a heated metal composite material laminate;
applying a force to a portion of the heated metal composite material laminate to impart a curvature to the metal composite material laminate; and
applying a compaction to the heated metal composite material laminate after the force is applied; and
placing a zero-degree thermoplastic composite material ply on a top of the thermoplastic composite material layup or a bottom of the thermoplastic composite material layup according to a direction of longitudinal curvature of the thermoplastic composite part.
2 . The method of claim 1 , further comprising welding the first metal sheet to the second metal sheet along side edges of the thermoplastic composite material layup.
3 . The method of claim 1 , further comprising applying a vacuum between the first metal sheet and the second metal sheet of the metal composite material laminate.
4 . The method of claim 1 , further comprising applying a tension to one of the first metal sheet or the second metal sheet in order to control an amount of curvature of the metal composite material laminate.
5 . The method of claim 1 , further comprising cooling the metal composite material laminate after the heated metal composite material laminate is compacted.
6 . The method of claim 1 , further comprising controlling at least one of a level of the force and a direction of the force applied to the portion of the heated metal composite material laminate to control a radius of the curvature of the heated metal composite material laminate.
7 . The method of claim 1 , further comprising pulling the heated metal composite material laminate across a pair of pinch rollers including a longitudinal axis that is non linear so as to apply a non linear shape in a plurality of directions to the heated metal composite material laminate.
8 . A method for roll forming thermoplastic composite parts, the method comprising:
forming a composite material layup including a plurality of thermoplastic composite material plies positioned one on another to create a stack:
forming a metal composite material laminate including a first metal sheet positioned in contact with an upper surface of the composite material layup and a second metal sheet positioned in contact with a lower surface of the composite material layup;
heating the metal composite material laminate to create a heated metal composite material laminate;
applying a force to a portion of the heated metal composite material laminate to impart a curvature to the metal composite material laminate; and
applying a compaction to the heated metal composite material laminate after the force is applied, wherein the first metal sheet has a coefficient of thermal expansion that is different from a coefficient of thermal expansion for the second metal sheet.
9 . The method of claim 8 , further comprising welding the first metal sheet to the second metal sheet along side edges of the thermoplastic composite material layup.
10 . The method of claim 8 , further comprising applying a vacuum between the first metal sheet and the second metal sheet of the metal composite material laminate.
11 . The method of claim 8 , further comprising applying a tension to one of the first metal sheet or the second metal sheet in order to control an amount of curvature of the metal composite material laminate.
12 . The method of claim 8 , further comprising cooling the metal composite material laminate after the heated metal composite material laminate is compacted.
13 . The method of claim 8 , further comprising controlling at least one of a level of the force and a direction of the force applied to the portion of the heated metal composite material laminate to control a radius of the curvature of the heated metal composite material laminate.
14 . The method of claim 8 , further comprising pulling the heated metal composite material laminate across a pair of pinch rollers including a longitudinal axis that is non linear so as to apply a non linear shape in a plurality of directions to the heated metal composite material laminate.
15 . The method of claim 8 , further comprising placing a zero-degree thermoplastic composite material ply on a top of the thermoplastic composite material layup or a bottom of the thermoplastic composite material layup according to a direction of longitudinal curvature of the thermoplastic composite part.
16 . The method of claim 8 , wherein the first metal sheet has a coefficient of thermal expansion that is different from a coefficient of thermal expansion for the second metal sheet.