Fiber reinforced composite cores and panels
A fiber reinforced core panel is formed from strips of plastics foam helically wound with layers of rovings to form webs which may extend in a wave pattern or may intersect transverse webs. Hollow tubes may replace foam strips. Axial rovings cooperate with overlying helically wound rovings to form a beam or a column. Wound roving patterns may vary along strips for structural efficiency. Wound strips may alternate with spaced strips, and spacers between the strips enhance web buckling strength. Continuously wound rovings between spaced strips permit folding to form panels with reinforced edges. Continuously wound strips are helically wrapped to form annular structures, and composite panels may combine both thermoset and thermoplastic resins. Continuously wound strips or strip sections may be continuously fed either longitudinally or laterally into molding apparatus which may receive skin materials to form reinforced composite panels.
1. A method of efficiently producing a continuous composite core panel comprising the steps of:
continuously forming an elongated strip of low density cellular material having parallel opposite side surfaces and parallel opposite faces perpendicular to the side surfaces,
continuously applying a layer of crossing reinforcement fibers onto the faces of the strip and continuously applying the same layer of crossing reinforcement fibers onto the side surfaces of the strip, wherein said continuous applications are by helical winding with fibrous reinforcements,
feeding and cutting the continuous strip into a plurality of strips positioned in adjacent relation into a molding apparatus with the crossing reinforcement fibers on opposing faces forming webs positioned between the adjacent strips,
applying a hardenable adhesive resin into the crossing reinforcement fibers forming the webs between the opposing faces while retaining porosity in the crossing reinforcement fibers on the side surfaces for subsequently receiving additional adhesive resin by the molding apparatus, and
curing the hardenable adhesive resin on the opposing faces of the strips within the molding apparatus to harden the adhesive resin within the webs between the opposing faces of the strips and to produce a continuous core panel reinforced with adhesively bonded webs between the opposing faces of the strips with porous crossing reinforcement fibers on the side surfaces thereof.
2. A method as defined in claim 1 wherein the step of applying hardenable adhesive resin to the crossing reinforcement fibers forming the webs comprises applying a heat activated adhesive resin, and including the step of heating the heat activated adhesive resin within the molding apparatus to cure the adhesive.
3. A method as defined in claim 1 and including the step of limiting the application of hardenable adhesive resin to crossing reinforcement fibers on the opposite faces so as to retain some porosity therein.
4. A method as defined in claim 1 wherein the step of continuously applying a layer of crossing reinforcement fibers onto the opposing faces and onto the side surfaces comprises helically winding with a first layer of fibrous reinforcements along the length of the strip, and helically winding a second layer of fibrous reinforcements over the first layer along the length of the strip, with the fibrous reinforcements in the second layer crossing the fibrous reinforcements in the first layer.
5. A method as defined in claim 1 and including the step of winding the continuous strip onto a rotatable reel after receiving the crossing reinforcement fibers on the faces and side surfaces thereof, and wherein the step of feeding comprises feeding the cut strips in laterally extending adjacent relation from the reel into the molding apparatus.
6. A method as defined in claim 1 wherein the step of cutting forms individual strips of predetermined equal lengths.
7. A method as defined in claim 1 further including applying skins to the core panel to form a composite sandwich panel using additional adhesive resin over the crossing reinforcement fibers on the side surfaces of the strips.
8. A method of efficiently producing a continuous composite core panel comprising the steps of:
continuously forming an elongated strip of low density cellular material having parallel opposite side surfaces and parallel opposite faces perpendicular to the side surfaces,
continuously applying a layer of crossing reinforcement fibers onto the faces of the strip and continuously applying the same layer of crossing reinforcement fibers onto the side surfaces of the strip, wherein said continuous applications are by helical winding with fibrous reinforcements,
further reinforcing the strip with longitudinally spaced transverse webs of crossing reinforcing fibers,
feeding and cutting the continuous strip into a plurality of strips positioned in adjacent relation into a molding apparatus with the crossing reinforcement fibers on opposing faces forming webs positioned between the adjacent strips,
applying a hardenable adhesive resin into the crossing reinforcement fibers forming the webs between the opposing faces while retaining porosity in the crossing reinforcement fibers on the side surfaces for subsequently receiving additional adhesive resin by the molding apparatus, and
curing the hardenable adhesive resin within the molding apparatus to harden the adhesive resin within the webs between the opposing faces of the strips to produce a continuous core panel reinforced with transverse webs and adhesively bonded webs between the opposing faces of the strips with porous crossing reinforcement fibers on the side surfaces thereof.
9. A method as defined in claim 8 wherein the step of applying hardenable adhesive resin to the crossing reinforcement fibers forming the webs comprises applying a heat activated adhesive resin, and including the step of heating the heat activated adhesive resin within the molding apparatus to cure the adhesive.
10. A method as defined in claim 8 and including the step of limiting the application of hardenable adhesive resin to crossing reinforcement fibers on the opposite faces so as to retain some porosity therein.
11. A method as defined in claim 8 wherein the step of continuously applying a layer of crossing reinforcement fibers onto the opposing faces and onto the side surfaces comprises helically winding with a first layer of fibrous reinforcements along the length of the strip, and helically winding a second layer of fibrous reinforcements over the first layer along the length of the strip, with the fibrous reinforcements in the second layer crossing the fibrous reinforcements in the first layer.
12. A method as defined in claim 1 and including the step of winding the continuous strip onto a rotatable reel after receiving the crossing reinforcement fibers on the faces and side surfaces thereof, and wherein the step of feeding comprises feeding the cut strips in laterally extending adjacent relation from the reel into the molding apparatus.
13. A method as defined in claim 8 wherein the step of cutting forms individual strips of predetermined equal lengths.
14. A method as defined in claim 8 further including applying skins to the core panel to form composite sandwich panel using additional adhesive resin over the crossing reinforcement fibers on the side surfaces of the strips.