Prepregs for use in building lay-ups of composite materials
A scrim-reinforced prepreg assembly for use in building low-porosity lay-ups. The assembly includes a prepreg that is composed of a fibrous reinforcement and a heat-curable resin mixture, the prepreg having suitable viscosity and sufficient tackiness to hold a scrim which is adhered to the prepreg by applying light pressure. The scrim is impressed onto the prepreg to such a degree, that less than half of the circumference of the scrim strands becomes coated by the heat-curable resin mixture.
1. A prepreg assembly comprising
a prepreg comprising a fibrous reinforcement comprising reinforcing fibers and a prepreg resin comprising a thermoset resin that is curable at a curing temperature, said prepreg having a surface that has tack and comprises said prepreg resin and wherein the surface mass of said reinforcing fibers is from 80 g/m 2 to 4000 g/m 2 , and
a scrim located on said surface of the prepreg, said scrim comprising a plurality of thermoplastic strands that each have a cross-sectional diameter of 100 microns to 1000 microns, said thermoplastic strands forming form a grid of parallelograms comprising warp direction strands and strands that are crosswise to said warp direction strands, said warp direction strands being spaced from 3 to 60 millimeters from each other and wherein said strands that are crosswise to said warp direction strands are from 3 to 60 millimeters from each other, said thermoplastic strands each having a cross-sectional diameter and a circumference which is determined by said cross-sectional diameter, wherein less than half of the circumference of each of said thermoplastic strands is coated by said prepreg resin and more than half of the circumference of each of said thermoplastic strands is not coated with said prepreg resin and wherein said prepreg has sufficient tackiness to hold said scrim in place on the surface of said prepreg.
2. A prepreg assembly according to claim 1 wherein said thermoplastic strands each have a cross-sectional diameter of 200 microns to 600 microns.
3. A prepreg assembly according to claim 2 wherein said thermoplastic strands each have a cross-sectional diameter of 300 microns to 400 microns.
4. A prepreg assembly according to claim 1 wherein less than 30% of the circumference of each of said thermoplastic strands is coated by said prepreg resin.
5. A prepreg assembly according to claim 1 wherein said fibrous reinforcement in said prepreg comprises fibers that are unidirectionally aligned.
6. A prepreg assembly according to claim 1 wherein the thermoplastic strands have a substantially round cross-section.
7. A prepreg assembly according to claim 1 wherein said prepreg comprises an edge and wherein said scrim extends outwardly beyond said edge.
8. A prepreg assembly according to claim 1 wherein the curing temperature of said prepreg resin is between 75° C. and 120° C.
9. A prepreg according assembly according to claim 1 wherein said prepreg resin has a gelling temperature and wherein the melting point of said thermoplastic strands is at least 10° C. higher than said gelling temperature.
10. A prepreg assembly according to claim 1 wherein said thermoset resin is selected from the group consisting of epoxy resin, cyanate ester resin, polyester resin, vinyl ester resin and bismaleimide resin.
11. A prepreg assembly according to claim 10 wherein said thermoset resin is epoxy resin.
12. A prepreg assembly according to claim 1 wherein said thermoplastic strands are selected from the group consisting of polyester, polyamide, polyethersulfone and polypropylene.
13. A prepreg assembly according to claim 12 wherein said thermoplastic strands are polyester.
14. A prepreg assembly according to claim 11 wherein said thermoplastic strands are polyester.
15. A cured composite part that comprises a prepreg assembly according to claim 1 which has been cured.
16. A prepreg assembly according to 1 wherein said reinforcing fibers have a surface mass of from 150 g/m 2 to 2000 g/m 2 and consists of carbon tows comprising from 12,000 to 48,000 filaments.
17. A prepreg assembly according to claim 16 were said carbon tows are unidirectionally aligned.
18. A prepreg assembly according to claim 1 wherein said fibrous reinforcement consists of glass fibers which have a linear mass of from 600 tex to 2400 tex.