Claims
- 1-11. (Canceled)
- 12. A method for manufacturing a plurality of SMC components comprising:
cutting a plurality of blanks from a single prepreg web, wherein the blanks are directly adjacent to one another in the prepreg web prior to cutting; stacking said plurality of blanks to form a multilayer prepreg stack; placing said multilayer prepreg stack into a heated mold of a molding press; flow molding the prepreg stack by at least partially closing the mold to form a SMC component; and thermally curing said SMC component in said mold, wherein said mold is closed during curing, wherein at least one blank of said plurality of blanks is a reference blank, said reference blank being cut to size to have a reference shape and reference surface area (Fr), and wherein at least one additional SMC component is formed from at least one additional multilayer prepreg stack, each said at least one additional multilayer prepreg stack including an additional reference blank having said reference shape and said reference surface area, each additional reference blank being separately weighed after cutting; wherein the weight of said reference blank Gr,actual, the surface area of said reference blank Fr, and the desired total weight Gg for all blanks in a multilayer prepreg stack are used to determine a total surface area Fu for the non-reference blanks in said multilayer prepreg stack in accordance with the relationship Fu=Fr·(Gg/Gr,actual−1), or in accordance with a relationship derived therefrom and identical in principle; and wherein the other blanks of said plurality of blanks are non-reference blanks, said non-reference blanks being cut from a portion of the prepreg web directly adjacent to the reference blank, and said non-reference blanks having a total surface area Fu.
- 13. The method as claimed in claim 12, wherein the blanks for said multilayer prepreg stack and said one or more additional multilayer prepreg stacks are cut from said single prepreg web.
- 14. A method for manufacturing a plurality of SMC components, comprising:
cutting a plurality of single-layer blanks from a single prepreg web; placing each said single-layer blank into a heated mold of a molding press; flow molding each blank by at least partially closing the mold to form a SMC component; and thermally curing each said SMC component in said mold, wherein said mold is closed during curing; wherein cutting a plurality of single-layer blanks comprises: cutting a plurality of reference blanks having a reference shape and reference surface area from the prepreg web; determining an excess surface area Fa for each reference blank based on the actual weight of the reference blank Gr,actual, the surface area of the reference blank Fr, and desired weight of the single-layer blank Gn, in accordance with the relationship Fa=Fr·(1−Gn/Gr,actual), or in accordance with a relationship which is derived therefrom and identical in principle; and cutting a waste piece having said surface area Fa from an edge of each reference blank to form single-layer blanks having the desired weight Gn and a shape corresponding to a desired single-layer blank shape.
- 15. The method as claimed in claim 12, wherein the non-reference blanks in said multilayer prepreg stack are rectangular and congruent in relation to one another, wherein a dimension (l) of the side of the rectangle is the same for the non-reference blanks of said multilayer prepreg stack and for the non-reference blanks of said at least one additional multilayer prepreg stack, and wherein a dimension (b) transverse to the dimension (l) is dimensioned individually for the non-reference blanks in each multilayer prepreg stack in accordance with the relationship b=Fr·(Gg/Gr,actual−1)/l·n, where n denotes the number of non-reference blanks.
- 16. The method as claimed in claim 15, wherein the dimension (l) is aligned parallel to the longitudinal direction of the prepreg web and the dimension (b) is aligned transversely to the longitudinal direction of the prepreg web.
- 17. The method as claimed in claim 12, wherein the surface area of the reference blank is approximately 20 to 60% of a total surface area of all blanks of the multilayer prepreg stack.
- 18. The method as claimed in claim 12, wherein the blank lying at the bottom of the multilayer prepreg stack is the reference blank.
- 19. The method as claimed in claim 12, wherein the reference blank and the non-reference blanks of the multilayer prepreg stack are cut out next to one another from the prepreg web, transversely to the longitudinal direction of the prepreg web, in such a way that the space required in the longitudinal direction of the prepreg web is as small as possible.
- 20. The method as claimed in claim 12, wherein said cutting is performed by a robot-guided cutting tool, and wherein the prepreg web rests on a hard base.
- 21. The method as claimed in claim 12, wherein said cutting is performed by a circular saw blade, said circular saw blade performing a rotary oscillating movement with more than 15,000 cycles per minute, and also having rotary oscillating displacements, wherein said displacements are greater than a tooth pitch of said circular saw blade.
- 22. The method as claimed in claim 21, wherein said circular saw blade performs a rotary oscillating movement having from about 20,000 to about 30,000 cycles per minute.
- 23. The method as claimed in claim 21, wherein said displacements are smaller than the thickness of the prepreg web.
- 24. The method as claimed in claim 21, wherein during the cutting by the rotary oscillating circular saw blade, the prepreg web is supported by a smooth, continuous base that is free from joints, wherein said base is composed of a harder material than the cutting teeth of the circular saw blade.
- 25. The method as claimed in claim 12, wherein the prepreg web is stripped of coverings or protective films prior to cutting.
Priority Claims (1)
Number |
Date |
Country |
Kind |
101 45 308.6 |
Sep 2001 |
DE |
|
Parent Case Info
[0001] This application claims the prirority of German Patent Document No. 101 45 308.6, filed 14 Sep. 2001 and PCT/EP02/09095 filed 14 Aug. 2002 the disclosure of which is expressly incorporated by reference herein, respectively.
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/EP02/09095 |
8/14/2002 |
WO |
|