Retroreflective cube corner sheeting, molds therefore, and methods of making the same

Claims

What is claimed is:

1. A method of manufacturing a plurality of laminae for use in a mold suitable for use in forming retroreflective cube corner articles, each lamina having opposing first and second major surfaces defining therebetween a first reference plane, the first and second major surfaces being substantially planar, each lamina further including a third surface connecting the first and second major surfaces, the method comprising:

orienting a plurality of laminae in an assembly to have their respective first reference planes parallel to each other and disposed at a first angle relative to a fixed reference axis;

forming a plurality of cube corner elements on the third surfaces of at least some of the plurality of the laminae by machining at least three intersecting sets of parallel grooves, each cube corner element having three approximately mutually perpendicular lateral faces, and wherein an assembly of the plurality of laminae defines a mold surface in the third surfaces thereof; and

removing at least a portion of at least one lamina to alter the configuration of the mold surface.

2. A method of manufacturing a plurality of laminae for use in a mold suitable for use in forming retroreflective cube corner articles, each lamina having opposing first and second major surfaces defining therebetween a first reference plane, each lamina further including a third surface connecting the first and second major surfaces, the method comprising:

orienting a plurality of laminae in an assembly to have their respective first reference planes parallel to each other and disposed at a first angle relative to a fixed reference axis;

forming a plurality of cube corner elements on the third surfaces of at least some of the plurality of the laminae at least in part while the laminae are disposed at the first angle relative to the fixed reference axis, each cube corner element having three approximately mutually perpendicular lateral faces, and wherein an assembly of the plurality of laminae defines a mold surface in the third surfaces thereof; and

machining at least one major surface of at least one lamina to alter the configuration of the mold surface.

3. A method of manufacturing a plurality of laminae for use in a mold suitable for use in forming retroreflective cube corner articles, each lamina having opposing first and second major surfaces defining therebetween a first reference plane, each lamina further including a third surface connecting the first and second major surfaces, the method comprising:

orienting a plurality of laminae in an assembly to have their respective first reference planes parallel to each other and disposed at a first angle relative to a fixed reference axis;

forming a plurality of cube corner elements on the third surfaces of at least some of the plurality of the laminae while the laminae are disposed at the first angle relative to the fixed reference axis, the plurality of cube corner elements defining a first, second, and third set of parallel grooves that mutually intersect at first, second, and third base angles .beta..sub.1, .beta..sub.2, .beta..sub.3, each cube corner element having three approximately mutually perpendicular lateral faces, and wherein an assembly of the plurality of laminae defines a mold surface in the third surfaces thereof; and

removing at least a portion of at least one lamina from the assembly to alter the configuration of the mold surface.

4. A method of manufacturing a plurality of laminae for use in a mold suitable for use in forming retroreflective cube corner articles, each lamina having opposing first and second major surfaces defining therebetween a first reference plane, each lamina further including a third surface connecting the first and second major surfaces, the method comprising:

orienting a plurality of laminae in an assembly to have their respective first reference planes parallel to each other and disposed at a first angle relative to a fixed reference axis;

forming a plurality of cube corner elements on the third surfaces of at least some of the plurality of the laminae by machining a first groove set while the laminae are disposed at the first angle relative to the fixed reference axis, the first groove set including at least two parallel adjacent grooves defining a first groove surface and a second groove surface that intersect substantially orthogonally, and by machining a second groove set defining a third groove surface that intersects substantially orthogonally the first and second groove surfaces to form at least one cube corner element, each cube corner element having three approximately mutually perpendicular lateral faces, and wherein an assembly of the plurality of laminae defines a mold surface in the third surfaces thereof; and

removing at least a portion of at least one lamina from the assembly to alter the configuration of the mold surface;

wherein the first angle is greater than zero; and

wherein the plurality of lamina are oriented to have their respective first reference planes parallel to each other and disposed at a second angle relative to the fixed reference axis prior to forming the second groove set, the second angle being different from the first angle.

5. The method of claim 4, wherein the third surface of each lamina defines a second reference plane substantially parallel to the third surface and perpendicular to the first reference plane, the method further comprising:

rotating some of the plurality of the laminae 180.degree. about an axis perpendicular to the second reference plane prior to forming the second groove set.

6. A method of manufacturing a plurality of laminae for use in a mold suitable for use in forming retroreflective cube corner articles, each lamina having opposing first and second major surfaces defining therebetween a first reference plane, each lamina further including a third surface connecting the first and second major surfaces, the method comprising:

orienting a plurality of laminae in an assembly to have their respective first reference planes parallel to each other and disposed at a first angle relative to a fixed reference axis;

forming a plurality of cube corner elements on the third surfaces of at least some of the plurality of the laminae, each cube corner element having three approximately mutually perpendicular lateral faces, and wherein an assembly of the plurality of laminae defines a mold surface in the third surfaces thereof; and

removing at least a portion of at least one lamina to alter the configuration of the mold surface;

wherein the forming step comprises machining at least one set of parallel grooves such that at least two adjacent grooves have different groove depths.

7. A method of manufacturing a plurality of laminae for use in a mold suitable for use in forming retroreflective cube corner articles, each lamina having opposing first and second major surfaces defining therebetween a first reference plane, each lamina further including a third surface connecting the first and second major surfaces, the method comprising:

orienting a plurality of laminae in an assembly to have their respective first reference planes parallel to each other and disposed at a first angle relative to a fixed reference axis;

forming a plurality of cube corner elements on the third surfaces of at least some of the plurality of the laminae, each cube corner element having three approximately mutually perpendicular lateral faces, and wherein an assembly of the plurality of laminae defines a mold surface in the third surfaces thereof; and

removing at least a portion of at least one lamina to alter the configuration of the mold surface;

wherein the forming step comprises forming a set of parallel grooves having a variable groove spacing.

8. The method of claim 1, wherein the intersecting sets of parallel grooves comprise two secondary groove sets that intersect to define a first angle .beta..sub.1, and a primary groove set that intersects the secondary groove sets to define a second and third angle .beta..sub.2 and .beta..sub.3 respectively.

9. The method of claim 8, wherein the angles .beta..sub.1, .beta..sub.2, and .beta..sub.3 form the base angles of a triangle.

10. The method of claim 8, further comprising removing a plurality of laminae from the assembly prior to machining the primary groove set.

11. The method of claim 8, wherein the angle .beta..sub.1 measures between 0.degree. and 60.degree..

12. The method of claim 8, wherein the angle .beta..sub.1 measures between about 10.degree. and about 45.degree..

13. The method of claim 8, wherein the angle .beta..sub.1 measures between about 24.degree. and about 40.degree..

14. The method of claim 8, wherein the forming step comprises forming successive grooves in the primary groove set every n.sup.th laminae, where n is an integer greater than 1.

15. The method of claim 8, wherein the removing step comprises removing laminae selected from the group of laminae which lack a primary groove in their respective third surfaces.

16. The method of claim 8, further comprising reassembling a plurality of the laminae comprising a primary groove on their respective third surfaces to form a mold surface including a plurality of cube corner element segments.

17. The method of claim 16, wherein the cube corner element segments represent more optically active portions of the respective cube corner elements.

18. The method of claim 1, further comprising rotating one or more of the laminae within the assembly 180.degree..

19. The method of claim 1, wherein the third surfaces of the plurality of laminae are substantially parallel but not coplanar.

20. The method of claim 1, wherein the third surfaces of the plurality of laminae are substantially coplanar.

21. The method of claim 1,

wherein the orienting step comprises assembling the plurality of laminae in a suitable fixture, the fixture defining a base plane;

wherein the fixed reference axis is substantially normal to the base plane; and

wherein the first angle measures about 0.degree..

22. The method of claim 1,

wherein the orienting step comprises assembling the plurality of laminae in a suitable fixture, the fixture defining a base plane;

wherein the fixed reference axis is substantially normal to the base plane; and

wherein the first angle measures from about 0.degree. to about 40.degree..

23. The method of claim 22, wherein the first angle measures from about 7.degree. to about 30.degree..

24. The method of claim 1, wherein the forming step is performed while the first angle is greater than zero, the method further comprising:

reorienting the plurality of laminae after the forming step to have their respective first reference planes parallel to each other and disposed at a second angle different than the first angle.

25. The method of claim 24, wherein the second angle is less than the first angle.

26. The method of claim 24, wherein the second angle is about zero.

27. The method of claim 1, wherein machining comprises a material removal technique selected from the group of ruling, fly-cutting, grinding, and milling.

28. The method of claim 1, wherein the forming step comprises inducing relative motion between the plurality of laminae and a cutting tool.

29. The method of claim 1, further comprising replicating the mold surface to form a negative copy of the plurality of cube corner elements suitable for use as a mold for forming retroreflective articles.

30. A mold comprising a copy of the plurality of cube corner elements manufactured according to the method of claim 1.

31. A method of forming retroreflective sheeting, comprising:

providing a mold according to claim 30; and

forming a retroreflective sheeting in the mold.