Ballistic-resistant composite article

• US 4,916,000 A
• Filed: 07/13/1987
• Issued: 04/10/1990
• Est. Priority Date: 07/13/1987
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Kwon, Young D., Harpell, Gary A., Prevorsek, Dusan C., Li, Hsin L.
• Primary Examiner(s): Bell, James J.
• Application Number:
  US07/062,998
• Time in Patent Office: 1,002 Days
• Field of Search: 428/105, 428/114, 428/224, 428/284, 428/295, 428/397, 428/398, 428/902, 428/911, 428/285
• US Class Current: 428/105
• CPC Class Codes: A42B 3/062 with reinforcing means
• CPC Class Codes: B32B 2262/0223 Vinyl resin fibres
• CPC Class Codes: B32B 2262/0253 Polyolefin fibres
• CPC Class Codes: B32B 2262/0269 Aromatic polyamide fibres
• CPC Class Codes: B32B 2305/20 in the form of a non-woven mat
• CPC Class Codes: B32B 2307/54 Yield strength; Tensile strength
• CPC Class Codes: B32B 2307/558 Impact strength, toughness
• CPC Class Codes: B32B 2571/02 defensive, e.g. armour plates or anti-ballistic clothing
• CPC Class Codes: B32B 5/26 another layer next to it also being fibrous or filamentary relative arrangement of fibres or filaments of different layers B32B5/12
• CPC Class Codes: F41H 5/0485 all the layers being only fibre- or fabric-reinforced layers
• CPC Class Codes: Y10S 428/902 High modulus filament or fiber
• CPC Class Codes: Y10S 428/911 Penetration resistant layer
• CPC Class Codes: Y10T 428/24058 including grain, strips, or filamentary elements in respective layers or components in angular relation
• CPC Class Codes: Y10T 428/24132 including grain, strips, or filamentary elements in different layers or components parallel
• CPC Class Codes: Y10T 428/2973 Particular cross section
• CPC Class Codes: Y10T 428/2975 Tubular or cellular
• CPC Class Codes: Y10T 442/2623 Ballistic resistant

Abstract

The present invention provides an improved composite which comprises one or more layers, at least one of said layers comprising network of high strength filaments having a tensile modulus of at least about 160 grams/denier, a tenacity of at least about 7 g/denier and an energy-to-break of at least about 8 joules/gram in a matrix material, the ratio of the thickness of said layer to the equivalent diameter of said filaments is equal to or less than about 12.8, and complex composite articles formed from said composite.

Claims

1. An impact resistance composite comprised of one or more layers;

at least one of said layers comprising a network of filaments having a tensile modulus of at least about 150 g/denier, and an energy-to-break of at least about 8 j/g and a tenacity equal to or greater than about 7 g/denier in a matrix wherein, the ratio of the thickness of said layer to the equivalent diameter of said filaments is equal to or less than about 12.8.

2. A composite as recited in claim 1 wherein said ratio is from 1 to about 10.

3. A composite as recited in claim 2 wherein said ratio is from 1 to about 8.

4. A composite as recited in claim 3 wherein said ratio is from about 1 to about 5.

5. A composite as recited in claim 4 wherein said ratio is from about 1.5 to about 3.

6. A composite as recited in claim 1 wherein the filaments have a tenacity equal to or greater than about 10 g/d, a tensile modulus equal to or greater than about 300 g/d and an energy-to-break equal to or greater than about 10 j/g.

7. A composite as recited in claim 6 wherein said tenacity is equal to or greater than about 20 g/d, said modulus is equal to or greater than about 500 g/d and said energy-to-break is equal to or greater than about 15 j/g.

8. A composite as recited in claim 7 wherein said tenacity is equal to or greater than about 25 g/d, said modulus is equal to or greater than about 1000 g/d, and said energy-to-break is equal to or greater than about 20 j/g.

9. A composite as recited in claim 1 wherein said tenacity is equal to or greater than about 30 g/d, said modulus is equal to or greater than about 1300 g/d and the energy-to-break is equal to or greater than about 30 j/g.

10. A composite as recited in claim 1 wherein the thickness of said layer is less than or equal to about 0.04 cm.

11. A composite as recited in claim 10 wherein said thickness is equal to or less than about 0.03 cm.

12. A composite as recited in claim 11 wherein said thickness is from about 0.0007 to about 0.02 cm.

13. A composite as recited in claim 12 wherein said thickness is from about 0.002 to about 0.02 cm.

14. A composite as recited in claim 1 which comprises more than one layer.

15. A composite as recited in claim 1 wherein said filaments are polyethylene filaments having a tensile modulus of at least about 800 g/denier and an energy-to-break of at least 35 j/g.

16. A composite as recited in claim 15 wherein said filaments have a tensile modulus of at least about 1100 g/denier and an energy-to-break of at least about 40 j/g.

17. A composite as recited in claim 1 wherein said network of filaments comprises a sheet-like filament array in which said filaments are arranged substantially parallel to one another along a common filament direction.

18. A composite as recited in claim 17 wherein said composite comprises more than one layer, with adjacent layers aligned, at a 90°

angle with respect to the longitudinal axis of the parallel filaments contained in said layers.

19. A composite as recited in claim 1 wherein said network of filaments comprises a non-woven fabric.

20. A composite as recited in claim 1 wherein said network of filaments comprises a woven fabric.

21. A composite as recited in claim 1 wherein the volume fraction of said filaments is at least about 0.4.

22. A composite as recited in claim 1 wherein the volume fraction of said filaments is at least about 0.6.

23. A composite as recited in claim 1 wherein the volume fraction of said filaments is at least about 0.7.

24. A composite according to claim 1 wherein said matrix material is rigid having a tensile modulus of greater than about 6000 psi (41,300 kpa) measured at 25°

C.

25. A composite according to claim 24 wherein said matrix material is selected from the group consisting from the group consisting of phenolic resins, epoxy resins, allylic, high density polyethylene, polyvinyl chloride, polyvinyl ester resin, unsaturated polyester resin, polymethylmethacrylate and polystyrene.

26. A composite according to claim 1 wherein said matrix material is an elastomeric materials having a tensile modulus equal to or less than about 6,000 psi (41,300 kpa) at 25°

C.

27. A composite as recited in claim 2 wherein said elastomeric matrix material comprises an elastomer having a glass transition temperature of less than about 0°

C.

28. A composite as recited in claim 27 wherein said elastomer has a glass transition temperature of less than about -40°

C.

29. A composite as recited in claim 28 wherein said elastomer has a glass transition temperature of less than about -50°

C.

30. A composite as recited in claim 26 wherein said elastomeric matrix has tensile modulus of less than about 5,000 psi.

31. A composite as recited in claim 26 wherein said elastomeric matrix material has a tensile modulus of less than about 1,000 psi (6,883 kpa).

32. A composite as recited in claim 26 wherein said elastomeric matrix material has a tensile modulus of less than about 500 psi (3,442 kpa).

33. A composite as recited in claim 1 wherein said filaments have a tenacity of at least about 15 g/denier.

34. A composite as recited in claim 1 wherein said filaments are polypropylene filaments having a tenacity of at least about 8 grams/denier.

35. A composite as recited in claim 1 wherein said filaments are aramid filaments.

36. A composite as recited in claim 1 wherein said filaments are polyvinyl alcohol filaments.

37. A composite as recited in claim 1 comprising a plurality of networks each of said networks comprising a sheet-like array of said filaments in which said filaments are aligned substantially parallel to one another along a common filament direction.

38. A composite as recited in claim 37 wherein the filament alignment directions in selected networks are rotated with respect to the alignment direction of another layer.

39. A composite as recited in claim 1 wherein said filaments are coated with an elastomeric material having a modulus equal to or less than about 6000 psi (41,300 kpa).

40. A composite as recited in claim 39 wherein said networks are consolidated together with a binder composed of a non-elastomeric material.

41. A composite as recited in claim 39 wherein said coated filaments are in the form of yarn and a plurality of the yarns are arranged to form the network.

42. A composite as recited in claim 1 wherein said network of filaments is comprised of dissimilar filaments having different compositions.

43. A composite as recited in claim 1 wherein said elastomeric material consists essentially of a polystyrene-polyisoprene-polystyrene, tri-block copolymer.

44. A composite as recited in claim 1 wherein said elastomeric material consists essentially of a polystrene-polyethylene/butylene-polystyrene tri-block copolymer.

45. A composite as recited in claim 1 wherein said elastomeric material consists essentially of a cross-linked polyisoprene or natural rubber.

46. A composite as recited in claim 1 wherein said filaments comprise polyethylene strips.

47. A composite as recited in claim 43 wherein said strips are woven to form said network.

48. A composite of claim 47 wherein each of said filament is substantially coated with said elastomeric material

49. A composite fabricated totally or in part from the composite of claim 1.

50. A composite comprising the composite of claim 1 and at least one rigid material laminated to form a rigid composite article.

51. A composite article as recited in claim 50 wherein said at least one rigid material is arranged as a layer on a major surface of said simple composite.

52. A composite article as recited in claim 50 wherein a plurality of filament are arranged in a matrix of said elastomer material to form a sheet-like material on which at least two rigid materials in the form of layers are provided, at least one rigid layer being provided on each side of said sheet-like material.

53. A composite article as recited in claim 52 wherein said at least one rigid material comprises highly oriented high molecular weight polyethylene filament in a rigid matrix material.

54. Armor plate comprising the ballistic resistant article of claim 50.

55. A helmet comprising the ballistic resistant article of claim 50.

56. A composite article according to claim 50 wherein said rigid material is a ceramic.

57. A composite article according to claim 50 wherein said rigid material is a metal.

58. A composite as recited in claim 17 wherein said composite comprises more that one layer, with adjacent layers aligned at a 45°

angle with respect to the longitudinal axis of the parallel filaments contained in said layers.