Sandwiched fiber composites for ballistic applications

Patent metadata

Field	Value
Publication number	US-9682536-B2
Application number	US-96953210-A
Country	US
Kind code	B2
Filing date	Dec 15, 2010
Priority date	Dec 15, 2010
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

A structure may comprise a first outer layer and a polymer fiber composite layer mounted on one side of the first outer layer.

First claim

What is claimed is:

1. A structure, comprising
a first outer layer formed as a monolithic non-fibrous sheet of glass, ceramic, or glass-ceramic material;
a polymer fiber composite layer located directly adjacent to and bonded to one side of the first outer layer and including polymer fibers at least partially embedded in a matrix;
a second outer layer mounted directly adjacent to the polymer fiber composite layer on a side opposite the first outer layer, the second outer layer comprising a composite layer formed of glass fibers and/or polymer fibers having a higher stiffness than the polymer fibers in the polymer fiber composite layer, the second outer layer having a thinner cross section than the polymer fiber composite layer and configured to fail in a manner allowing the polymer fiber composite layer to deform at relatively high strains prior to fiber failure;
the first outer layer and the second outer layer each having a higher stiffness than the polymer fiber composite layer;
the polymer fiber composite layer acting as a spacer spacing apart the first and second outer layer and forming a sandwich stiffening structure increasing a global stiffness of the first outer layer relative to the stiffness of the first outer layer acting alone; and
the first outer layer and the polymer fiber composite layer are each substantially optically transparent.

2. The structure of claim 1 wherein:
at least one of the matrix and the polymer fibers are formed of at least one of the following materials:
a thermoplastic material comprising at least one of the following: acrylics, fluorocarbons, polyamides, polyethylenes, polyesters, polypropylenes, polycarbonates, polyurethanes, polyetheretherketone, polyetherketoneketone, polyetherimides; and
a thermoset comprising at least one of the following: polyurethanes, phenolics, polyimides, bismaleimides, polyesters, epoxy, silsesquioxanes.

3. The structure of claim 2 wherein:
the polymer fibers have a cross section with an aspect ratio of fiber width to fiber thickness; and
the aspect ratio being in the range of from approximately 3 to approximately 500.

4. The structure of claim 1 further comprising:
a spall layer mounted to the second outer layer.

5. The structure of claim 1 wherein the structure is configured as at least one of the following:
a windshield, a canopy, a window, a membrane, an armor panel, a structural panel, an architectural panel, a non-structural article.

6. The structure of claim 1 wherein the composite layer includes high density polyethylene fibers.

7. The structure of claim 1 wherein:
at least one of the polymer fiber composite layer and the second layer is configured as a composite layer assembly having at least one layer of fibers oriented parallel to each other.

8. The structure of claim 7 wherein:
the composite layer assembly has at least two layers of fibers;
the fibers in each of the at least two layers are parallel to each other; and
the fibers in one layer of the at least two layers are non-parallel to the fibers in the other one of the at least two layers.

9. The structure of claim 7 wherein:
the fibers in at least one of the layers have substantially planar fiber faces oriented substantially parallel to an assembly surface of the composite layer assembly.

10. The structure of claim 7 wherein:
the fibers in at least one of the layers have side edges that are in contacting relation with one another.

11. The structure of claim 7 wherein:
the fibers in at least one of the layers has a fiber thickness in the range of approximately 5-5,000 microns.

12. A transparent armor panel, comprising
a first outer layer formed as a monolithic non-fibrous sheet comprised of at least one of ceramic material and glass material;
a polymer fiber composite layer located directly adjacent to and bonded to one side of the first outer layer and comprising a plurality of polymer fibers at least partially embedded in a matrix;
a second outer layer mounted directly adjacent to the polymer fiber composite layer on a side thereof opposite the first outer layer, the second outer layer comprising a composite layer formed of glass fibers and/or polymer fibers having a higher stiffness than the polymer fibers in the polymer fiber composite layer;
the second outer layer having a thickness that is less than a thickness of the polymer fiber composite layer;
the first outer layer and the second outer layer each having a higher stiffness than the polymer fiber composite layer;
the polymer fiber composite layer acting as a spacer spacing apart the first and second outer layer and forming a sandwich stiffening structure increasing a global stiffness of the first outer layer relative to the stiffness of the first outer layer acting alone; and
the first outer layer, the polymer fiber composite layer and the second outer layer being substantially optically transparent.

13. A method of manufacturing a structure, comprising the steps of:
forming a first outer layer as a monolithic non-fibrous sheet of at least one of ceramic material and glass material;
forming a polymer fiber composite layer of a plurality of polymer fibers at least partially embedded within a matrix;
providing the polymer fiber composite layer with a stiffness that is less than the stiffness of the first outer layer;
mounting the polymer fiber composite layer directly adjacent to one side of the first outer layer;
forming a second outer layer as a composite layer formed of glass fibers and/or polymer fibers embedded in a matrix and having a higher stiffness than the polymer fibers in the polymer fiber composite layer, the second outer layer having a thinner cross section than the polymer fiber composite layer, the first outer layer and the second outer layer each having a higher stiffness than the polymer fiber composite layer; and
mounting the second outer layer directly adjacent to the polymer fiber composite layer on a side opposite the first outer layer.

14. The method of claim 13 further comprising the step of:
mounting a spall layer to the second outer layer.

15. The method of claim 13 wherein:
the first outer layer, the second outer layer, and the polymer fiber composite layer are each substantially optically transparent.

16. The method of claim 13 wherein:
the polymer fibers have a cross section with an aspect ratio of fiber width to fiber thickness in the range of from approximately 3-500.

17. The method of claim 13 wherein:
wherein the polymer fiber composite layer includes high density polyethylene fibers.

18. The method of claim 13 wherein:
at least one of the matrix and the polymer fibers are formed of at least one of the following materials:
a thermoplastic material comprising at least one of the following: acrylics, fluorocarbons, polyamides, polyethylenes, polyesters, polypropylenes, polycarbonates, polyurethanes, polyetheretherketone, polyetherketoneketone, polyetherimides; and
a thermoset comprising at least one of the following: polyurethanes, phenolics, polyimides, bismaleimides, polyesters, epoxy, silsesquioxanes.

19. The method of claim 13 wherein the step of mounting the polymer fiber composite layer directly adjacent to one side of to the first outer layer, and the step of mounting the second outer layer directly adjacent to the polymer fiber composite layer on a side opposite the first outer layer are performed by adhesive bonding.

20. A method of manufacturing a transparent armor panel, comprising the steps of:
forming a fir

Assignees

• Wilenski Mark S
• Kozar Michael P
• Boeing Co

Inventors

• Wilenski Mark S
• Kozar Michael P

Classifications

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title

• F41H5/0407

  Transparent bullet-proof laminates}{informative reference: layered products essentially comprising glass in general B32B17/06, e.g. B32B17/10009; manufacture or composition of glass, e.g. joining glass to glass C03; permanent multiple-glazing windows, e.g. with spacing therebetween, E06B3/66 · CPC title

• Y10T428/24983

  Hardness · CPC title

• B32B17/067

  of fibres or filaments · CPC title

• F41H5/0435

  the additional layers being only fibre- or fabric-reinforced layers · CPC title