USH1567H - Transparent ceramic armor - Google Patents

Transparent ceramic armor Download PDF

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Publication number
USH1567H
USH1567H US04/667,624 US66762467A USH1567H US H1567 H USH1567 H US H1567H US 66762467 A US66762467 A US 66762467A US H1567 H USH1567 H US H1567H
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United States
Prior art keywords
transparent
elastic modulus
armor
face plate
low density
Prior art date
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Abandoned
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US04/667,624
Inventor
Gordon R. Parsons
Fred E. Mooney
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US Department of Army
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US Department of Army
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Filing date
Publication date
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Priority to US04/667,624 priority Critical patent/USH1567H/en
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Publication of USH1567H publication Critical patent/USH1567H/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0407Transparent bullet-proof laminatesinformative 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2323/00Polyalkenes
    • B32B2323/10Polypropylene
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2325/00Polymers of vinyl-aromatic compounds, e.g. polystyrene
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2329/00Polyvinylalcohols, polyvinylethers, polyvinylaldehydes, polyvinylketones or polyvinylketals
    • B32B2329/06PVB, i.e. polyinylbutyral
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2355/00Specific polymers obtained by polymerisation reactions only involving carbon-to-carbon unsaturated bonds, not provided for in a single one of index codes B32B2323/00 - B32B2333/00
    • B32B2355/02ABS polymers, i.e. acrylonitrile-butadiene-styrene polymers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2367/00Polyesters, e.g. PET, i.e. polyethylene terephthalate
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2369/00Polycarbonates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2375/00Polyureas; Polyurethanes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2571/00Protective equipment
    • B32B2571/02Protective equipment defensive, e.g. armour plates, anti-ballistic clothing

Definitions

  • Non-combat vehicles are often subjected to spasmodic combat conditions and thus now receive armor considerations.
  • the role of the helicopter as a combat vehicle has stimulated concern of its vulunerability to small arms fire, which includes engines, fuel tanks, gear drives and crew personnel.
  • With mobility being a prime requisite for the present day army the ability to navigate, which depends on visibility becomes increasingly important.
  • suitable and efficient transparent protective material lags greatly behind that of opaque armor.
  • the object of this invention to provide a transparent composite (ceramic-glass-plastic), capable of defeating caliber .30 AP M2 projectiles at 0° obliquity, with 8 to 10 pounds areal density and caliber .50 AP M2 projectiles with an areal density of 18-20 pounds, which would not only decrease the vulnerability of vehicles of all types but would establish a technological milestone in the field of transparent armor.
  • Areal density armor weight expressed in pounds per square foot of surface area ##EQU1## where both the experimental and standard armors have the same areal density (lbs./sq. ft.)
  • V 50 penetration is a term used to indicate that there is a 50:50 chance of penetration
  • Elastic Modulus is the ratio of stress to strain within the elastic range of a particular material and the elastic range is the limit to which a particular material may be subjected and still return to its original form or shape.
  • This invention attains its stated object by the formation of a transparent composite consisting of a single ply transparent ceramic face plate,since the required property of high elastic modulus is more characteristic of ceramics than glass, and also of low density with the general overall characteristic of being relatively hard and brittle, while thee transparent back-up layer or layers is of low elastic moduli, of low density and also of relatively tough resilient material.
  • the face plate and the back-up plate of one or more layers are bonded together by any suitable transparent adhesive to form the desired composite.
  • FIG. 1 is a perspective view in section of a three layered transparent composite
  • FIG. 2 is a similar view in section of the composite utilizing two layers.
  • the transparent composite shown in FIG. 1 consists of a front face 10 of spinel plate (by weight substantially 71.5% AL203.28,5% MgO) with a thickness of 3/8", an intermediate layer 11 of sheets of polysulfone or other suitable transparent plastic material of 1/8"hot pressed together to form a tough resilient layer with a thickness of 1/2" and a 1/4" back layer 12 of polycarbonate known under the trade name of "Lexan” which is even more resilient than intermediate layer.
  • the face plate 10 is bonded to the intermediate layer 11 with a 0.0250" sheet of polyvinyl butyral and the back layer 12 is bonded to the layer 11 with a suitable cellulose acetate pressure sensitive adhesive and the configuration is subjected to heat and pressure to form the composite shown.
  • the plates as well as the bonding means are all transparent. It is essential that the ceramic face plate be of high elastic modulus and that the modulus of elasticity decreases from front to back in the composite with the back-plate being of low elastic modulus and all three layers being of as low a density as compatible with the aim of ballistic protection, because the other result sought is that the composite be light enough to be utilized on airborne vehicles. This composite varies in thickness from 1" to 11/2" and will defeat small arms ammunition up through and including caliber .30 AP M2 projectiles.
  • FIG. 2 shows a light weight transparent composite for defeating all small arms ammunition up through and including caliber .50 AP M2 projectiles, wherein the 1/2" face plate 13 may be spinel plate, of the composition set forth above and the back-up layer or layers 14 with an overall thickness of 1" to 11/4" and which may be made up singly or several combinations as interlayers or laminated sheets of the same material or cast in place.
  • This back-up layer 14 as in the composite in FIG. 1, should be of low elastic modulus and of low density.
  • the back-up layer or plate 14 may be composed of various transparent thermoplastic or thermosetting composition selected from the following.
  • each component and subsequently the entire composite will vary according to the specific materials utilized and the type of projectiles the armor is designed to defeat. In general, the composite thickness should vary between 1" and 11/4" for defeating caliber .30 AP M2 projectiles and between 11/2" to 13/4 to defeat caliber .50 AP M2 projectiles.
  • the areal density of these composites should vary from 8 to 10 pounds for defeating caliber .30 AP M2 projectiles at 0° obliquity and from 18 to 20 pounds for defeating caliber .50 AP M2 projectiles at 0° obliquity.
  • the transparent adhesive employed in effectively bonding the laminae together are readily available from various manufacturers.
  • the bonding adhesive is applied in a manner well known in the art and is followed by curing at elevated temperatures and pressures which will vary according to the type of resin employed.

Abstract

A transparent composite armor providing complete protection for small armsrojectiles up to and including caliber .50 AP M2 projectiles consisting of two or more layers of transparent material having a hard frangible face plate backed by one or more tough resilient plates to absorb the excess impact force after contact with the face plate, the several plates being bonded together with a suitable transparent adhesive.

Description

The invention described herein may be manufactured, used, and licensed by or for the Government for governmental purposes without the payment to me of any royalty thereon.
BACKGROUND
Heretofore, significant advances in transparent armor have been attained by the geometrical arrangement of commercially available materials such as hard glasses, chemically-tempered glasses, thermoset biaxially stretched acrylics, polycarbonates, etc. Utilizing these material composites with areal densities of 10 to 11 pounds have attained merit ratings of about 1.40 against caliber .30 BALL M2 projectiles at 0° obliquity, while, caliber 30 AP M2 projectiles have been defeated at 0° obliquity utilizing these materials with areal densities of approximately 20 lbs to show merit ratings of 1.10 to 1.36. These composites have areal densities which are unacceptable to military requirements, particularly for aircraft applications, and for that reason have not been incorporated in armor systems. Further, transparent composites that defeat caliber .50 BALL M2 and AP M2 projectiles are nonexistent, yet non-combat vehicles are increasingly subjected to these threats.
Present day combat has necessitated a change in tactics to cope with guerilla warfare and has resulted in stringent requirements affecting the design of air and land vehicles. Non-combat vehicles are often subjected to spasmodic combat conditions and thus now receive armor considerations. The role of the helicopter as a combat vehicle has stimulated concern of its vulunerability to small arms fire, which includes engines, fuel tanks, gear drives and crew personnel. With mobility being a prime requisite for the present day army, the ability to navigate, which depends on visibility becomes increasingly important. Yet, the development of suitable and efficient transparent protective material lags greatly behind that of opaque armor.
However, nearly all transparent materials have been deficient in that they have only a limited capability for inducing fracture of small arms armorpiercing projectiles, which is the criterion in determining favorable ballistic performance. Attempts to obtain stress-wave reinforcement of stresses in the projectile by variation of composite glass frontal layer thickness have been singularly unsuccessful. It appears that available glasses do not have sufficient strength or modulus to induce high amplitude stress pulses in the projectiles.
It is therefore, the object of this invention to provide a transparent composite (ceramic-glass-plastic), capable of defeating caliber .30 AP M2 projectiles at 0° obliquity, with 8 to 10 pounds areal density and caliber .50 AP M2 projectiles with an areal density of 18-20 pounds, which would not only decrease the vulnerability of vehicles of all types but would establish a technological milestone in the field of transparent armor.
The means, by which the selection of materials by properties and proper geometric arrangement for maximum ballistic protection, are the result of intensive investigation of the pressure wave transfer through ceramic composites impacted by steel cored projectiles. Theoretical and experimental conclusions indicate the fundamental material properties, modulus of elasticity and density, are favorable to ballistic protection when a high elastic modulus and low density facing material is utilized ia conjunction with a low elastic modulus and low density back-up material.
Expressions employed herein are defined as follows:
Areal density: armor weight expressed in pounds per square foot of surface area ##EQU1## where both the experimental and standard armors have the same areal density (lbs./sq. ft.)
AP: armor piercing
V50 penetration: is a term used to indicate that there is a 50:50 chance of penetration
Elastic Modulus: is the ratio of stress to strain within the elastic range of a particular material and the elastic range is the limit to which a particular material may be subjected and still return to its original form or shape.
This invention attains its stated object by the formation of a transparent composite consisting of a single ply transparent ceramic face plate,since the required property of high elastic modulus is more characteristic of ceramics than glass, and also of low density with the general overall characteristic of being relatively hard and brittle, while thee transparent back-up layer or layers is of low elastic moduli, of low density and also of relatively tough resilient material. The face plate and the back-up plate of one or more layers are bonded together by any suitable transparent adhesive to form the desired composite.
Variations of the composite are illustrated in the drawing in which:
FIG. 1 is a perspective view in section of a three layered transparent composite and
FIG. 2 is a similar view in section of the composite utilizing two layers.
The transparent composite shown in FIG. 1 consists of a front face 10 of spinel plate (by weight substantially 71.5% AL203.28,5% MgO) with a thickness of 3/8", an intermediate layer 11 of sheets of polysulfone or other suitable transparent plastic material of 1/8"hot pressed together to form a tough resilient layer with a thickness of 1/2" and a 1/4" back layer 12 of polycarbonate known under the trade name of "Lexan" which is even more resilient than intermediate layer. When the layers are assembled, the face plate 10 is bonded to the intermediate layer 11 with a 0.0250" sheet of polyvinyl butyral and the back layer 12 is bonded to the layer 11 with a suitable cellulose acetate pressure sensitive adhesive and the configuration is subjected to heat and pressure to form the composite shown. It should be noted that the plates as well as the bonding means are all transparent. It is essential that the ceramic face plate be of high elastic modulus and that the modulus of elasticity decreases from front to back in the composite with the back-plate being of low elastic modulus and all three layers being of as low a density as compatible with the aim of ballistic protection, because the other result sought is that the composite be light enough to be utilized on airborne vehicles. This composite varies in thickness from 1" to 11/2" and will defeat small arms ammunition up through and including caliber .30 AP M2 projectiles.
FIG. 2 shows a light weight transparent composite for defeating all small arms ammunition up through and including caliber .50 AP M2 projectiles, wherein the 1/2" face plate 13 may be spinel plate, of the composition set forth above and the back-up layer or layers 14 with an overall thickness of 1" to 11/4" and which may be made up singly or several combinations as interlayers or laminated sheets of the same material or cast in place. This back-up layer 14 as in the composite in FIG. 1, should be of low elastic modulus and of low density. The back-up layer or plate 14 may be composed of various transparent thermoplastic or thermosetting composition selected from the following.
Acrylonitrile-butadiene-styrene (BS)
Acetal resins
Cellulose acetate
Cellulose acetate butyrate
Cellulose acetate propionate
Acrylics and modified acrylics
Allyl resins
Cellulose triacetate
Chlorinated polyethers
Ethyl cellulose
Epoxy-rigid and flexible
Fluoroplastics
Ionomers-"Surlyn A" (DuPont trade mark)
Melamines
Nylons
Parylene polymers
Phenolics transparent (thermosetting)
Phenoxy resins
Polybutylene
Polycarbonates
Polyesters
Polyethylenes
Polyphenylene
Polypropylene
Polystyrene
Polyurethanes (thermoplastic and thermosetting)
Polysulphone
Polyvinyl alcohol
Polyvinyl fluoride
Polyvinyl butyral
Polyvinylidene chloride
Silicones
Styrene-acrylonitride
Styrene -butadiene
The ballistic protection afforded by these composites from experimental test data are as follows.
Projectile--caliber .30 AP M2
Obliquity--0°
Areal Density--12 lbs/ft2
Ballistic Limit--2930 ft/sec for V50 penetration
Merit Rating--1.65
The thickness of each component and subsequently the entire composite will vary according to the specific materials utilized and the type of projectiles the armor is designed to defeat. In general, the composite thickness should vary between 1" and 11/4" for defeating caliber .30 AP M2 projectiles and between 11/2" to 13/4 to defeat caliber .50 AP M2 projectiles.
The areal density of these composites should vary from 8 to 10 pounds for defeating caliber .30 AP M2 projectiles at 0° obliquity and from 18 to 20 pounds for defeating caliber .50 AP M2 projectiles at 0° obliquity.
The transparent adhesive employed in effectively bonding the laminae together are readily available from various manufacturers. The bonding adhesive is applied in a manner well known in the art and is followed by curing at elevated temperatures and pressures which will vary according to the type of resin employed.
In the foregoing, the preferred embodiment of this invention has been disclosed. However, it is not intended that this invention be so limited to the specific examples set forth above, as it will be apparent to those skilled in the art, that the ingredients may be varied and a variety of equivalent substances may be employed without departing from the spirit of the invention or exceeding the scope of the appended claims.

Claims (5)

We claim:
1. A transparent light weight armor affording complete ballistic protection against small arms ammunition up to and including caliber .30 AP M2 projectiles comprising, a light weight composite having a hard shatterable transparent ceramic face plate containing by weight substantially 71.5% aluminum oxide and 28.5% magnesium oxide with a high elastic modulus and a low density, a transparent intermediate laminated layer of polysulfone sheets hot pressed to form a tough resilient unitary plate of low density and of lower elastic modulus than the face plate, a back-up layer of even greater toughness and resiliency than intermediate layer being a single sheet of polycarbonate of low density and even lower elastic modulus than said intermediate layer, the several layers bonded by heat and pressure to each other with a transparent adhesive so constructed and arranged to form a low density composite with the elastic modulus of the several layers decreasing from front to back and the resiliency increasing in the same direction.
2. A transparent light weight armor affording complete ballistic protection against small arms ammunition up to and including caliber .30 AP M2 projectiles having a muzzle velocity of 2770 feet per second comprising, a light weight composite having a hard shatterable ceramic face plate containing by weight substantially 71.5% aluminum oxide and 28.5% magnesium oxide, said face plate being a single ply 3/8" thick with a high elastic modulus and a low density secured by a 0.0250" sheet of polyvinyl butyral to a transparent laminated intermediate layer of polysulfone sheets hot pressed to form a tough resilient unitary layer, said intermediate layer having a thickness of 1/2" with a low elastic modulus and a low density and a 1/4" back-up layer of greater resiliency than intermediate layer being a single ply transparent sheet of polycarbonate of even lower elastic modulus, low density and greater resiliency than said intermediate layer, said back-up layer being held to the intermediate layer with transparent adhesive the several layers bonded together by heat and pressure so constructed and arranged as to provide a low density transparent composite armor with an overall thickness of substantially 11/8" having an areal density of substantially 12 pounds per square foot with the elastic modulus decreasing from front to back and the resiliency increasing in the same direction capable of defeating small arms ammunition up to a V50 penetration of 2930 feet per sec. and with a merit rating of 1.65 as compared to standard steel armor of equal areal density.
3. A transparent lightweight composite armor comprising a transparent ceramic face plate of high elastic modulus and low density bonded by a transparent adhesive to a transparent laminated plastic back-up plate of low elastic modulus and low density, the face plate comprising a spinel composed of a transparent mixture of aluminum oxide and magnesium oxide, the composite armor being so constructed and arranged as to afford complete ballistic protection from small arms ammunition up to and including caliber .50 AP M2 projectiles.
4. Transparent ceramic armor as defined in claim 3 wherein the face plate has a thickness of substantially one-half inch, the back-up plate has a thickness of substantially one and one-quarter inches, and the overall composite armor has an areal density of substantially 18 to 20 pounds per square foot.
5. A transparent lightweight armor comprising a ceramic face plate formed from a transparent mixture of aluminum oxide and magnesium oxide, bonded by a transparent adhesive to a transparent plastic back-up plate, the face plate having a thickness of substantially three-eights of an inch, the plastic back-up plate having a thickness of substantially three-quarters of an inch, and the composite armor having an areal density of substantially twelve pounds per square foot and being so constructed and arranged as to afford complete ballistic protection from small arms ammunition up to and including caliber .30 AP M2 projectiles.
US04/667,624 1967-09-07 1967-09-07 Transparent ceramic armor Abandoned USH1567H (en)

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Cited By (33)

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Publication number Priority date Publication date Assignee Title
EP1166031A1 (en) 1999-02-09 2002-01-02 Rafael - Armament Development Authority Ltd. Ballistic armor panel
US20030221547A1 (en) * 2002-05-28 2003-12-04 Asher Peretz Lightweight armor plates, systems including same and methods of use thereof
US6860186B2 (en) * 2002-09-19 2005-03-01 Michael Cohen Ceramic bodies and ballistic armor incorporating the same
FR2876786A1 (en) * 2004-10-18 2006-04-21 Saint Gobain Laminated structure resistant to perforating projectiles, e.g. bullet proof glass, has at least one layer at up to 160 degrees to front surface
US20060249012A1 (en) * 2004-11-15 2006-11-09 Sai Sarva Hierarchical material assemblies and articles for use in projectile impact protection
US20070283801A1 (en) * 2006-06-09 2007-12-13 Armorsmith Company Armor apparatus and method
WO2008147391A2 (en) * 2006-11-16 2008-12-04 Neal Murray L Transparent ballistic resistant armor
US20080314237A1 (en) * 2005-10-07 2008-12-25 Cosimo Cioffi Bullet-Proof Structure
US20090217813A1 (en) * 2007-03-21 2009-09-03 John Carberry Glass-Ceramic with laminates
US20090320675A1 (en) * 2007-04-23 2009-12-31 Landingham Richard L Mosaic Transparent Armor
US20100043630A1 (en) * 2006-12-04 2010-02-25 Jay Sayre Composite Armor and Method for Making Composite Armor
US7770506B2 (en) 2004-06-11 2010-08-10 Bae Systems Tactical Vehicle Systems Lp Armored cab for vehicles
US20100257997A1 (en) * 2009-04-10 2010-10-14 NOVA Research, Inc Armor Plate
US20100330341A1 (en) * 2006-06-15 2010-12-30 Defbar Systems Llc Transparent blast and ballistic projectile resistant barrier
EP2275772A1 (en) 2005-06-10 2011-01-19 Saint-Gobain Ceramics and Plastics, Inc. Transparent ceramic composite
US7895932B1 (en) * 2006-11-14 2011-03-01 D&O Innovations, LLC Optically clear turret dome, and combined turret shroud
US20110088541A1 (en) * 2009-10-20 2011-04-21 Linda Ruth Pinckney Transparent armour having improved ballistic properties
US20110185884A1 (en) * 2008-06-13 2011-08-04 Esw Gmbh Bullet-resistant transparent laminate composite and protection arrangement having a bullet-resistant transparent laminate composite
US20110203452A1 (en) * 2010-02-19 2011-08-25 Nova Research, Inc. Armor plate
US8066319B2 (en) * 2006-12-01 2011-11-29 Bae Systems Land & Armaments, L.P. Vehicle emergency egress assembly
US8161862B1 (en) * 2007-01-08 2012-04-24 Corning Incorporated Hybrid laminated transparent armor
US8176829B1 (en) 2007-03-21 2012-05-15 Schott Corporation Armor system and method of manufacture
WO2012145664A1 (en) * 2011-04-22 2012-10-26 Schott Corporation Light weight temperature resistant transparent laminate structure
US20120291621A1 (en) * 2010-01-29 2012-11-22 Battelle Memorial Institute Composite armor and method for making composite armor
US8603616B1 (en) 2007-09-27 2013-12-10 Schott Corporation Lightweight transparent armor window
US8632120B2 (en) 2006-12-01 2014-01-21 Bae Systems Land & Armaments L.P. Universal latch mechanism
US8695476B2 (en) 2011-03-14 2014-04-15 The United States Of America, As Represented By The Secretary Of The Navy Armor plate with shock wave absorbing properties
US20140290473A1 (en) * 2011-06-21 2014-10-02 Bayer Materialscience Llc Polycarbonate laminate for close-proximity blast events
US9091510B2 (en) * 2007-03-21 2015-07-28 Schott Corporation Transparent armor system and method of manufacture
US9157703B2 (en) 2011-04-01 2015-10-13 Am General Llc Transparent Armor Structure
US20190178611A1 (en) * 2017-09-17 2019-06-13 Kris McKenna Transparent Projectile-Proof Panels, Devices and Methods
US20200025527A1 (en) * 2017-09-17 2020-01-23 Tardigrade Industries Transparent Projectile Proof Panels, Devices and Methods
CN111006547A (en) * 2019-12-19 2020-04-14 中国航空制造技术研究院 Light bulletproof armor composite structure containing transparent aerogel

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US1423652A (en) * 1921-08-18 1922-07-25 American Abrasive Metals Compa Plate for resisting flame and cutting tools
US3083123A (en) * 1960-06-01 1963-03-26 Gen Electric Magnesia alumina spinel articles and process of preparing same
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Cited By (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1166031A1 (en) 1999-02-09 2002-01-02 Rafael - Armament Development Authority Ltd. Ballistic armor panel
US20030221547A1 (en) * 2002-05-28 2003-12-04 Asher Peretz Lightweight armor plates, systems including same and methods of use thereof
US6860186B2 (en) * 2002-09-19 2005-03-01 Michael Cohen Ceramic bodies and ballistic armor incorporating the same
US7770506B2 (en) 2004-06-11 2010-08-10 Bae Systems Tactical Vehicle Systems Lp Armored cab for vehicles
FR2876786A1 (en) * 2004-10-18 2006-04-21 Saint Gobain Laminated structure resistant to perforating projectiles, e.g. bullet proof glass, has at least one layer at up to 160 degrees to front surface
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