EP3329205A1 - Ballistic resistant panel - Google Patents
Ballistic resistant panelInfo
- Publication number
- EP3329205A1 EP3329205A1 EP16742251.8A EP16742251A EP3329205A1 EP 3329205 A1 EP3329205 A1 EP 3329205A1 EP 16742251 A EP16742251 A EP 16742251A EP 3329205 A1 EP3329205 A1 EP 3329205A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- tapes
- ballistic
- sheets
- hdpe
- article
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000011159 matrix material Substances 0.000 claims abstract description 95
- 229920001903 high density polyethylene Polymers 0.000 claims abstract description 64
- 239000004700 high-density polyethylene Substances 0.000 claims abstract description 64
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 24
- 229910052751 metal Inorganic materials 0.000 claims abstract description 10
- 239000002184 metal Substances 0.000 claims abstract description 10
- 229910010293 ceramic material Inorganic materials 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 claims description 24
- 229920001971 elastomer Polymers 0.000 claims description 22
- 239000000806 elastomer Substances 0.000 claims description 20
- 238000004519 manufacturing process Methods 0.000 claims description 15
- 229920002725 thermoplastic elastomer Polymers 0.000 claims description 15
- 239000000919 ceramic Substances 0.000 claims description 7
- 229920010741 Ultra High Molecular Weight Polyethylene (UHMWPE) Polymers 0.000 claims 1
- 239000010410 layer Substances 0.000 description 116
- 229920000642 polymer Polymers 0.000 description 23
- -1 polyethylene Polymers 0.000 description 22
- 239000004698 Polyethylene Substances 0.000 description 19
- 229920000573 polyethylene Polymers 0.000 description 18
- 239000000463 material Substances 0.000 description 15
- 238000002844 melting Methods 0.000 description 11
- 230000008018 melting Effects 0.000 description 11
- 230000008569 process Effects 0.000 description 10
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 9
- 239000005977 Ethylene Substances 0.000 description 9
- 230000006835 compression Effects 0.000 description 9
- 238000007906 compression Methods 0.000 description 9
- 239000004711 α-olefin Substances 0.000 description 8
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 6
- 238000001816 cooling Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 230000032798 delamination Effects 0.000 description 5
- 239000011344 liquid material Substances 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 239000004793 Polystyrene Substances 0.000 description 4
- 239000011230 binding agent Substances 0.000 description 4
- 125000004432 carbon atom Chemical group C* 0.000 description 4
- 229920001577 copolymer Polymers 0.000 description 4
- 239000000835 fiber Substances 0.000 description 4
- 208000014674 injury Diseases 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 229920002223 polystyrene Polymers 0.000 description 4
- 238000012545 processing Methods 0.000 description 4
- 230000008733 trauma Effects 0.000 description 4
- VXNZUUAINFGPBY-UHFFFAOYSA-N 1-Butene Chemical compound CCC=C VXNZUUAINFGPBY-UHFFFAOYSA-N 0.000 description 3
- KWKAKUADMBZCLK-UHFFFAOYSA-N 1-octene Chemical compound CCCCCCC=C KWKAKUADMBZCLK-UHFFFAOYSA-N 0.000 description 3
- VSKJLJHPAFKHBX-UHFFFAOYSA-N 2-methylbuta-1,3-diene;styrene Chemical compound CC(=C)C=C.C=CC1=CC=CC=C1.C=CC1=CC=CC=C1 VSKJLJHPAFKHBX-UHFFFAOYSA-N 0.000 description 3
- RRHGJUQNOFWUDK-UHFFFAOYSA-N Isoprene Chemical compound CC(=C)C=C RRHGJUQNOFWUDK-UHFFFAOYSA-N 0.000 description 3
- 229920002633 Kraton (polymer) Polymers 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 229920001519 homopolymer Polymers 0.000 description 3
- 239000000178 monomer Substances 0.000 description 3
- YWAKXRMUMFPDSH-UHFFFAOYSA-N pentene Chemical compound CCCC=C YWAKXRMUMFPDSH-UHFFFAOYSA-N 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- QQONPFPTGQHPMA-UHFFFAOYSA-N propylene Natural products CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 229920001169 thermoplastic Polymers 0.000 description 3
- 239000004416 thermosoftening plastic Substances 0.000 description 3
- ZGEGCLOFRBLKSE-UHFFFAOYSA-N 1-Heptene Chemical compound CCCCCC=C ZGEGCLOFRBLKSE-UHFFFAOYSA-N 0.000 description 2
- LIKMAJRDDDTEIG-UHFFFAOYSA-N 1-hexene Chemical compound CCCCC=C LIKMAJRDDDTEIG-UHFFFAOYSA-N 0.000 description 2
- WSSSPWUEQFSQQG-UHFFFAOYSA-N 4-methyl-1-pentene Chemical compound CC(C)CC=C WSSSPWUEQFSQQG-UHFFFAOYSA-N 0.000 description 2
- KAKZBPTYRLMSJV-UHFFFAOYSA-N Butadiene Chemical compound C=CC=C KAKZBPTYRLMSJV-UHFFFAOYSA-N 0.000 description 2
- LFVLUOAHQIVABZ-UHFFFAOYSA-N Iodofenphos Chemical compound COP(=S)(OC)OC1=CC(Cl)=C(I)C=C1Cl LFVLUOAHQIVABZ-UHFFFAOYSA-N 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- MKFFGUZYVNDHIH-UHFFFAOYSA-N [2-(3,5-dihydroxyphenyl)-2-hydroxyethyl]-propan-2-ylazanium;sulfate Chemical compound OS(O)(=O)=O.CC(C)NCC(O)C1=CC(O)=CC(O)=C1.CC(C)NCC(O)C1=CC(O)=CC(O)=C1 MKFFGUZYVNDHIH-UHFFFAOYSA-N 0.000 description 2
- 239000002313 adhesive film Substances 0.000 description 2
- 239000012790 adhesive layer Substances 0.000 description 2
- 229920001400 block copolymer Polymers 0.000 description 2
- HGCIXCUEYOPUTN-UHFFFAOYSA-N cyclohexene Chemical compound C1CCC=CC1 HGCIXCUEYOPUTN-UHFFFAOYSA-N 0.000 description 2
- 150000001993 dienes Chemical class 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 239000008188 pellet Substances 0.000 description 2
- 229920006254 polymer film Polymers 0.000 description 2
- 239000005060 rubber Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229920000785 ultra high molecular weight polyethylene Polymers 0.000 description 2
- 238000009736 wetting Methods 0.000 description 2
- BLDFSDCBQJUWFG-UHFFFAOYSA-N 2-(methylamino)-1,2-diphenylethanol Chemical compound C=1C=CC=CC=1C(NC)C(O)C1=CC=CC=C1 BLDFSDCBQJUWFG-UHFFFAOYSA-N 0.000 description 1
- FRWYFWZENXDZMU-UHFFFAOYSA-N 2-iodoquinoline Chemical compound C1=CC=CC2=NC(I)=CC=C21 FRWYFWZENXDZMU-UHFFFAOYSA-N 0.000 description 1
- 229910052580 B4C Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241000905957 Channa melasoma Species 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 241000202867 Helicops Species 0.000 description 1
- 239000004705 High-molecular-weight polyethylene Substances 0.000 description 1
- 229920000106 Liquid crystal polymer Polymers 0.000 description 1
- 239000005062 Polybutadiene Substances 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- 239000004372 Polyvinyl alcohol Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000004699 Ultra-high molecular weight polyethylene Substances 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 150000001336 alkenes Chemical class 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- LTPBRCUWZOMYOC-UHFFFAOYSA-N beryllium oxide Inorganic materials O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 1
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 1
- IAQRGUVFOMOMEM-UHFFFAOYSA-N butene Natural products CC=CC IAQRGUVFOMOMEM-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 238000007596 consolidation process Methods 0.000 description 1
- 235000019628 coolness Nutrition 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 230000009477 glass transition Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 229920001179 medium density polyethylene Polymers 0.000 description 1
- 239000004701 medium-density polyethylene Substances 0.000 description 1
- TVMXDCGIABBOFY-UHFFFAOYSA-N n-Octanol Natural products CCCCCCCC TVMXDCGIABBOFY-UHFFFAOYSA-N 0.000 description 1
- JRZJOMJEPLMPRA-UHFFFAOYSA-N olefin Natural products CCCCCCCC=C JRZJOMJEPLMPRA-UHFFFAOYSA-N 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 229920002239 polyacrylonitrile Polymers 0.000 description 1
- 229920002857 polybutadiene Polymers 0.000 description 1
- 239000002861 polymer material Substances 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 229940068984 polyvinyl alcohol Drugs 0.000 description 1
- 235000019422 polyvinyl alcohol Nutrition 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 125000004805 propylene group Chemical group [H]C([H])([H])C([H])([*:1])C([H])([H])[*:2] 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0414—Layered armour containing ceramic material
- F41H5/0428—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics
- F41H5/0435—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics the additional layers being only fibre- or fabric-reinforced layers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0442—Layered armour containing metal
- F41H5/0457—Metal layers in combination with additional layers made of fibres, fabrics or plastics
- F41H5/0464—Metal layers in combination with additional layers made of fibres, fabrics or plastics the additional layers being only fibre- or fabric-reinforced layers
Definitions
- the present invention pertains to a ballistic resistant panel, and to a method for manufacturing thereof.
- WO2009/109632 describes a ballistic resistant moulded article comprising a compressed stack of sheets comprising reinforcing tapes and an organic matrix material, the direction of the tapes within the compressed stack being not unidirectionally, wherein the tapes have a width of at least 2 mm and a width to thickness ratio of at least 10:1 with the stack comprising 0.2-8 wt . % of an organic matrix material.
- the reinforcing tapes preferably are tapes of ultra-high molecular weight polyethylene.
- the moulded article may be combined with an inorganic strike face, e.g., a plate of metal or ceramic material.
- the present invention pertains to a ballistic-resistant panel comprising
- an inorganic strike face with a thickness of at least 1 mm the strike face comprising one or more of a metal sheet and a sheet of a ceramic material
- the moulded article comprising a HDPE-based layer comprising a compressed stack of sheets comprising reinforcing tapes having a tensile strength of at least 1.0 GPa, a tensile modulus of at least 40 GPa, and a tensile energy-to-break of at least 15 J/g, the direction of the tapes within the compressed stack being not unidirectional, and a high-density polyethylene (HDPE) as matrix material.
- HDPE high-density polyethylene
- WO2009/109632 describes a ballistic resistant moulded article comprising a compressed stack of sheets compris ⁇ ing reinforcing elongate bodies and an organic matrix material.
- the elongate bodies are, for example, polyethylene tapes. Many possible matrix materials are mentioned.
- Prinlin B7137AL is used, which is an aqueous styrene-isoprene-styrene resin .
- WO 2009/141276 describes a laminate for antiballistic purposes which comprises unidirectional the placed polymeric tapes with an E-modulus of an individual polymeric tape of at least 50 GPa and a square metre weight of the laminate above 150 g.
- a laminate for antiballistic purposes which comprises unidirectional the placed polymeric tapes with an E-modulus of an individual polymeric tape of at least 50 GPa and a square metre weight of the laminate above 150 g.
- matrix materials are mentioned. In the example no matrix material is specified.
- WO 2009/056287 describes a material sheet comprising a woven fabric of unidirectional tapes of drawn polymer, wherein the width of a tape varies less then 2% on average in the longitudi ⁇ nal direction of the tape.
- the possibility of using a binder is mentioned, but no information on specific binders is provided. In the example, no binders seem to have been used. None of these references discloses the specific combination of an inorganic strike face and ballistic resistant moulded article comprising a layer based on HDPE as matrix material. Further, none of these references, alone or in combination, suggest that the specific ballistic resistant panel of the invention, would show improved back face deformation and improved performance at higher temperatures.
- the ballistic-resistant panel according to the invention will be discussed in more detail below.
- the ballistic resistant panel according to the invention com ⁇ prises an inorganic strike face with a thickness of at least 1 mm, the strike face comprising one or more of a metal sheet and a sheet of a ceramic material.
- the inorganic strike face generally has a thickness between 1 mm and 25 mm, depending on the threat level. In one embodiment the inorganic strike face has a thickness in the range of 1-15 mm, in some embodiments 4-10 mm. In another embodiment, the inorgan- ic strike face has a thickness of 10-25 mm.
- Suitable metal sheets for use in the strike face used in the in ⁇ vention include sheets comprising steel and/or titanium.
- Suitable ceramic materials for use in the strike face used in the invention include aluminium oxide, boron carbide, silicon carbide, beryllium oxide, and combinations thereof, such as bo ⁇ ron carbide mixed with silicon carbide.
- the strike face generally has a hardness of at least 1000 kg/mm2, in particular at least 1400 kg/mm2.
- the strike face generally has a Brinell Hardness of 250, preferably 350.
- the ballistic resistant panel according to the invention further comprises a ballistic resistant moulded article below the strike face.
- a ballistic resistant moulded article below the strike face.
- the term “below” is intended to refer to the opposite side of the strike face than the side from which ballistic impact is expected.
- the ballistic resistant moulded article below the strike face comprises a HDPE-based layer comprising a compressed stack of sheets comprising reinforcing tapes having a tensile strength of at least 1.0 GPa, a tensile modulus of at least 40 GPa, and a tensile energy-to-break of at least 15 J/g, the direction of the tapes within the compressed stack being not unidirectional, and a high-density polyethylene (HDPE) as matrix material.
- HDPE high-density polyethylene
- the term HDPE- based layer refers to a layer comprising sheets comprising reinforcing tapes and a high-density polyethylene (HDPE) as matrix.
- the matrix content of this layer can vary, e.g., between 0.2 and 20 wt . % .
- the optimum matrix content is determined on the one hand by the amount of HDPE required to provide good delamination properties. On the other hand the amount of matrix should not be more than is required to obtain this effect, as excess matrix does not contribute substantially to the ballistic properties of the panel. It may be preferred for the amount of HDPE matrix ma ⁇ terial in this layer to be in the range of 0.2 to 15 wt . ⁇ 6 , more in particular in the range of 0.2-10 wt.%, still more in partic ⁇ ular in the range of 0.2 to 4 wt.%.
- the HDPE used in the HDPE-based layer generally has a density in the range of 0.925 to 0.970 g/cm3m, determined in accordance with ASTM D792. Materials with a density at the lower end of this range are sometimes sold under the indication MDPE . Within the context of the present specification they are regarded as HDPE.
- the HDPE generally has a molecular weight Mw in the range of 1 ⁇ 10 ⁇ 4 to 1 ⁇ 10 ⁇ 8 g/mol, in particular 1 ⁇ 10 ⁇ 5 to 1 ⁇ 10 ⁇ 7 g/mol.
- the HDPE matrix used in the present invention is an isotropic material and can therewith be distinguished from reinforcing ul ⁇ tra-high molecular weight polyethylene tapes, which are
- the ratio between the strength of the material determined in the direction where it strength is highest (machine direction) and the strength in the direction perpendicular thereto is generally at most 5:1.
- the ratio between the strength of the material deter ⁇ mined in the direction where it strength is highest (machine direction) and the strength in the direction perpendicular thereto is generally at least 50:1.
- This parameter can e.g. be determined from the breaking tenacity as determined in accord ⁇ ance with ASTM-D 7744-11.
- the HDPE-based layer may also encompass other types of matrix material.
- a layer will be indicated as a HDPE- based layer if of the matrix present in this layer at least 60 wt . % is HDPE.
- the matrix present in the HDPE-based layer it is preferred for the matrix present in the HDPE-based layer to comprise at least 70 wt . % HDPE, prefera ⁇ bly at least 80 wt.%, more preferably at least 90 wt . % .
- the moulded article further comprises an elasto ⁇ mer-based layer comprising a compressed stack of sheets
- the ballistic resistant moulded article of the panel according to the invention thus comprises two layers with dif ⁇ ferent types of matrix materials.
- the combination of a layer comprising HDPE as matrix with a layer comprising a thermoplastic elastomer as matrix results in an article which combines high impact re ⁇ sistance with improved constructional integrity of the article and reduced dynamic and static back face deformation upon im ⁇ pact.
- this layer combination ensures that the moulded article also shows good performance at extreme temperatures, e.g., -50°C or +70°C or +90°C.
- the moulded article also shows good peel resistance and good processing properties, in particular being easier to drill or cut.
- the matrix content is between 0.2 and 8 wt.%, calculated on the total of tapes and organic matrix material.
- thermoplastic elastomer matrix material may be present in an amount of at least 1 wt.%, more in particular in an amount of at least 2 wt.%, in some instances at least 2.5 wt.%. In some embodiments it may be preferred for the matrix ma ⁇ terial to be present in an amount of at most 7 wt.%, sometimes at most 6.5 wt.%.
- thermo ⁇ plastic rubbers which are used as matrix in the elastomer-based layer of the moulded article of the panel according to the in ⁇ vention are a class of copolymers or a physical mix of polymers (usually a plastic and a rubber) which consist of materials with both thermoplastic and elastomeric properties, i.e., they show plastic flow above their Tg (glass transition temperature) , Tm (melting point) , or Ts (softening point) (thermoplastic behav ⁇ ior) and resilient properties below the softening point.
- the material has an elongation at break of at least 100%, in particular at least 200%.
- the upper limit is not criti- cal to the present invention. A value of 600% may be mentioned in general.
- the elongation at break of the elastomer is higher than the elongation at break of the fiber or tape that may be manufactured from the composition of the present inven ⁇ tion, as will be discussed in more detail below.
- thermoplastic elastomer has a tensile modulus (at 25°C) of at most 40 MPa (ASTM D7744-11) .
- thermoplastic elastomers include polyurethanes , poly ⁇ vinyls, polyacrylates , block copolymers and mixtures thereof.
- the thermoplastic elastomer is a block copolymer of styrene and an alpha-olefin comonomer.
- Suitable comonomers include C2-C12 alpha-olefins such as ethylene, propylene, buta ⁇ diene, and isoprene.
- the use of polystyrene - polybutadiene - polystyrene polymer or polystyrene - isoprene - polystyrene is considered preferred at this point in time.
- These kind of poly- mers are commercially available, e.g., under the trade name Kraton or Styroflex.
- thermoplastic elastomer and the HDPE as described herein are not the same polymer.
- the HDPE does not have the characteristic properties of the thermo- plastic elastomer, and the other way around.
- HDPE does not generally behave as thermoplastic elastomers, even if it con ⁇ tains small amounts of other monomers or polymers.
- the elastomer-based layer it is possible for the elastomer-based layer to also encompass other types of matrix material.
- a layer will be indicated as an elastomer-based layer if of the matrix present in this layer at least 60 wt . % is elastomer.
- the matrix present in the elastomer-based layer comprises at least 70 wt . % thermoplastic elastomer, preferably at least 80 wt.%, more preferably at least 90 wt.%.
- the matrix present in the elastomer-based layer may comprise at least 70 wt . % thermoplastic elastomer, preferably at least 80 wt.%, more preferably at least 90 wt.%.
- a single type of elastomer or combinations of different elastomers may be used.
- Both the HDPE-based layer and, if present, the elastomer-based layer comprises sheets comprising reinforcing tapes and a ma ⁇ trix .
- the term sheet refers to an individual sheet comprising tapes, which sheet can individually be combined with other corresponding sheets.
- the sheet may or may not comprise a matrix material, as will be elucidated below.
- matrix material is provided within the sheets themselves, where it serves to adhere the tapes to each other.
- matrix material is provided on the sheet, where it acts as a glue or binder to adhere the sheet to further sheets within the stacks. Obviously, the combination of these two embodiments is also envisaged.
- the sheets them ⁇ selves contain reinforcing tapes and a matrix material.
- Sheets of this type may, for example, be manufactured as fol ⁇ lows.
- the tapes are provided in a layer, and then a matrix material is provided onto the layer under such conditions that the matrix material causes the tapes to adhere together.
- This embodiment is particularly attractive where the matrix material is in the form of a film.
- the tapes are provided in a parallel arrangement.
- Sheets of this type may, for a further example, also be manufac ⁇ tured by a process in which a layer of tapes is provided, a layer of a matrix material is applied onto the tapes, and a fur ⁇ ther layer of tapes is applied on top of the matrix.
- the first layer of tapes encompasses tapes arranged in parallel and the second layer of tapes are arranged parallel to the tapes in the first layer but offset thereto.
- the first layer of tapes is arranged in parallel, and the second layer of tapes is arranged crosswise on the first layer of tapes.
- the provision of the matrix material is ef ⁇ fected by applying one or more films of matrix material to the surface, bottom or both sides of the plane of tapes and then causing the films to adhere to the tapes, e.g., by passing the films together with the tapes, through one or more heated pres ⁇ sure rolls.
- the tape layer is provided with an amount of a liquid substance containing the ma ⁇ trix material.
- the liquid substance may be for example a solution, a dispersion or a melt of the matrix material. If a solution or a dispersion of the matrix material is used in the manufacture of the sheet, the process also comprises evaporating the solvent or dispersant. This can for instance be accomplished by using an organic matrix material of very low viscosity in wetting the tape surfaces in the manufacture of the sheet. If so desired, the matrix material may be applied at a reduced pressure (vacuum) .
- the matrix material is applied in the form of a powder, which is adhered to the sheets by heat or pressure, or a combination of both.
- the sheet may be manufactured by the steps of providing a layer of tapes and where necessary adhering the tapes together by the application of heat and pressure.
- the tapes overlap each other at least partial ⁇ ly, and are then compressed to adhere to each other.
- sheets may be free of matrix are when the sheets are manufactured by weaving tapes, either with other tapes, or with bonding thread.
- the matrix material will then be applied onto the sheets to ad ⁇ here the sheets to each other during the manufacture of the ballistic material.
- the matrix material can be applied in the form of a film or in the form of a liquid material, as discussed above for the application onto the tapes themselves. It is also possible to apply the matrix in the form of a powder.
- the matrix material is applied in the form of a web, wherein a web is a discontinu ⁇ ous polymer film, that is, a polymer film with holes. This allows the provision of low weights of matrix materials. Webs can be applied during the manufacture of the sheets, but also between the sheets.
- the matrix mate ⁇ rial is applied in the form of strips, yarns, powder, pellets, or fibres of polymer material, the latter for example in the form of a woven or non-woven yarn of fibre web or other polymeric fibrous weft. Again, this allows the provision of low weights of matrix materials. Strips, yarns, powder, pellets or fibres can be applied during the manufacture of the sheets, but also between the sheets.
- the matrix ma ⁇ terial is applied in the form of a liquid material, as described above, where the liquid material may be applied homogeneously over the entire surface of the elongate body plane, or of the sheet, as the case may be.
- the matrix material in the form of a liquid material inhomogene- ously over the surface of the elongate body plane, or of the sheet, as the case may be.
- the liquid material may be applied in the form of dots or stripes, or in any other suit ⁇ able pattern.
- the matrix material is distributed inhomogeneously over the sheets.
- the matrix material is distributed in- homogeneously within the compressed stack.
- more matrix material may be provided there were the compressed stack encounters the most influences from outside which may det ⁇ rimentally affect stack properties.
- the ballistic-resistant moulded article used in the panel according to the invention comprises a HDPE-based layer and an elastomer-based layer. If so desired, the article may comprise more than one HDPE-based layer and/or more than one elastomer-based layer.
- the moulded article comprises a HDPE-based layer at or near the back face of the article, wherein the back face is the face opposite the strike face side, which is the side from which impact is expected, and where the inorganic strike face is located. It is expected that the presence of the HDPE-based layer at or near the back face of the article helps to prevent delamination and fragmentation of the article. Further the retention of internal structure is maintained.
- the wording "at the back face” means that the lowest point of the layer at issue is within 5%, determined over the cross-section of the article, from the bottom of the article in question, preferably within 3%, in particular at 0% (thus at the outer side of the article, not counting layers not comprising reinforcing tapes and matrix, e.g., cover layers) .
- the wording "near the back face” means that the lowest point of the layer at issue is between 5 and 20%, determined over the cross-section of the article, from the bottom of the article in question.
- the moulded article comprises a HDPE- based layer at or near the strike face side of the article.
- the wording "at the strike face side” means that the highest point of the layer at issue is within 5% from the front of the moulded article in question, determined over the cross-section of the article, preferably within 3%, in particular at 0% (thus at the outer side of the article, not counting layers not comprising rein- forcing tapes and matrix, e.g., cover layers) .
- near the strike face side means that the highest point of the layer at issue is between 5 and 20% from the front of the article in question, determined over the cross-section of the article.
- the article comprises a HDPE-based layer at or near the strike face side of the article, and a HDPE-based layer at or near the back face of the article.
- an elastomer-based layer will be present between the HDPE- based layers.
- the article comprises an elastomer-based layer at or near the strike face of the article, and an elasto ⁇ mer-based layer at or near the back face of the article.
- the article with this structure is a helmet.
- a HDPE-based layer will be present between the elas ⁇ tomer-based layers. This embodiment may be attractive where a system with a very high stiffness is desired. As will be evident to the skilled person, systems with more than three layers, e.g., 4, 5, 6, or even more can also be manufac ⁇ tured if so desired.
- the ballistic resistant moulded article according to the inven ⁇ tion may be flat, single-curved, double curved, or multicurved.
- Examples include panels, e.g., for use in vehicles and helicop ⁇ ters, shields, and helmets.
- the panel according to the invention meets the requirements of one or more of NIJ standard threat level III, NIJ III+, NIJ IV, Stanag 4569, and AEP 55.
- the ballistic resistant moulded article ac ⁇ cording to the invention is a helmet which meets the
- an inorganic strike face thickness of 1 to 5 mm is preferred.
- This ballistic performance is preferably accompanied by a low areal weight, in particular a mass per area of at most 20 kg/m2, more in particular at most 15 kg/m2, even more in particular at most 11 kg/m2.
- the requirements of class NIJ IV threat level of the said Standard are met.
- an inorganic strike face thickness of 4 to 10 mm is preferred.
- This ballistic performance is preferably accompanied by a low areal weight, in particular a mass per area of at most 40 kg/m2, more in particular at most 35 kg/m2, even more in particular at most 30 kg/m2.
- layers are par ⁇ allel to the main (i.e. largest) outer surface of the article. It is preferred for the various layers of the article to extend along substantially the entire article, as this is believed to provide the best possible properties. It is of course possible that, e.g., at the edges of the article one or more of the lay ⁇ ers are not present but it is preferred that both a HDPE based- layer and an elastomer-based layer are present over at least 75%, preferably at least 85%, more preferably at least 90% of the panel, determined from a top or bottom perspective.
- composition of the moulded article used in the panel accord ⁇ ing to the invention can vary within wide ranges, depending on the required properties of the resulting article.
- the article comprises only HDPE-based layers. Where the article also comprises elastomer-based layers, they are generally present in an amount of 5-95 wt.%, the HDPE-based layers also being present in an amount of 5-95 wt.%. In one em- bodiment, the article comprises at least 50 wt.% of HDPE-based layers .
- the HDPE-based layer (s) and elastomer-based layer (s) build up at least 70 wt% of the article, preferably at least 80 wt%, more preferably at least 90 wt% (percentages calculated on lay ⁇ ers comprising reinforcing tapes) .
- the number of sheets in the stack in the ballistic resistant article according to the inven ⁇ tion is generally at least 10, in particular at least 20.
- the number of sheets generally is at most 500, in particular at most 400.
- a sheet comprises a single layer of parallel tapes, wherein the tapes do not overlap or overlap to a very limited extent.
- a sheet comprises a first layer of parallel tapes and a second layer of parallel tapes on top of the first layer of parallel tapes, wherein the tapes of the second layer are parallel to the tapes of the first layer but offset thereto.
- a third, and even a fourth, layer of parallel tapes may be provided, in each case parallel to the tapes in the previous layer, but offset thereto.
- the sheet it is generally preferred for the sheet to comprise two or three lay- ers of parallel tapes, in particular two layers of parallel tapes.
- the sheet comprises woven tapes.
- the moulded article may comprise a compressed stack of sheets wherein the sheets comprise a single layer of parallel tapes which do not overlap, and wherein the direction of the tapes in a second sheet is ro- tated with respect to the direction of the tapes in the adjacent sheet.
- the moulded article may comprise a compressed stack of sheets wherein the sheets comprise a first layer of parallel tapes and a second layer of parallel tapes on top of the first layer of parallel tapes, wherein the tapes of the second layer are parallel to the tapes of the first layer but offset thereto, and wherein the direction of the tapes in a second sheet is rotated with respect to the direction of the tapes in the adjacent sheet.
- the direction of tapes within the compressed stack is not unidirectional. This means that in the stack as a whole, tapes are oriented in different directions.
- the tapes in a sheet are unidirectionally oriented, and the direction of the tapes in a sheet is rotated with respect to the direction of the tapes of other sheets in the stack, more in particular with respect to the direction of the tapes in adjacent sheets. Good results are achieved when the total rotation within the stack amounts to at least 45 degrees. Preferably, the total rotation within the stack amounts to approximately 90 degrees.
- the stack comprises adjacent sheets wherein the direction of the tapes in one sheet is perpendicular to the direction of tapes in adjacent sheets.
- the ballistic-resistant panel according to the invention which comprises an inorganic strike face and a ballistic resistant moulded article may be manufactured by various methods.
- a ballistic-resistant moulded article is man ⁇ ufactured, and then combined with the inorganic strike face.
- the ballistic-resistant panel is manufac ⁇ tured in a single step.
- a ballistic- resistant moulded article according to the invention is manufac ⁇ tured by a method claims comprising the steps of
- a ballistic resistant moulded article by stack ⁇ ing sheets comprising reinforcing tapes in such a manner that the direction of the tapes within the compressed stack is not unidirectional to form a stack of sheets, wherein the stack of sheets comprises a high-density polyethylene (HDPE) as matrix material, and compressing the stack of sheets to form a ballis ⁇ tic resistant moulded article, and
- HDPE high-density polyethylene
- the ballistic-resistant moulded article may be manufactured by methods used in the art, e.g., as described in WO2009/109632. Suitable methods include the manufacture of sheets, stacking the sheets in such a manner that the direction of the tapes within the compressed stack is not unidirectional, and compressing the stack, wherein it is ensured during manufacture that the layer structure and matrix content of the article are obtained. For this, reference is made to what has been stated above. Compress ⁇ ing can be done under pressure, e.g., of at least 0.5 MPa.
- Compression can also be performed under vacuum.
- the temperature during compression is selected such that the matrix material is brought above its softening or melting point, if this is necessary to cause the matrix to help adhere the tapes and/or sheets to each other.
- Compression at an elevated temperature is intended to mean that the moulded arti ⁇ cle is subjected to the given pressure for a particular
- the required compression time and compression temperature depend on the nature of the tape and matrix material and on the thick ⁇ ness of the moulded article and can be readily determined by the person skilled in the art.
- cooling under pressure is in ⁇ tended to mean that the given minimum pressure is maintained during cooling at least until so low a temperature is reached that the structure of the moulded article can no longer relax under atmospheric pressure. It is within the scope of the skilled person to determine this temperature on a case by case basis. Where applicable it is preferred for cooling at the given minimum pressure to be down to a temperature at which the organ ⁇ ic matrix material has largely or completely hardened or
- the pressure during the cooling does not need to be equal to the pressure at the high temperature.
- the pressure should be monitored so that appropriate pres ⁇ sure values are maintained, to compensate for decrease in pressure caused by shrinking of the moulded article and the press .
- the stack may be made starting from loose sheets. Loose sheets are difficult to handle, howev ⁇ er, in that they easily tear in the direction of the tapes. It is therefore preferred to make the stack from consolidated sheet packages containing from 2 to 8, as a rule 2, 4 or 8.
- consolidated sheet packages containing from 2 to 8, as a rule 2, 4 or 8.
- Consolidated is intended to mean that the sheets are firmly at ⁇ tached to one another. Very good results are achieved if the sheet packages, too, are compressed.
- the sheets may be consoli ⁇ dated by the application of heat and/or pressure, as is known in the art .
- the thus-obtained ballistic resistant moulded article can be combined with the inorganic strike face via methods known in the art. This can be done, e.g., using an adhesive. If so desired, bonding layers may be present between the ballistic-resistant moulded article and the inorganic strike face, to improve the connection between the two.
- the bonding layer may, e.g., be a an adhesive film layer connected to the ballistic-resistant moulded article, which serves as a carrier for the adhesive layer.
- the structural integrity of the ballistic- resistant moulded article may be improved by applying stitching through the article.
- the ballistic- resistant panel is manufactured by a process comprising the steps of - providing an inorganic strike face, stacking sheets comprising reinforcing tapes onto the back side of the strike face in such a manner that the direction of the tapes within the compressed stack is not unidirectional to form a stack of sheets, wherein the stack of sheets comprises a high-density polyethylene (HDPE) as matrix material, and
- HDPE high-density polyethylene
- This embodiment has the advantage that the shape of the ballis- tic-resistant moulded article is matched exactly to the shape of the inorganic strike face.
- Compres ⁇ sion under vacuum may be preferred in this embodiment, because it ensures that a homogeneous pressure is applied irrespective of the shape of the inorganic strike face.
- a bonding layer may be applied between the inorganic strike face and the stack of sheets comprising reinforcing tapes.
- the bond ⁇ ing layer lay e.g., be a thin fabric layer connected to the ballistic-resistant moulded article, which serves as a carrier for the adhesive layer.
- tape as used in the present invention is an object of which the length is larger than the width and the thickness, while the width is in turn larger than the thickness.
- the ratio between the width and the thickness is more than 10:1, in particular more than 20:1, more in particular more than 50:1, still more in particular more than 100:1.
- the maximum ratio between the width and the thickness is not critical to the present invention. It generally is at most 1000:1, depending on the tape width.
- the width of the tape used in the present invention is at least 2 mm, in particular at least 10 mm, more in particular at least 20 mm.
- the width of the tape is not critical and may generally be at most 500 mm.
- the thickness of the tape is generally at least 8 microns, in particular at least 10 microns.
- the thick ⁇ ness of the tape is generally at most 150 microns, more in particular at most 100 microns.
- the tapes used in the present invention have a linear density of at least 500 dtex, in particular at least 1000 dtex, more in particular at least 3000 dtex, still more in par ⁇ ticular at least 5000 dtex, even more in particular at least 10000 dtex, or even at least 15000 dtex.
- Higher dtex tapes have the advantages that fewer tapes have to be used to obtain an ar ⁇ ticle of a certain areal weight. This is not only process efficient, but may also reduce the risk of edge effects.
- the ratio between the length and the width of the tapes used in the present invention is not critical. It depends on the width of the tape and the size of the ballistic resistant moulded ar- ticle.
- the ratio between length and width is at least 1. As a general value, a maximum length to width ratio of 1 000 000 may be mentioned.
- any natural or synthetic tapes may in principle be used in the present specification. Use may be made of for instance tapes made of metal, semimetal, inorganic materials, organic materials or combinations thereof.
- the tapes bodies be ballistically effective, which, more specifically, re- quires that they have a high tensile strength, a high tensile modulus and a high energy absorption, reflected in a high energy-to-break.
- the tapes used in the present invention have a tensile strength of at least 1.0 GPa, a tensile modulus of at least 40 GPa, and a tensile energy-to-break of at least 15 J/g.
- Suitable inorganic tapes having a high tensile strength are for example carbon fibre tapes, glass fibre tapes, and ceramic fibre tapes.
- Suitable organic tapes having a high tensile strength are for example tapes made of aramid, of liquid crystalline polymer, and of highly oriented polymers such as polyolefins, polyvinyl- alcohol, and polyacrylonitrile .
- polyethylene and polypropylene are preferred.
- These polyole ⁇ fins may contain small amounts of one or more other polymers, in particular other alkene-l-polymers .
- the tapes used in the present invention sheet are high-drawn tapes of high-molecular weight linear polyethylene.
- High molecular weight means a weight average molecular weight of at least 400 000 g/mol.
- Linear polyethylene here means polyethylene having fewer than 1 side chain per 100 C atoms, preferably fewer than 1 side chain per 300 C atoms.
- the polyethylene may also contain up to 5 mol % of one or more other alkenes which are copolymerisable therewith, such as propylene, butene, pentene, 4-methylpentene, octene.
- UHMWPE ultra-high mo ⁇ lecular weight polyethylene
- the use of tapes with a molecular weight of at least 1 * 10 6 g/mol may be particularly preferred.
- the maximum molecular weight of the UHMWPE tapes suitable for use in the present invention is not critical. As a general value a maximum value of 1 * 10 8 g/mol may be mentioned.
- the molecular weight distribution and molecu- lar weight averages (Mw, Mn, Mz) can be determined as described in WO2009/109632.
- the tensile strength of the tapes is at least 1.2 GPa, more in particular at least 1.5 GPa, still more in par- ticular at least 1.8 GPa, even more in particular at least 2.0 GPa. In one embodiment, the tensile strength of these tapes is at least 2.0 GPa, in particular at least 2.5 GPa, more in par ⁇ ticular at least 3.0 GPa, still more in particular at least 4 GPa. Tensile strength is determined in accordance with ASTM
- the tapes have a tensile modulus of at least 50 GPa. More in particular, the tapes may have a tensile modulus of at least 80 GPa, more in particular at least 100 GPa, still more in particular at least 120 GPa, even more in particular at least 140 GPa, or at least 150 GPa.
- the modulus is determined in accordance with ASTM D7744-11.
- the tapes have a tensile energy to break of at least 20 J/g, in particular at least 25 J/g. In another em- bodiment, the tapes have a tensile energy to break of at least 30 J/g, in particular at least 35 J/g, more in particular at least 40 J/g, still more in particular at least 50 J/g.
- the ten ⁇ sile energy to break is determined in accordance with ASTM
- the polyethylene tapes used in the present invention have a high molecular orientation as is evidenced by their XRD diffraction pattern.
- the tapes have a 200/110 uniplanar orientation parameter ⁇ of at least 3.
- the 200/110 uniplanar orientation parameter ⁇ is defined as the ratio between the 200 and the 110 peak areas in the X-ray diffraction (XRD) pattern of the tape sample as determined in reflection geometry.
- the 200/110 uniplanar orientation parameter gives information about the extent of orientation of the 200 and 110 crystal planes with respect to the tape surface. For a tape sample with a high 200/110 uniplanar orientation the 200 crystal planes are highly oriented parallel to the tape surface. It has been found that a high uniplanar orientation is generally accompanied by a high modulus, high tensile strength and high tensile energy to break.
- the ratio between the 200 and 110 peak areas for a specimen with randomly oriented crystallites is around 0.4.
- the crystallites with indi ⁇ ces 200 are preferentially oriented parallel to the film surface, resulting in a higher value of the 200/110 peak area ratio and therefore in a higher value of the uniplanar orienta- tion parameter.
- This parameter can be determined as described in WO2009/109632.
- the UHMWPE tapes used in one embodiment of the ballistic materi ⁇ al according to the invention have a 200/110 uniplanar
- orientation parameter of at least 3. It may be preferred for this value to be at least 4, more in particular at least 5, or at least 7. Higher values, such as values of at least 10 or even at least 15 may be particularly preferred.
- the theoretical maxi ⁇ mum value for this parameter is infinite if the peak area 110 equals zero. High values for the 200/110 uniplanar orientation parameter are often accompanied by high values for the strength and the energy to break.
- the UHMWPE tapes used in the present inven ⁇ tion have a narrow molecular weight distribution have an Mw/Mn ratio of at most 6. More in particular the Mw/Mn ratio is at most 5, still more in particular at most 4, even more in partic ⁇ ular at most 3.
- the use of materials with an Mw/Mn ratio of at most 2.5, or even at most 2 is envisaged in particular.
- the UHMWPE tapes in particular UHMWPE tapes have a DSC crystallinity of at least
- the DSC crystallinity can be determined as described in WO2009/109632.
- the polyethylene used in this embodiment of the present inven ⁇ tion can be a homopolymer of ethylene or a copolymer of ethylene with a co-monomer which is another alpha-olefin or a cyclic olefin, both with generally between 3 and 20 carbon atoms. Examples include propene, 1-butene, 1-pentene, 1-hexene, 1-heptene, 1- octene, cyclohexene, etc.
- dienes with up to 20 carbon atoms is also possible, e.g., butadiene or 1-4 hexadiene.
- the amount of non-ethylene alpha-olefin in the ethylene homopolymer or copolymer used in the process according to the invention preferably is at most 10 mole%, preferably at most 5 mole ⁇ 6 , more preferably at most 1 mole%. If a non-ethylene alpha-olefin is used, it is generally present in an amount of at least 0.001 mol.%, in particular at least 0.01 mole%, still more in particu ⁇ lar at least 0.1 mole%.
- substantially free from non-ethylene alpha-olefin is preferred.
- the wording substantially free from non-ethylene alpha-olefin is intended to mean that the only amount non-ethylene alpha-olefin present in the polymer are those the presence of which cannot reasonably be avoided.
- the UHMWPE tapes have a polymer solvent content of less than 0.05 wt.%, in particular less than 0.025 wt . ⁇ 6 , more in particular less than 0.01 wt.%.
- the tapes used in the present invention in particular UHMWPE tapes have a high strength in combination with a high linear density.
- the linear density is expressed in dtex. This is the weight in grams of 10.000 metres of tape.
- the tapes used in the invention have a denier of at least 500 dtex, in particular at least 100 dtex, more in particular at least 3000 dtex, even more in particular at least 5000 dtex, more in particular at least 10000 dtex, even more in particular at least 15000 dtex, or even at least 20000 dtex, in combination with strengths of at least 1.0 GPa, in particular at least 1.5 GPa, more in particular at least 2.0 GPa, still more in particular at least 2.5 GPA, more in particular at least 3.0 GPa, still more in particular at least 3.5 GPa, and even more in particular at least 4 GPa.
- the polyethylene tapes are tapes manufactured by a process which comprises sub ⁇ jecting a starting polyethylene with a weight average molecular weight of at least 100 000 gram/mole, an elastic shear modulus
- the starting material for said manufacturing process is a highly disentangled UHMWPE . This can be seen from the combination of the weight average molecular weight and the elastic modulus. For further elucidation .
- the starting polymer has an elastic shear modulus directly after melting at 160°C of at most 1.4 MPa, more in particular at most 1.0 MPa, still more in particular at most 0.9 MPa, even more in particu ⁇ lar at most 0.8 MPa, and even more in particular at most 0.7.
- the wording "directly after melting" means that the elastic mod ⁇ ulus is determined as soon as the polymer has melted, in
- the elastic modulus typically increases from 0.6 to 2.0 MPa in several hours .
- the elastic shear modulus directly after melting at 160°C is a measure for the degree of entangledness of the polymer.
- G N ° is the elastic shear modulus in the rubbery plateau region. It is related to the average molecular weight between entanglements
- Me which in turn is inversely proportional to the entanglement density.
- rho is the density in g/cm3
- R is the gas constant
- T is the absolute temperature in K.
- a low elastic modulus thus stands for long stretches of polymer between entanglements, and thus for a low degree of entanglement.
- the adopted method for the in ⁇ vestigation on changes in with the entanglements formation is the same as described in publications (Rastogi, S., Lippits, D., Peters, G., Graf, R., Yefeng, Y.
- the disentangled polyethylene for use in this embodiment may be manufactured by a polymerisation process wherein ethylene, op ⁇ tionally in the presence of other monomers as discussed above, is polymerised in the presence of a single-site polymerisation catalyst at a temperature below the crystallisation temperature of the polymer, so that the polymer crystallises immediately up ⁇ on formation.
- Suitable methods for manufacturing polyethylenes used in the present invention are known in the art. Reference is made, for example, to WO01/21668 and US20060142521.
- the UHMWPE tapes which may be used in the present invention may be manufactured by solid state processing of the UHMWPE, which process comprises compacting UHMWPE powder, and stretching the resulting compacted sheets to form tapes.
- Suitable methods for solid state processing UHMWPE are known in the art, and de ⁇ scribed, e.g., in WO2009/109632, WO2009/153318 and WO2010/079172 and require no further elucidation here.
- the present invention is illustrated by the following examples, without being limited thereto or thereby.
- a ballistic resistant panel according to the invention was manu ⁇ factured as follows.
- the starting material consisted of UHMW polyethylene tapes com- briefly available as Endumax Tape TA23 from Teijin Endumax .
- the tapes had a width of 133 mm and a thickness of 50 ⁇ .
- the tapes had a tensile strength of 2.0 GPa, a tensile modulus of 188, and a tensile energy to break of 20 J/g .
- UD-sheets were manufactured by aligning tapes in parallel to form a first layer, aligning a further layer of tapes onto the first layer parallel and offset to the tapes in the first layer, and heat-pressing the tape layers to form a UD-sheet .
- a HPDE foil is applied between the two tape layers and on top of the upper tape layer .
- UD-sheets were cross-plied to form a cross-ply sheet .
- 58 cross- ply sheets were stacked and compressed at a temperature of 136- 137C, at a pressure of 60 bar .
- the material was cooled down and removed from the press to form a ballistic-resistant moulded ar ⁇ ticle .
- the article comprised 58 layers of cross-ply sheet, had an areal weight of 12.5 kg/m2 and a matrix content of 9 wt . % .
- the ballistic resistant moulded article thus obtained was com- bined with an inorganic strike face, namely a 7 Alotec 96 SB 7 mm, which is a ceramic aluminium oxide tile with an areal weight of 26.25 kg/m2 and a density of 3.75 g/cm3.
- the panel and the strike face were adhered together using a commercially available adhesive film, viz . Nolax S22.2031. Consolidation of the com- plete ballistic resistant article including inorganic strike face was performed on a vacuum table at 135 °C for 30 minutes.
- the panel was subj ected to ballistic testing in accordance with the VRAM standard APR 2006 and PM 2007 (test level 9) employing AP7.62 mm ammunition ( full metal j acket (FMJ) Armour Piercing (AP) hardened steel core, P80 ) .
- a 63 mm cartridge was used to achieve higher proj ectile velocities .
- the distance between bar ⁇ rel and target was 5 m.
- the tests were carried out at 20C and 90C, the latter to investigate the performance of the panel at higher temperature . The results are presented in Table 1.
- the panel according to the invention showed good performance, both at 20C and at 90C, with only a limited decrease in performance at the higher tempera ⁇ ture .
- the panel showed a good structural performance, with only small trauma, and without delamination occurring .
- Panels were manufactured as described above for Example 1 , e x ⁇ cept that 33 or 36 cross-ply sheets comprising 4 UHMWPE tape layers were used and an 8 mm Alotec 96 SB ceramic aluminium ox- ide tile with an areal weight of 30 kg/m2 and a density of 3.75 g/cm3 was used .
- the panels were tested at 20C according to the method described above, and the results are presented in Table 2.
- the panel showed a good structural performance, with only small trauma, and without delamination occurring .
- a panel was prepared as described in Example 1, except that ra ⁇ ther than cross-ply sheets comprising four tape layers stacked in a 0-0-90-90 degree order, cross-ply sheets comprising four tape layers in a 0-90-0-90 degree order were applied .
- the panel was combined with the 7 mm strike face described above .
- the pan ⁇ el which had an areal weight of 39.3 kg/m2 was tested at 20C according to the method described above, and the results are presented in Table 3.
- a panel according to the invention was prepared analogous to that in described in example 1 using a 7 mm ceramic plate and 60 layers of cross-ply sheets as in example 1.
- a comparative panel was prepared in the same manner, except that instead of an HDPE matrix the panel contained 4 weight percent of a styrene- isoprene-styrene matrix (Kraton) . To obtain the same panel weight 65 layers of polyethylene tape cross-ply were used. Both panels had an areal weight of 39.1 kg/m2.
- the panel ac ⁇ cording to the invention has a higher V50 than the comparative panel . This is particularly surprising since the comparative panel contains more polyethylene tapes and would therefore be expected to show better results .
- Example 5 To further investigate the effect of an HDPE matrix in comparison with a standard elastomeric matrix the following experiment was carried out .
- a panel according to the invention was prepared analogous to that in described in example 1 using a 8 mm ceramic plate and 37 layers of cross-ply sheet .
- a comparative panel was prepared in the same manner, except that instead of an HDPE matrix the panel contained 4 weight percent of a styrene-isoprene-styrene matrix (Kraton) .
- Kraton styrene-isoprene-styrene matrix
- Both panels had an areal weight of about 37.8 kg/m2.
- Figure 1 shows photographs of the strike face and the back face of the panel according to the invention and the comparative pan ⁇ el. Both panels were shot according to NIJ standard 01.0104 level IV with 30.06 AP ammunition at muzzle velocity .
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15179317 | 2015-07-31 | ||
PCT/EP2016/067249 WO2017021143A1 (en) | 2015-07-31 | 2016-07-20 | Ballistic resistant panel |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3329205A1 true EP3329205A1 (en) | 2018-06-06 |
EP3329205B1 EP3329205B1 (en) | 2021-03-24 |
Family
ID=53783093
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16742251.8A Active EP3329205B1 (en) | 2015-07-31 | 2016-07-20 | Ballistic resistant panel |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3329205B1 (en) |
ES (1) | ES2868192T3 (en) |
WO (1) | WO2017021143A1 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009056287A1 (en) * | 2007-10-31 | 2009-05-07 | Dsm Ip Assets B.V. | Material sheet and process for its preparation |
RU2498194C2 (en) * | 2008-03-06 | 2013-11-10 | Тейджин Арамид Б.В. | Bullet-resistant products containing elongated elements |
WO2009141276A1 (en) * | 2008-05-23 | 2009-11-26 | Novameer B.V. | Smart laminates |
-
2016
- 2016-07-20 WO PCT/EP2016/067249 patent/WO2017021143A1/en unknown
- 2016-07-20 EP EP16742251.8A patent/EP3329205B1/en active Active
- 2016-07-20 ES ES16742251T patent/ES2868192T3/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP3329205B1 (en) | 2021-03-24 |
WO2017021143A1 (en) | 2017-02-09 |
ES2868192T3 (en) | 2021-10-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA2662960C (en) | High performance ballistic composites having improved flexibility and method of making the same | |
AU2007204399B2 (en) | Process for the production of a monolayer composite article, the monolayer composite article and a ballistic-resistant article | |
US20100293691A1 (en) | Multilayered material sheet for use in soft ballistics | |
CA2568559A1 (en) | Method of forming adhesive mixtures and ballistic composites utilizing the same | |
WO2015018909A1 (en) | Ballistic resistant sheets, articles comprising such sheets and methods of making the same | |
KR20060110345A (en) | Ballistic-resistant article | |
EP3105528B1 (en) | Ballistic resistant articles comprising tapes | |
US10655940B2 (en) | Ballistic resistant sheet and use of such a sheet | |
WO2018114266A1 (en) | Ballistic-resistant assembly | |
KR102627783B1 (en) | Polyethylene sheets and articles made therefrom | |
EP3329205B1 (en) | Ballistic resistant panel | |
WO2013068351A1 (en) | Ballistic resistant article comprising polyethylene tapes | |
WO2012004392A1 (en) | Ballistic resistant article |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20180228 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20190311 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20201126 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602016054822 Country of ref document: DE Ref country code: AT Ref legal event code: REF Ref document number: 1374912 Country of ref document: AT Kind code of ref document: T Effective date: 20210415 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: VALIPAT S.A. C/O BOVARD SA NEUCHATEL, CH |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: FP |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG9D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210625 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210624 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210624 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2868192 Country of ref document: ES Kind code of ref document: T3 Effective date: 20211021 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210724 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210726 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602016054822 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
26N | No opposition filed |
Effective date: 20220104 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20210731 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210724 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210720 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210720 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210731 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: UEP Ref document number: 1374912 Country of ref document: AT Kind code of ref document: T Effective date: 20210324 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20160720 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210324 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230710 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20230724 Year of fee payment: 8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20230727 Year of fee payment: 8 Ref country code: GB Payment date: 20230720 Year of fee payment: 8 Ref country code: ES Payment date: 20230801 Year of fee payment: 8 Ref country code: CH Payment date: 20230801 Year of fee payment: 8 Ref country code: AT Payment date: 20230719 Year of fee payment: 8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20230721 Year of fee payment: 8 Ref country code: FR Payment date: 20230721 Year of fee payment: 8 Ref country code: DE Payment date: 20230724 Year of fee payment: 8 |