JPS60500364A - Variable density multilayer composite material - Google Patents
Variable density multilayer composite materialInfo
- Publication number
- JPS60500364A JPS60500364A JP59500227A JP50022784A JPS60500364A JP S60500364 A JPS60500364 A JP S60500364A JP 59500227 A JP59500227 A JP 59500227A JP 50022784 A JP50022784 A JP 50022784A JP S60500364 A JPS60500364 A JP S60500364A
- Authority
- JP
- Japan
- Prior art keywords
- fiber
- layer
- density
- fibers
- intermediate layer
- 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.)
- Pending
Links
- 239000011185 multilayer composite material Substances 0.000 title claims description 7
- 239000000463 material Substances 0.000 claims description 107
- 239000010410 layer Substances 0.000 claims description 91
- 239000000835 fiber Substances 0.000 claims description 46
- 239000004033 plastic Substances 0.000 claims description 44
- 229920003023 plastic Polymers 0.000 claims description 44
- 239000002131 composite material Substances 0.000 claims description 35
- 229910052751 metal Inorganic materials 0.000 claims description 26
- 239000002184 metal Substances 0.000 claims description 26
- 229920006231 aramid fiber Polymers 0.000 claims description 13
- 239000004760 aramid Substances 0.000 claims description 12
- 239000004917 carbon fiber Substances 0.000 claims description 11
- 229920005989 resin Polymers 0.000 claims description 11
- 239000011347 resin Substances 0.000 claims description 11
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 10
- 229920002994 synthetic fiber Polymers 0.000 claims description 9
- 239000003365 glass fiber Substances 0.000 claims description 8
- 239000012209 synthetic fiber Substances 0.000 claims description 8
- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 239000000919 ceramic Substances 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 5
- 229920003235 aromatic polyamide Polymers 0.000 claims description 4
- 239000011247 coating layer Substances 0.000 claims description 4
- 239000003822 epoxy resin Substances 0.000 claims description 4
- 229920000647 polyepoxide Polymers 0.000 claims description 4
- 229920002635 polyurethane Polymers 0.000 claims description 4
- 239000004814 polyurethane Substances 0.000 claims description 4
- 229910052580 B4C Inorganic materials 0.000 claims description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 3
- 229910052796 boron Inorganic materials 0.000 claims description 3
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 229910001018 Cast iron Inorganic materials 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 description 9
- 230000035939 shock Effects 0.000 description 7
- 238000005452 bending Methods 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 229910052719 titanium Inorganic materials 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- 229920002457 flexible plastic Polymers 0.000 description 4
- 239000011229 interlayer Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 3
- 239000004744 fabric Substances 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 2
- 230000001413 cellular effect Effects 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 210000000056 organ Anatomy 0.000 description 2
- 229920002379 silicone rubber Polymers 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229920000914 Metallic fiber Polymers 0.000 description 1
- 229920005830 Polyurethane Foam Polymers 0.000 description 1
- PPWPWBNSKBDSPK-UHFFFAOYSA-N [B].[C] Chemical compound [B].[C] PPWPWBNSKBDSPK-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- NFDFQCUYFHCNBW-SCGPFSFSSA-N dienestrol Chemical compound C=1C=C(O)C=CC=1\C(=C/C)\C(=C\C)\C1=CC=C(O)C=C1 NFDFQCUYFHCNBW-SCGPFSFSSA-N 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000007688 edging Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 229910001234 light alloy Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000001465 metallisation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000011496 polyurethane foam Substances 0.000 description 1
- 235000021395 porridge Nutrition 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63C—SKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
- A63C5/00—Skis or snowboards
- A63C5/12—Making thereof; Selection of particular materials
- A63C5/122—Selection of particular materials for damping purposes, e.g. rubber or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
- B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
- B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/28—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
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- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/14—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by a layer differing constitutionally or physically in different parts, e.g. denser near its faces
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/14—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by a layer differing constitutionally or physically in different parts, e.g. denser near its faces
- B32B5/145—Variation across the thickness of the layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B32/00—Water sports boards; Accessories therefor
- B63B32/57—Boards characterised by the material, e.g. laminated materials
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- 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
- F41H5/0421—Ceramic layers in combination with metal layers
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- 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
- F41H5/045—Layered armour containing metal all the layers being metal 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more layers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/103—Metal fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B32/00—Water sports boards; Accessories therefor
- B63B32/40—Twintip boards; Wakeboards; Surfboards; Windsurfing boards; Paddle boards, e.g. SUP boards; Accessories specially adapted therefor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Textile Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるため要約のデータは記録されません。 (57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】 可変密度多層複合材料 失五淀見 本発明は例えば防弾チョッキ、よろい及び保護壁。[Detailed description of the invention] Variable density multilayer composite material Lost Goyodomi The invention applies, for example, to bulletproof vests, armor and protective walls.
梁、テニス・ラケット、スキー、サーフィン・ボード他の浮き子、貯蔵タンク等 の適用例と併せて金属、特に鋼、又はチタンといった金属のものより高い特に密 度で割った弾性係数と密度で割った破壊強度の比を有する新規な多層複合材料に 関するものである。Beams, tennis rackets, skis, surfing boards and other floats, storage tanks etc. In addition to applications such as metals, especially steel or titanium, which have higher densities than metals, A novel multilayer composite material with a ratio of elastic modulus divided by density to fracture strength divided by density It is related to
先行技術 一層軽量で2例えば成型により一層容易に成型される複合材料によって金属及び 合金といった伝統的な材料と置換するためこの種の通用例に対して既に努力が払 われている。prior art Composite materials that are lighter and more easily formed, e.g. by molding Efforts have already been made towards this type of application to replace traditional materials such as alloys. It is being said.
特に、樹脂で被覆され又は樹脂で含浸され全体的に満足の行く機械的特性を有す るが、著しく高いコストのため適用例上限界があるホウ素繊維で形成された層状 材料が知られている。焼結炭化ホウ素の如き材料は極りて高い耐衝撃性を呈する が、衝撃波の存在下においてはもろい性状を呈す3と共に亀裂が全体的に瞬時の 破壊をもたらすことも知られている。その上これらの材料は1500°C以上の 温度で成型しなければならず、そのコストは極めて高いものである。In particular, those coated with resin or impregnated with resin have overall satisfactory mechanical properties. However, due to its extremely high cost, there are limits to its application. The material is known. Materials like sintered boron carbide exhibit extremely high impact resistance However, in the presence of shock waves, it exhibits brittle properties and the cracks are entirely instantaneous. It is also known to cause destruction. Moreover, these materials can withstand temperatures above 1500°C. It must be molded at high temperatures, and the cost is extremely high.
密度で割つn弾性係数と密度で割った破壊強度の極めて高い比率を有する樹脂若 しくはプラスチック材料にて被覆された高品質の炭素繊維を含む層状材料も知ら れている。然し乍ら、これらの材料は普通の衝撃強度を有し、破壊の点でもろい 。これらの材料は又、極めて高価である。A resin young material with an extremely high ratio of n elastic modulus divided by density and fracture strength divided by density. Alternatively, layered materials containing high-quality carbon fibers coated with plastic materials are also known. It is. However, these materials have moderate impact strength and are brittle in terms of fracture. . These materials are also extremely expensive.
アラミド繊維製の層状材料もが9り荊から市場に出ており、商標’ K E V L A RJで市販されているが。Layered materials made of aramid fibers have been on the market since 900, and have the trademark 'KEV'. It is commercially available as L A RJ.
これらの材料のコストは高く、その圧縮強度と1断強度は不充分である。これら のアラミド繊維と樹脂又はプラスチック材料の複合体は現在防弾チョッキ製造用 の可縮性シートの形態で使用されている。然し乍ら。The cost of these materials is high and their compressive strength and single break strength are inadequate. these Composites of aramid fibers and resin or plastic materials are currently used in the production of bulletproof vests. It is used in the form of a compressible sheet. However.
金属又は合金)の2枚の板材で作製された複合材料も公知である。然し乍ら9機 械的特性と延性材料製MRヒプラスチック材料製コアの間の膨張係数の差が大き いことから、複合材料が機械的応力又は高い温度上昇を受ける際、糊付けが常時 その組立て体を均一にするのを確実にするとは限らない。Composite materials made of two sheets of metal or metal alloys are also known. However, 9 aircraft There is a large difference in mechanical properties and coefficient of expansion between the core made of MR plastic material made of ductile material. gluing is not always possible when composite materials are subjected to mechanical stress or high temperature increases. It does not necessarily ensure that the assembly is uniform.
本発明の開示内容 本発明は競合する複合材料(例えばアラミド繊維に基づく)の機械的特性と少な くとも比肩し得る機械的特性を有し、競合する複合材料より廉く、更に前述した 欠点のない軽量な複合材料を提供するものである。Disclosure of the present invention The present invention improves the mechanical properties of competing composite materials (e.g. based on aramid fibers) and It has comparable mechanical properties, is less expensive than competing composite materials, and It provides a lightweight composite material with no drawbacks.
3 本発明による多層複合材料は織成合成繊維又は金属繊維又はヤーン製の中間層を 含み、プラスチック材料及び少なくとも1つの外側被幕層で含浸され更に前記中 間層の密度がその厚さに亘り変化し、その中間面から外側面まで増加し、中間面 の密度により割られた外側繊維の密度の比が3ないし13になっていることを特 徴としている。3 The multilayer composite material according to the invention has an intermediate layer made of woven synthetic fibers or metal fibers or yarns. comprising, impregnated with a plastic material and at least one outer coating layer; The density of the interlayer varies across its thickness, increasing from its medial surface to its outer surface, and increasing from its medial surface to its outer surface. The ratio of the density of the outer fiber divided by the density of is between 3 and 13. It is a sign.
この材料の可変密度構造によって材料の重量は削減出来2又、特に効果的な1曲 げにおける弾性係数及び曲げとねしりにおける慣性係数が得られる。The variable density structure of this material reduces the weight of the material, making it especially effective for The elastic modulus in bending and the inertia coefficient in bending and torsion are obtained.
この複合材料が狙いとする適用例に従って、中間層に含浸するプラスデック材料 は堅固な(rigidL 半堅固な(semi−rigid)又は可攬性にする ことが出来、外側被覆層は高い表面硬度を有する材料(例えばアルミナ又はセラ ミック)にすることが出来又は織成シートに含浸する材料と同−又はこれと共存 し得る(compati−ble)プラスチック材料で被覆された繊維で形成出 来。PlusDeck material impregnated into the interlayer according to the intended application of this composite material be rigid (semi-rigid) or flexible The outer coating layer can be made of a material with high surface hardness (e.g. alumina or ceramic). The same or coexistence with the material that can be impregnated into the woven sheet Made of fibers coated with compatible plastic material Come.
外側被覆層は例えばホウ素、炭素、ガラス又はアラミドの繊維である。The outer covering layer is, for example, boron, carbon, glass or aramid fibers.
一般に本発明による複合材料は例えば弾丸の衝撃に起因する衝撃波が当該複合材 料を貫通するのを阻止し一部の実施でも弾丸の進入を阻止する。本発明によるこ の複合材料は又、もろく破壊しないという利点を有しており、又、比較的強度の 高い破壊比を有している。In general, the composite material according to the present invention is such that a shock wave caused by, for example, a bullet impacts the composite material. It prevents the bullet from penetrating the material and in some implementations also prevents the bullet from entering. According to the present invention Composite materials also have the advantage of being brittle and unbreakable, and are relatively strong. It has a high fracture ratio.
本発明のたの特徴によれば、この材料は炭素ホウ素。According to another feature of the invention, the material is carbon boron.
4 特表昭GO−500364(3) アルミナ、セラミック、チタン等といった堅固で硬質な材料の板材を間に配設し た状態で相互に固定される前述した形式の織成層を重ねたものから成り、2つの 層の間に配設されたこ九らの堅固な板材はプラスチック材料が充填された間隙に より相互から分離され、その両側の部分的な重なりを提供すべく織成層の反対側 で相互に対し相対的に偏寄っている。4 Special feature Sho GO-500364 (3) Plates made of solid and hard materials such as alumina, ceramic, titanium, etc. are placed in between. It consists of a superposition of woven layers of the type previously described which are fixed to each other in a state in which two These solid plates placed between the layers fill the gaps filled with plastic material. Opposite sides of the woven layer to be more separated from each other and provide partial overlap on both sides and are relatively biased toward each other.
従って、板材の寸法の機能として多かれ少なかれ可焼性があり、且つ防弾チョッ キ又は他の被覆を形成するのに適している構造が得られる。Therefore, as a function of the dimensions of the plate, it is more or less flammable and bulletproof. A structure is obtained which is suitable for forming coatings or other coatings.
本発明の他の特徴によれば、高い表面硬度を有するプラスチック材料の層を含む 外側面を備えた円形、卵形、又は多角形横断面形状の中空棒の形態になった複合 材料が作成される。これらの特性は更に詳細には梁枠、バー、フレーム等の作製 を対象としている。According to another feature of the invention, it comprises a layer of plastic material with high surface hardness. Composite in the form of a hollow rod of circular, oval, or polygonal cross-sectional shape with an external surface Material is created. These characteristics are explained in more detail in the production of beam frames, bars, frames, etc. The target is
更に詳細に言えば、スキーの製造を狙いとしている本発明の更に他の特徴によれ ば、その材料はプラスチック材料で被覆された繊維の個\の層で外側面が被覆さ れる前述した形式の2個の織成層の間に配設でれたエポキシ樹脂の如きプラスチ ック材料の中間層を含む。More particularly, according to still further features of the invention aimed at the manufacture of skis. For example, the material is coated on the outside with a layer of fibers coated with plastic material. A plastic material such as an epoxy resin disposed between two woven layers of the type previously described. includes an intermediate layer of backing material.
上の最良の様式 一例として掲げられる以下の説明において添附図面を参照する。best style above In the following description, which is given by way of example, reference is made to the accompanying drawings.
第1図は本発明による複合材料の第1実施態様の模式的断面図。FIG. 1 is a schematic cross-sectional view of a first embodiment of the composite material according to the present invention.
第2図は、防弾チョッキの提供に本発明を適用する状態を示す模式的断面図。FIG. 2 is a schematic cross-sectional view showing how the present invention is applied to provide a bulletproof vest.
第3図は公知形式の防弾チョッキに補強部材を提供する本発明の別の適用例を示 す模式的断面図。FIG. 3 shows another example of the application of the invention for providing reinforcing elements in a known type of body armor. A schematic cross-sectional view.
第4図はよろい又は保護壁の模式的断面図。FIG. 4 is a schematic cross-sectional view of the armor or protective wall.
第5図は防弾チョッキに対する本発明の改変実施態様の模式的断面図。FIG. 5 is a schematic cross-sectional view of a modified embodiment of the invention for a bulletproof vest.
第6図は本発明による複合材料を使用したセル状梁の模式的断面図。FIG. 6 is a schematic cross-sectional view of a cellular beam using a composite material according to the present invention.
第7図、第8図及び第9図は各一本発明による材料を使った円形、矩形及び卵形 横断面を有する構造の断面図。Figures 7, 8 and 9 each show circular, rectangular and oval shapes made of the material according to the invention. FIG. 3 is a cross-sectional view of a structure with a cross section.
第10図は本発明による材料を使ったスキーの底面の断面図。FIG. 10 is a sectional view of the bottom of a ski using the material according to the invention.
本発明による材料の一実tC例の一部分を模式的断面で示す第1図を最初に参照 する。Reference is first made to FIG. 1, which shows in schematic cross section a portion of an actual tC example of a material according to the invention. do.
この複合材料は織成した合成若しくは金属性繊維又はヤーン12で作製された中 間層10を含み、当該中間層は材料に対する所定の適用例に応して堅固2半堅固 又は可援性の形式に出来るプラスチック材料14でその全体の厚さに亘り且つそ の全体の長さに沿って含浸される。The composite material is made of woven synthetic or metallic fibers or yarns. an interlayer 10, which may be rigid or semi-rigid depending on the given application for the material; or a plastic material 14 which can be made into a supportable form over its entire thickness and is impregnated along its entire length.
料fで被覆された繊維19で作架された材料の少なくとも1つの層16で被覆さ れる。NIOの他方の面も同様にして層16のよう(:で層10に含浸するプラ スチック材料と同−又は当該プラスチック材料と共た可能なプラスチック材料で 被覆されている繊維で形成された材料の層18で被覆される。状況に応じて層1 8は層16の厚さと等しくすることが出来るが゛fi当該厚さと異なる厚さにす ることも出来る。これらの2つの層は等しい密度にするか又は異なる密度にず2 ることが出来る。coated with at least one layer 16 of material strung with fibers 19 coated with material f. It will be done. Similarly, the other side of NIO is coated with a plastic impregnated into layer 10 like layer 16 (:). Possible plastic material that is the same as the stick material or the same plastic material. It is coated with a layer 18 of material formed from coated fibers. Tier 1 depending on the situation 8 can be equal to the thickness of the layer 16, but the thickness can be different from that thickness. You can also do that. These two layers can be of equal density or have different densities. Rukoto can.
中間層10及び外側層16.18はこれらが含浸されるプラスチック材料1m、 c/l相互に近密に接続され。the middle layer 10 and the outer layer 16.18 are impregnated with 1 m of plastic material; c/l are closely connected to each other.
従って、これらの層は複合材料が極めて厳しい機械的力を受ける際引き離された り又は非積層状態にされる危険を何んら伴なわずに固定される。Therefore, these layers are pulled apart when the composite is subjected to extremely severe mechanical forces. fixed without any risk of being bent or unlaminated.
中間層10の密度はその厚さに亘って変化しく外側層16及び18に平行な)そ の中間面からその外側面に向かって増加する。外側層16及び18は各\実質的 に一定の密度にすることが出来、又はそれらの密度は外側に向かって増加させる ことが出来るので本発明による多層複合材料の厚さを横切り中間面の密度により 割った外側繊維の密度の比率は3ないし13になっている。The density of the middle layer 10 varies over its thickness (parallel to the outer layers 16 and 18). increases from the middle surface to its outer surface. The outer layers 16 and 18 are each substantially can be of constant density, or their density increases outwards. Due to the density of the intermediate plane across the thickness of the multilayer composite material according to the present invention, it is possible to The density ratio of the split outer fibers is 3 to 13.
この複合材料は加圧状態下の熱開成型又は冷間成型により又は層10を形成する 1個以上の合成又は金属織成シート及び層16と層18を形成する繊維の板材又 は織成シートを含む金型内にプラスチック材料を射出することにより形成可能で ある。中間層10は複数個の金属又は合成織成シートで成型出来又は中間層は金 属又は合成繊維又はヤーンの3次元織成により形成可能である。前畠己繊維又は ヤーンは直径0.2mm以下のステンレス鋼線、又は機械的性能の高い軽合金線 。The composite material is formed into layer 10 by hot-open molding or cold molding under pressure. one or more synthetic or woven metal sheets and fibrous plates forming layers 16 and 18; can be formed by injecting plastic material into a mold containing a woven sheet. be. The intermediate layer 10 can be molded from a plurality of metal or synthetic woven sheets, or the intermediate layer can be made of gold. It can be formed by three-dimensional weaving of synthetic or synthetic fibers or yarns. Maebata Mi Fiber or The yarn is stainless steel wire with a diameter of 0.2 mm or less, or light alloy wire with high mechanical performance. .
又は金属繊維若しくはヤーンと合成繊維若しくはヤーンの混合物若しくはその組 合せ体にすることが出来る。or a mixture or combination of metal fibers or yarns and synthetic fibers or yarns. Can be combined.
層】6及0゛18を形成するため使用される繊維はホウ素、炭素、ガラス、アラ ミド等で作成可能である。The fibers used to form layers 6 and 0 and 18 include boron, carbon, glass, and aluminum. It can be created using Mido etc.
中間層10及び層16.18を含浸させるため使用される材料は冷間中に熱又は 圧力を加えることにより重合される樹脂、即ちシリコーン・エラストマー、ポリ ウレグン等にするこヒが出来る。The materials used to impregnate intermediate layer 10 and layers 16.18 are heated or Resins that are polymerized by applying pressure, i.e. silicone elastomers, poly You can make porridge to make things like uregun.
本発明による複合材料は金属特に鋼及びチタンの持つ比率より高い、密度により 割られた弾性係数と密度により割られた破壊強度の比を有する本質的特性を備え 、特に層10が鋼製ヤーンで織成される場合、当該複合材料は又機械的及び音響 的振動に対する極めて良好な減衰係数、極めて高い破壊tヒ3段階的及び部分的 破壊モードも備えている。The composite material according to the invention has a density that is higher than that of metals, especially steel and titanium. with the intrinsic property of having the ratio of the modulus of elasticity divided by the breaking strength divided by the density , especially if layer 10 is woven with steel yarns, the composite material also has mechanical and acoustic properties. Extremely good damping coefficient for physical vibrations, extremely high destructive resistance 3 stages and partial It also has a destruction mode.
ここで防弾チョッキの製造に対する本発明の通用例を示している第2図を参照す る。Reference is now made to FIG. 2, which shows an example of the application of the invention to the manufacture of bulletproof vests. Ru.
第2図に示された構造は可変密度の複数個のシート20を含み、当該シートは本 例の場合9枚数が5枚であり、各シートは可、1ル性プラスチツク材料で含浸さ れた織成金属若しくは合成繊維若しくはヤーンの層若しくはシートを含み5片側 面又は両側面に同じ可1ル性プラスチック材料で被覆された繊維の層を任意に含 む。The structure shown in FIG. 2 includes a plurality of sheets 20 of variable density, the sheets being In the example, the number of 9 sheets is 5, and each sheet is impregnated with a flexible plastic material. 5 sides containing layers or sheets of woven metal or synthetic fibers or yarns Optionally includes a layer of fibers coated on one or both sides with the same flexible plastic material. nothing.
チタン又は炭化ホウ素の如き極めて硬い材料製の板材22がシート20の間で相 互に分離された状態で配設され2部分的にシートのいずれか一方の側に重なるよ うな様式でシート20のいずれか一方の側にて相互に片寄って設けである。板材 22は垂直方向で10ないし20cmの長さにし、水平方向で4ないし3cmの 幅にすることが出来る。2枚のシート20の間の板材22の間の間隙24には構 造が全体として成型さd−る隙間し可」ム性プラスチック材料が充填される。第 2図に示された構造の厚さは例えば約4m、mである。シート20に含浸し2間 隙24を充填する可屹性ブラチチック材料は構造の各種構成要素を共に結合する 。この様式で得られた組立て体はチョッキの内側面と外側面を構成する2つの織 物シートの間に設けることが出来る。Plates 22 made of extremely hard material such as titanium or boron carbide are interleaved between the sheets 20. The sheets are arranged so that they are separated from each other and partially overlap on either side of the sheet. They are offset from each other on either side of the sheet 20 in this manner. board material 22 should be 10 to 20 cm long in the vertical direction and 4 to 3 cm in the horizontal direction. It can be made wide. In the gap 24 between the plates 22 between the two sheets 20, there is a structure. The entire structure is molded and the gaps are filled with a flexible plastic material. No. The thickness of the structure shown in FIG. 2 is, for example, approximately 4 m, m. Impregnate sheet 20 for 2 hours The flexible brachytic material filling the gaps 24 binds the various components of the structure together. . The assembly obtained in this manner consists of two fabrics forming the inner and outer surfaces of the vest. It can be provided between the material sheets.
第2図に示された構造は半堅固な形式のものでありそれ自体1人の胸と背中の曲 率半径に適合する。この半堅固性は又、衝撃帯域におけるチョッキの変形と変位 により弾丸の運動エネルギーの一部分を吸収することも出来る。更に、シー)2 0を構成する複合材料の構造は衝撃に起因する衝撃波の横方向の広がりを回避出 来るようにし、かくして体の繊細な部分や器官を保護し、又、衝撃波を直接受け ない1枚以上の板材22の破壊を防止することも出来る。The structure shown in Figure 2 is of a semi-rigid type and as such it is capable of bending the chest and back of a person. Fits the radius. This semi-rigidity also reduces deformation and displacement of the vest in the impact zone. It can also absorb a portion of the bullet's kinetic energy. Furthermore, C)2 The structure of the composite material that makes up 0 avoids the lateral spread of shock waves caused by impact. thus protecting sensitive parts and organs of the body and also protecting them from direct shock waves. It is also possible to prevent one or more plates 22 from being destroyed.
第3図は公知形式の防弾チョッキを補強する構造を示す。この構造は本発明によ る複合材料製の波型板材26の形態になっており、当該板材は例えばアラミド繊 維の複数枚の重ね合せたシート28により外側又は衝撃を受ける側に形成された ポケット内及び把持布30により体側に設置される。波型板材26は半堅固プラ スチック材料で含浸された金属ヤーン中間層、任官、の適当な手段2例えばプラ ズマ・トーチ又は金属化により外側面上に蒸着可能なセラミック又はアルミナの 如き極めて硬い材料製の外側被覆層32を含む。波型板材26は本発明による複 合材料製で密度の異なる複数枚の重ねたシートの形態にすることが出来1把持布 と接触している板材の液部の隆起部は平坦にされている二とが有利である。FIG. 3 shows a structure for reinforcing a body armor of a known type. This structure is according to the present invention. It is in the form of a corrugated plate material 26 made of a composite material, and the plate material is made of, for example, aramid fiber. Formed on the outside or on the impact side by a plurality of overlapping sheets 28 of fiber. It is installed inside the pocket and on the side of the body by the gripping cloth 30. The corrugated plate material 26 is semi-rigid plastic. Metal yarn interlayer impregnated with a stick material, suitable means 2 for example plastic Ceramic or alumina that can be deposited on the external surface by Zuma torch or metallization It includes an outer covering layer 32 made of a very hard material such as. The corrugated plate material 26 is a composite material according to the present invention. Made of composite material, it can be made into multiple stacked sheets with different densities. 1 Gripping cloth Advantageously, the ridges of the liquid part of the plate which are in contact with the plate are flattened.
この構造は通常アラミド繊維製の公知の防弾チョッキのポケット内に入れられる 鋼板と置換する目的に使用可能である。これらの鋼板は重過ぎること及び人体の 繊細な器官に極めて危険な衝撃波を伝える特別の欠点を有している。This structure is usually placed inside the pocket of a known bulletproof vest made of aramid fibers. It can be used to replace steel plates. These steel plates are too heavy and It has the special drawback of transmitting shock waves that are extremely dangerous to delicate organs.
例えば、車両又はアプローチ・シールド等、よろい又は保護壁の一部を模式的断 面で示す第4図をここで参照する。当該壁は極めて高い機械的性能を有するチタ ン又は他の任意の材料製の外側板材361本発明による複合材料製の内側板材3 8.同様に本発明による複合材料製の中間波型板材40を含む。内側板材38は 堅固なプラスチック材料で含浸された織成金属層で作製され、同じ堅固なプラス チック材料で含浸された繊維を基礎にする材、2料の層を有する少なくヒも1つ の面が備えである。中間の波型板材40は半堅固なプラスチック材料で含浸され た織成金属層で作間しである。For example, schematically cutting away parts of armor or protective walls, such as vehicles or approach shields. Reference is now made to FIG. The wall is made of titanium, which has extremely high mechanical performance. an outer plate 361 made of carbon or any other material; an inner plate 3 made of a composite material according to the invention; 8. Also included is an intermediate corrugated board 40 made of composite material according to the invention. The inner board material 38 is Made with a woven metal layer impregnated with a tough plastic material, the same tough plus A material based on fibers impregnated with a tic material, having at least one layer of two materials. This aspect is preparation. The intermediate corrugated board 40 is impregnated with a semi-rigid plastic material. It is lined with woven metal layers.
外側板材36に与えられる衝撃の影響下で波型板材40は平坦化する傾向があり 、その衝撃又は打撃の機械的エネルギーの1つの層を吸収し、衝撃波をやわらげ る:1:がτう、一方、内側板材38に対する衝撃波の伝達を防止するか又は少 なくとも削減するニヒかで゛さ、当該内側板材はそれ自体で又2伝達され得る衝 撃波を吸収するニヒが℃きる。Under the influence of the impact applied to the outer plate 36, the corrugated plate 40 tends to flatten. absorbs one layer of the mechanical energy of that impact or blow, softening the shock wave. 1: On the other hand, the transmission of shock waves to the inner plate 38 is prevented or reduced. In order to at least reduce the impact, the inner plate itself also The Nihi that absorbs the attack wave becomes colder.
第5回は本発明による異なる防弾チョッキの一部分度発泡ポリウレタンで壱浸さ れる織成金属繊維又はヤーン製の中間層42を含む。中間F!42の両側面はガ ラス繊維又はアラミド繊維といった繊維製の一連の可撓性ノート44で被覆され 、当該繊維には例えば中間層42に対し使用されるのと同じシリコーン・エラヌ l・マーヒいった可撓性プラスチック材料が含浸される。Part 5 of different bulletproof vests according to the present invention is partially soaked with polyurethane foam The intermediate layer 42 is made of woven metal fibers or yarns. Intermediate F! Both sides of 42 are Covered with a series of flexible notes 44 made of fibers such as lath fibers or aramid fibers. , the fibers may include, for example, the same silicone elastomer material used for the intermediate layer 42. A flexible plastic material such as L. Mahi is impregnated.
中間層42を構成する金属繊維又はヤーンの密度はその中間面からその外側面ま で増加し、当該密度は例えば中間面では約0,6てあり、外側面では約3であり 2平均的密度は1ないし2の間になっている。層42の各面を覆うンーI・44 の枚数はマないし10が有利であり、各シートは約0,2ないし0,4ミリの厚 さになっている。シート44は異なる繊維で作製可能であり。The density of the metal fibers or yarns constituting the intermediate layer 42 varies from its intermediate surface to its outer surface. For example, the density is about 0.6 on the middle surface and about 3 on the outer surface. 2 The average density is between 1 and 2. 44 covering each side of layer 42 Advantageously, the number of sheets is from 1 to 10, each sheet having a thickness of approximately 0.2 to 0.4 mm. It's getting dark. Sheet 44 can be made of different fibers.
層42の内側面のシートは例えばガラス繊維であり。The sheet on the inner surface of layer 42 is, for example, glass fiber.
一方2層42の外側面のシードは炭素繊維、アラミド繊維又は金属繊維でもある 。Meanwhile, the seeds on the outer surface of the second layer 42 are also carbon fibers, aramid fibers or metal fibers. .
一例として、チョッキの外側面にあるアラミド繊維のシート44は各\厚さが0 .3ミリで重さが1平方メートルあたり約285 g (g/m2)にすること が出来、チョッキの内側に設けられた慣用的な織成に対するガラス繊維製のシー ト44は各\厚さが約0,2ミリで重さが約200 g / m であり、これ らの各種のシートはプラスチック材料で含浸されない。As an example, each sheet of aramid fiber 44 on the outer surface of the vest has a thickness of 0. .. 3 mm and weighs approximately 285 g per square meter (g/m2) The result is a fiberglass sheath as opposed to the traditional weave on the inside of the vest. Each 44 has a thickness of about 0.2 mm and a weight of about 200 g/m, and this These various sheets are not impregnated with plastic material.
第5図の構造は王としてアラミド横部又は炭素繊維で作製された同様の1膏造の 係数に少なくとも等しくなっている曲げにおける弾性係数1曲げとねじりにおけ る弾性係数を有し、この構造の全体的な密度又は質量は実質的には各種の場合に おける値と同じである。第5図に示された構造は炭素繊維又はアラミド繊維製の 同じ構造より廉くなっている。The structure in Figure 5 is similar to one made of aramid laterals or carbon fiber as the king. The modulus of elasticity in bending is at least equal to 1 in bending and torsion The overall density or mass of this structure is substantially smaller in each case. is the same as the value in The structure shown in Figure 5 is made of carbon fiber or aramid fiber. It is cheaper than the same structure.
本発明による複合材料は又、7、サーフィン・ボード又は他の浮き子を作製する のにも使用可能であり、この場合材料の中間層の密度により割られた外側繊維の 密度の比は好適には3ないし5の間であり、中間層は1ないし5ミリの厚さで好 適には発泡ポリウレタン又は樹脂で含浸され、当該樹脂は中空ガラス又は数十分 の1ミリの直径を備えたエラストマー球体により軽くされ、外側層は炭素繊維又 はアラミド繊維又はガラス繊維、又は合成繊維の3次元織成シートである。Composite materials according to the invention can also be used to make surfing boards or other floats. It can also be used for the outer fibers divided by the density of the middle layer of the material. The density ratio is preferably between 3 and 5, and the intermediate layer is preferably between 1 and 5 mm thick. It is suitably impregnated with foamed polyurethane or resin, and the resin is filled with hollow glass or several tens of minutes. The outer layer is made of carbon fiber or is a three-dimensional woven sheet of aramid fibers, glass fibers, or synthetic fibers.
本発明による複合材料は貯蔵タンク又は多室型浮き子の製造にも使用可能であり 、従って中間面の密度により割られた外側繊維の密度の比は好適には4ないし7 であり、外側層は織成金属繊維又はヤーンのシートによって及び炭素、アラミド 又はガラス繊維の織成ノートによって構成される。The composite material according to the invention can also be used to manufacture storage tanks or multichamber floats. , so the ratio of the density of the outer fibers divided by the density of the intermediate plane is preferably between 4 and 7. and the outer layer is formed by a sheet of woven metal fibers or yarns and carbon, aramid. Or constructed by woven glass fiber notes.
場合には中間面の密度により割られた外側繊維の密度の比は好適には6ないし1 3であり、エラストマー樹脂の層は前述した中間層と外側層の間に設けることが 出来る。従って、これらの外側層はアモルファス鋳鉄の織成テープ層、及び/又 はニラサル又はコバルト母材合金の板材、及び/又はプラズマ・トーチによって 蒸着されるのが好ましいセラミック又はアルミナ層で作製可能であり、金属繊維 又は合成繊維のシートは外側層とエラストマー樹脂の層の間に任意に配設される 。In this case, the ratio of the density of the outer fibers divided by the density of the intermediate plane is preferably between 6 and 1. 3, and the elastomer resin layer may be provided between the aforementioned intermediate layer and outer layer. I can do it. These outer layers may therefore be woven tape layers of amorphous cast iron and/or by Nilasal or cobalt-based alloy plate and/or plasma torch. Can be made with ceramic or alumina layers, preferably vapor deposited, with metal fibers or a sheet of synthetic fiber is optionally disposed between the outer layer and the layer of elastomeric resin. .
3 本発明による複合材料は又、管、梁、7レーA等を作輩するのに使用可能である 。例えば、第1図の材料は好適には堅固で高密度のスヤンク7%乞椅つ堅固なポ リウレタン、Filち比較的高い表面硬度を有するこχが好ましいプラスチック 材料のコーティングを少なくともその外側面」二に含む四角形、矩形、多角形1 円形又は卵形の断面を有する棒に成型可能である。こうした。3 The composite material according to the invention can also be used to make pipes, beams, 7-ray A, etc. . For example, the material of FIG. Plastics with relatively high surface hardness such as urethane and fil are preferred. Quadrilaterals, rectangles, polygons containing a coating of material on at least their outer surfaces It can be molded into a bar with a circular or oval cross section. Like this.
棒は中空にすることが出来又は軽量なプラスチック材料例えば高密度の発泡ポリ ウレタンを充填出来る。The rod can be hollow or made of a lightweight plastic material such as high-density polyfoam. Can be filled with urethane.
第6図は一例として掲げてあり、当該図は本昼明による複合材料のセル状梁の模 式的断面図である。Figure 6 is shown as an example, and is a model of a cellular beam made of composite material by Akira Honhiru. It is a formal cross-sectional view.
梁は本発明による複合材料製の2本の棒を並置させることにより作製、され、棒 の矩形横断面が第6図に部分的に示さね、各棒は高密度ポリウレタンの如き堅固 により任意にガラス及び/又は炭素繊維を(シート50の外、側面に対し)含む プラスチック材料の層で被覆される。The beam is made by juxtaposing two bars made of composite material according to the invention, The rectangular cross-section of the rod is partially shown in FIG. optionally containing glass and/or carbon fibers (on the outside, side surfaces of the sheet 50) Covered with a layer of plastic material.
2本の棒50はその垂直長手方向面の1つに沿って並置され、その上部及び底部 の水平面は同じ堅固なプラスチック材料で含浸された織成金属シート52によっ て梁の全範囲に亘り被覆される。2本の棒の間の結合部において各織成金属シー ト52は比較的硬し)外側面層56を構成する前記プラスチック材料で同様にし 4 て含浸された織成金處テープ54て被覆される。梁形底枠は空の状態にすること が出来、又は断熱と防音の改良のため発泡ポリウレタン又は発泡ジエノールを充 填出来る。The two bars 50 are juxtaposed along one of their vertical longitudinal planes, with their top and bottom The horizontal planes of are covered by woven metal sheets 52 impregnated with the same rigid plastic material The entire area of the beam is covered. At the joint between the two bars each woven metal sheet (52 is relatively hard) The plastic material constituting the outer surface layer 56 is similarly 4 A woven metal tape 54 impregnated with the metal is coated. The beam-shaped bottom frame must be empty. or filled with expanded polyurethane or expanded dienol for improved thermal and sound insulation. It can be filled.
本発明による梁は又ハニカム構造ぎ有すること炉゛出来、従って第6図を参照し て前述した様式で相互に組立てられる複数個の並置棒で作製可能である。The beam according to the invention can also have a honeycomb structure, so see FIG. can be made of a plurality of juxtaposed bars assembled together in the manner described above.
第7図、第8図及び第9図は2本発明による複合材料の噴状構造を示し、各管状 構造はポリウレタンの如き堅固なプラスチック材料で含浸された織成金属又は合 成繊維又はヤーンの層で構成されたコア60を含み高い表面硬度を有している。Figures 7, 8 and 9 show two jet-shaped structures of the composite material according to the present invention, each of which has a tubular shape. The structure is made of woven metal or composite impregnated with a tough plastic material such as polyurethane. It includes a core 60 composed of layers of grown fibers or yarns and has high surface hardness.
プラスチック含浸繊維の層66を任意に織成層60の外側面とプラスチック材料 の外側層62の間に設けることが出来、前記層66は織成層60の周わりに巻か れた管又は2本のテープにより構成され相互にlOoないし45°の角度で相互 に交差している。A layer 66 of plastic-impregnated fibers is optionally woven between the outer surface of layer 60 and the plastic material. between the outer layers 62 of the woven layer 60, said layer 66 being wrapped around the woven layer 60. It consists of a tube or two tapes that are connected to each other at an angle of 100 to 45 degrees. intersects with.
第8図において、プラスチック材料64の内側層は補強用リブ68を有し、当該 リブは又射出中にプラスチック材料の流れを改善する効果を有している。同様に して、秤9図に示された構造はこの構造の卵形断面の短かい軸線に沿って走るプ ラスチック補強材70を含む。In FIG. 8, the inner layer of plastic material 64 has reinforcing ribs 68. The ribs also have the effect of improving the flow of plastic material during injection. similarly Therefore, the structure shown in Figure 9 has a prism running along the short axis of the oval cross section of this structure. Includes a plastic reinforcement 70.
l5 第7図の構造は例えばスキーのストック、ヨツトのマスト及び管構造に適用可能 である。第8図の構造は例えばテニス・ラケットのフレームの製造及び適当な高 さ7幅の比を有するスキーの製造に適用可能である。l5 The structure shown in Figure 7 can be applied to ski poles, yacht masts, and pipe structures, for example. It is. The structure shown in Figure 8 can be used, for example, in the manufacture of tennis racket frames and It is applicable to the production of skis with a width ratio of 7.
第9図の構造は例えば水力タービン又は風車用の羽根の製造に通用可能である。The structure of FIG. 9 can be used, for example, in the production of blades for water turbines or windmills.
こILらの構造において内側の空間は空にするか又は約0.2の密度を有する軽 量な材料を充填出来る。In this IL et al. structure, the inner space is either empty or filled with a light material having a density of about 0.2. Can be filled with a large amount of material.
第10図は本発明による複合材料で作表された構造の一部分を示す断面図である 。当該構造はエポキシ樹脂の如きプラスチック材料製でプラスチック材料が含浸 された金属繊維又はヤーンの2枚の織成層74の間に設置され5タト側面が各\ エポキシ樹脂の如きプラスチック材料の層76で被覆され、それ自体が樹脂含浸 繊維製の材料で作成されたM2Sで被覆され6中間層72を含み、繊維はアラミ ド、炭素又はガラス繊維等である。FIG. 10 is a cross-sectional view showing a part of a structure made of a composite material according to the present invention. . The structure is made of plastic material such as epoxy resin and is impregnated with plastic material. placed between two woven layers 74 of metal fibers or yarns with 5 strips on each side. coated with a layer 76 of plastic material such as epoxy resin, itself impregnated with resin. 6 intermediate layers 72 coated with M2S made of fiber material, the fibers are aramid carbon, glass fiber, etc.
この構造は壁、特に自動車の車体の製造及びスキー0図の構造は厚でか2ないし 3ミリでスキーの全長にした構造は曲げとねじりの振動を極めて良好に減衰させ 、ねじりの点で極めて堅固であり、こうして好ましいエツジング′玄7rニア。This structure is used in walls, especially in the manufacture of automobile bodies and in the construction of skis, with a thickness of only 2 or 2 mm. The 3mm full-length ski structure provides excellent damping of bending and torsional vibrations. , is extremely rigid in terms of torsion and is thus a preferred edging.
162 FIG、6 国際調査報告162 FIG.6 international search report
Claims (1)
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Application Number | Priority Date | Filing Date | Title |
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FR8220881 | 1982-12-13 | ||
FR8220881A FR2537502B1 (en) | 1982-12-13 | 1982-12-13 | COMPOSITE MATERIAL COMPRISING A FRAMEWORK FORMED BY A WOVEN TABLECLOTH, IMPREGNATED WITH PLASTIC MATERIAL AND PROVIDED WITH AT LEAST ONE EXTERIOR COATING LAYER |
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JPS60500364A true JPS60500364A (en) | 1985-03-22 |
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JP59500227A Pending JPS60500364A (en) | 1982-12-13 | 1983-12-12 | Variable density multilayer composite material |
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AU (1) | AU2332284A (en) |
DE (1) | DE3390383T1 (en) |
FR (1) | FR2537502B1 (en) |
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US4550044A (en) * | 1983-08-08 | 1985-10-29 | Figgie International, Inc. | Ballistic resistant armor panel and method of constructing the same |
IT1218653B (en) * | 1987-04-08 | 1990-04-19 | Ferrari Spa Esercizio Fabbrich | COMPOSITE STRUCTURAL SUPPORTING ELEMENT FOR VEHICLE BODIES AND PROCEDURE FOR ITS MANUFACTURE |
IT1208428B (en) * | 1987-05-05 | 1989-06-12 | Alusuisse Italia S P A Ferrari | STRUCTURAL STRUCTURAL ELEMENT COMPOSITE AND PROCEDURE FOR ITS MANUFACTURE IN PARTICULAR FOR THE REALIZATION OF BODYWORKS OF VEHICLES |
CA1332129C (en) * | 1987-11-21 | 1994-09-27 | Tadao Inabata | Light filler material having damping function and composite material thereof |
FR2625516B1 (en) * | 1988-01-04 | 1990-06-01 | Duflot & Fils | PROTECTIVE TEXTILE BARRIER AGAINST MECHANICAL AND / OR THERMAL ASSAULT |
AT391088B (en) * | 1988-05-26 | 1990-08-10 | Head Sportgeraete Gmbh | SKI WITH DAMPING LAYERS |
EP0378854A1 (en) * | 1989-01-19 | 1990-07-25 | General Electric Company | Expanded fiber composite structure and process for making said structure |
DE69226038T2 (en) * | 1991-04-18 | 1998-10-29 | Suehiro Kogyo Co Ltd | Multi-layer tube |
DE4302409C2 (en) * | 1993-01-28 | 1996-05-30 | Ferriere Belloli & Co | Tension or rock anchors with molded thread and method for producing the same |
FR2716117B1 (en) * | 1994-02-17 | 1997-06-06 | Rossignol Sa | Process for the manufacture of a core ski and ski thus obtained. |
WO2010094053A1 (en) * | 2009-02-19 | 2010-08-26 | Gremarol Pty Ltd | Penetration resistant material |
DE102011101303A1 (en) * | 2011-05-12 | 2012-11-15 | Eads Deutschland Gmbh | Impact protection plate for vehicles, in particular aircraft |
TWI848847B (en) * | 2023-11-08 | 2024-07-11 | 財團法人金屬工業研究發展中心 | Variable density multilayer insulation composite and method of forming the same |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3722355A (en) * | 1965-08-03 | 1973-03-27 | Aerojet General Co | Lightweight armor material |
DE2151015A1 (en) * | 1971-10-08 | 1973-04-19 | Mannesmann Ag | Bullet proof armour plating - for security cars made from reinforced steel and polyamide sandwiched layers |
US3832265A (en) * | 1973-09-20 | 1974-08-27 | Us Army | Ballistic armor of plies of nylon fabric and plies of glass fabric |
DE2651238A1 (en) * | 1976-11-10 | 1978-05-18 | Ver Seidenwebereien Ag | Bullet-proof fabric - is formed from layers of materials using aramid fibres |
ES461189A1 (en) * | 1977-07-29 | 1978-06-01 | Vallcorba Tura | Bullet-proof laminate - comprises glass cloth with aramide layers each side and impregnated with thermosetting resin (PT 24.10.78) |
FR2443397A1 (en) * | 1978-12-08 | 1980-07-04 | Imi Kynoch Ltd | Laminated container of epoxy! and polyamide bonded glass fibres - sandwiching elastomeric layers used for storing dangerous materials e.g. explosives |
-
1982
- 1982-12-13 FR FR8220881A patent/FR2537502B1/en not_active Expired
-
1983
- 1983-12-12 GB GB08420409A patent/GB2141379B/en not_active Expired
- 1983-12-12 WO PCT/FR1983/000250 patent/WO1984002306A1/en active Application Filing
- 1983-12-12 DE DE19833390383 patent/DE3390383T1/en not_active Withdrawn
- 1983-12-12 JP JP59500227A patent/JPS60500364A/en active Pending
- 1983-12-12 AU AU23322/84A patent/AU2332284A/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
GB2141379B (en) | 1986-05-29 |
GB8420409D0 (en) | 1984-09-12 |
FR2537502B1 (en) | 1985-07-19 |
WO1984002306A1 (en) | 1984-06-21 |
FR2537502A1 (en) | 1984-06-15 |
GB2141379A (en) | 1984-12-19 |
AU2332284A (en) | 1984-07-05 |
DE3390383T1 (en) | 1985-01-24 |
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