JPH10511049A - 複合材料の製造用のワイヤ予備成形物及びその製造方法 - Google Patents
複合材料の製造用のワイヤ予備成形物及びその製造方法Info
- Publication number
- JPH10511049A JPH10511049A JP8535728A JP53572896A JPH10511049A JP H10511049 A JPH10511049 A JP H10511049A JP 8535728 A JP8535728 A JP 8535728A JP 53572896 A JP53572896 A JP 53572896A JP H10511049 A JPH10511049 A JP H10511049A
- Authority
- JP
- Japan
- Prior art keywords
- wire
- adhesive
- layer
- preform
- fibers
- 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
- 238000000034 method Methods 0.000 title claims abstract description 56
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 39
- 239000002131 composite material Substances 0.000 title claims description 47
- 239000000835 fiber Substances 0.000 claims abstract description 200
- 239000000853 adhesive Substances 0.000 claims abstract description 90
- 230000001070 adhesive effect Effects 0.000 claims abstract description 90
- 230000004888 barrier function Effects 0.000 claims abstract description 71
- 239000000758 substrate Substances 0.000 claims abstract description 58
- 238000000576 coating method Methods 0.000 claims abstract description 21
- 239000011248 coating agent Substances 0.000 claims abstract description 20
- 239000010410 layer Substances 0.000 claims description 141
- VLKZOEOYAKHREP-UHFFFAOYSA-N n-Hexane Chemical compound CCCCCC VLKZOEOYAKHREP-UHFFFAOYSA-N 0.000 claims description 38
- 238000004804 winding Methods 0.000 claims description 35
- 239000012790 adhesive layer Substances 0.000 claims description 25
- 239000002904 solvent Substances 0.000 claims description 19
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 claims description 16
- 229920002367 Polyisobutene Polymers 0.000 claims description 11
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical group [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 10
- 229920003229 poly(methyl methacrylate) Polymers 0.000 claims description 10
- 239000004926 polymethyl methacrylate Substances 0.000 claims description 10
- 239000010936 titanium Substances 0.000 claims description 10
- 229910052719 titanium Inorganic materials 0.000 claims description 10
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 8
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 8
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 7
- 239000004830 Super Glue Substances 0.000 claims description 2
- FGBJXOREULPLGL-UHFFFAOYSA-N ethyl cyanoacrylate Chemical compound CCOC(=O)C(=C)C#N FGBJXOREULPLGL-UHFFFAOYSA-N 0.000 claims description 2
- 239000000463 material Substances 0.000 abstract description 36
- 239000003733 fiber-reinforced composite Substances 0.000 abstract description 8
- 238000010618 wire wrap Methods 0.000 abstract 1
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- 239000011159 matrix material Substances 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 229910052782 aluminium Inorganic materials 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 239000011888 foil Substances 0.000 description 4
- 229920000642 polymer Polymers 0.000 description 4
- 239000012779 reinforcing material Substances 0.000 description 4
- 239000002657 fibrous material Substances 0.000 description 3
- 238000009730 filament winding Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- 208000019901 Anxiety disease Diseases 0.000 description 2
- 230000036506 anxiety Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- VQTUBCCKSQIDNK-UHFFFAOYSA-N Isobutene Chemical group CC(C)=C VQTUBCCKSQIDNK-UHFFFAOYSA-N 0.000 description 1
- 229920000271 Kevlar® Polymers 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 239000004820 Pressure-sensitive adhesive Substances 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000004809 Teflon Substances 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000004581 coalescence Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000001513 hot isostatic pressing Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- -1 polyethylene Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Classifications
-
- 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
- B32B19/00—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/064—Winding wires
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/002—Manufacture of articles essentially made from metallic fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
- B29C53/8016—Storing, feeding or applying winding materials, e.g. reels, thread guides, tensioners
-
- 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
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
-
- 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
- B32B3/10—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 discontinuous layer, i.e. formed of separate pieces of material
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/20—Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12444—Embodying fibers interengaged or between layers [e.g., paper, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12576—Boride, carbide or nitride component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/2936—Wound or wrapped core or coating [i.e., spiral or helical]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/294—Coated or with bond, impregnation or core including metal or compound thereof [excluding glass, ceramic and asbestos]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Metal Extraction Processes (AREA)
- Reinforced Plastic Materials (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Description
Claims (1)
- 【特許請求の範囲】 1.a) 基板を準備し、 b) 前記基板に接着剤を付け、 c) 前記接着剤に複数のワイヤを付け、 d) 前記ワイヤにバリヤー層を付け、 e) 前記バリヤー層に接着剤を付け、 f) 前記接着剤と前記バリヤー層は互いに不溶解性である、複合材料製造用 のワイヤ予備成形物の製造方法。 2. 前記ワイヤ予備成形物は複合材料のための一体の被覆として使用さレル、請 求の範囲1に記載の方法。 3.a) 基板を準備し、 b) 前記基板に接着剤を付け、 c) 前記接着剤に複数の繊維を間隔を隔てた関係に付け、 d) 前記繊維にバリヤー層を付け、 e) 前記バリヤー層を被う接着剤に複数のワイヤを間隔を隔てた関係に付け 、 f) 前記複数のワイヤに前記接着剤を付け、 g) 前記接着剤と前記バリヤー層は互いに不溶解性である、複合材料製造用 のワイヤ予備成形物の製造方法。 4. 接着剤は溶剤としてヘキサンを使用し、バリヤー層は溶剤としてアセトンを 使用する、請求の範囲3に記載の方法。 5. 前記接着剤はポリイソブチレンであり、バリヤー層はポリメチルメタクリレ ートである、請求の範囲3に記載の方法。 6. 前記ワイヤはチタン又はチタン合金である、請求の範囲3に記載の方法。 7. 前記ワイヤは隣接した繊維を受け入れるための凹部を有する断面形状を有す る、請求の範囲3に記載の方法。 8. 前記凹部は角張った形状又は湾曲形状をする、請求の範囲7に記載の方法。 9. 前記湾曲形状の凹部は前記繊維の湾曲形状に対応するように寸法決めされて いる、請求の範囲8に記載の方法。 10. 前記繊維は均一に間隔を隔てられている、請求の範囲3に記載の方法。 11. 前記予備成形物がマンドレルに巻かれて複数の交互の繊維層とワイヤ層を形 成するとき、隣接した繊維間の距離が前記マンドレルに巻かれた次々の繊維層に ついて増すように、前記基板に付けられたとき前記繊維の間隔を隔てた関係を調 整することを更に有する、請求の範囲3に記載の方法。 12. 前記基板をドラムに取り付け、前記ワイヤをそれに巻く、請求の範囲3に記 載の方法。 13. 複数の予備成形物が作られ、引き続く複合材料の製造用に互いに積み重ねら れる、請求の範囲3に記載の方法。 14.a) 基板と、 b) 前記基板上の接着剤層と、 c) 前記接着剤に置かれた複数のワイヤと、 d) 前記ワイヤ上に形成されたバリヤー層と、 e) 前記バリヤー層上に形成された他の接着剤層と、 f) 前記バリヤー層及び各前記接着剤層は互いに不溶解性である、複合材料 製造用のワイヤ予備成形物。 15. 各接着剤層は溶剤としてヘキサンを有し、前記バリヤー層は溶剤としてアセ トンを有する、請求の範囲14に記載のワイヤ予備成形物。 16. 各前記接着剤層はポリイソブチレンを有する、請求の範囲14に記載のワイ ヤ予備成形物。 17. 前記バリヤー層はポリメチルメタクリレートを有する、請求の範囲14に記 載のワイヤ予備成形物。 18. 各前記接着剤層はヘキサン中の1.0重量%のポリイソブチレンであり、前 記バリヤー層はアセトン中の1.0重量%のポリメチルメタクリレートである、 請求の範囲14に記載のワイヤ予備成形物。 19. 前記ワイヤはチタン又はチタン合金である、請求の範囲14に記載のワイヤ 予備成形物。 20.a) 基板と、 b) 前記基板上の接着剤層の第1層と、 c) 前記接着剤に間隔を隔てた関係をなして付けられた複数の繊維と、 d) 前記繊維に付けられたバリヤー層と、 e) 前記第1のバリヤー層に付けられた前記接着剤の第2の層と、 f) 前記複数のワイヤに前記第2の接着剤層に付けられた複数のワイヤと、 g) 前記複数のワイヤに付けられた前記接着剤の第3の層と、を有し、 h) 前記接着剤と前記バリヤー層は互いに不溶解性である、複合材料製造用 のワイヤ予備成形物。 21. 接着剤層は溶剤としてヘキサンを有し、前記バリヤー層は溶剤としてアセト ンを有する、請求の範囲20に記載のワイヤ予備成形物。 22. 前記接着剤はポリイソブチレンを有する、請求の範囲20に記載のワイヤ予 備成形物。 23. 前記バリヤー層はポリメチルメタクリレートを有する、請求の範囲20に記載 のワイヤ予備成形物。 24. 前記接着剤層はヘキサン中の1.0重量%のポリイソブチレンであり、前記 バリヤー層はアセトン中の1.0重量%のポリメチルメタクリレートである、請 求の範囲14に記載のワイヤ予備成形物。 25. 前記ワイヤはチタン又はチタン合金である、請求の範囲20に記載のワイヤ 予備成形物。 26. 前記繊維は炭化珪素である、請求の範囲20に記載のワイヤ予備成形物。 27. 前記繊維は均一に間隔を隔てられている、請求の範囲20に記載のワイヤ予 備成形物。 28. 前記繊維は、前記予備成形物がマンドレルに巻かれて複数の交互の繊維層と ワイヤ層を形成するとき、隣接した繊維間の距離が前記マンドレルに巻かれた次 々の繊維層について増すように、不均一に間隔を隔てられる、請求の範囲20に 記載のワイヤ予備成形物。 29. 前記ワイヤは隣接した繊維を受け入れるための凹部を有する断面形状を有す る、請求の範囲20に記載のワイヤ予備成形物。 30. 前記凹部は角張った形状又は湾曲形状をする、請求の範囲29に記載のワイ ヤ予備成形物。 31. 前記湾曲形状の凹部は前記繊維の湾曲形状に対応するように寸法決めされて いる、請求の範囲30に記載のワイヤ予備成形物。 32.a) 複数の繊維収容ボビンを準備し、 b) 複数のワイヤ収容ボビンを準備し、 c) マンドレル収容回転ドラムを準備し、 d) 前記繊維及びワイヤを、ワイヤの平らな層に隣接した繊維の少なくとも 1つの平らな層を有する層配列をなして引出し、 e) 前記層配列の端を前記マンドレルに取り付け、 f) 前記マンドレルに前記層配列を巻き、 g) 前記層配列の他端を前記巻かれた層配列に取り付け、 h) 前記ドラムからマンドレルを取り外し、 i) 各前記繊維及び各前記ワイヤをマンドレルに巻き、それぞれの繊維及び ワイヤの軸線はドラムの巻き面とほぼ垂直に維持される、複合材料製造用のワイ ヤ予備成形物の製造方法。 33. 前記層配列は繊維及びワイヤの交互の平らな層からなる、請求の範囲32に 記載の方法。 34. 前記層配列は、多プライ層配列を形成するために、前記他端を取り付けるに 先立って前記マンドレルドラムに多巻回に巻かれる、請求の範囲32に記載の方 法。 35. 接着剤は前記取り付け段階に使用される、請求の範囲32に記載の方法。 36. 前記接着剤はシアノアクリレート接着剤である、請求の範囲35に記載の方 法。 37. 前記層配列のワイヤ及び繊維の前記平らな層は前記マンドレルに取り付けら れる、請求の範囲32に記載の方法。 38. 各前記ワイヤは隣接した繊維を受け入れるための凹部を有する断面形状を有 する、請求の範囲32に記載の方法。 39. 前記凹部は角張った形状又は湾曲形状をする、請求の範囲38に記載の方法 。 40. 前記湾曲形状の凹部は前記繊維の湾曲形状に対応するように寸法決めされて いる、請求の範囲39に記載の方法。 41.a) マンドレルと、 b) 一端を前記マンドレルに取り付けたワイヤの第1の平らな層と、 c) 一端を前記マンドレルに取り付けた繊維の第2の平らな層と、を有し、 d) ワイヤの前記第1の平らな層及び繊維の前記第2の層は隣接した積み重 ね関係をなして前記マンドレルに配置され、繊維及びワイヤの隣接した層は互い に重ねられ、前記ワイヤ及び繊維の軸線は前記マンドレルの表面に対してほぼ垂 直である、複合材料製造用のワイヤ繊維予備成形物。 42. 前記繊維は炭化珪素であり、前記ワイヤはチタン又はチタン合金である、請 求の範囲41に記載のワイヤ繊維予備成形物。 43. 前記積み重ね関係は繊維とワイヤの隣接した多層からなる、請求の範囲41 に記載のワイヤ繊維予備成形物。 44. 各前記ワイヤは隣接した繊維を受け入れるための凹部を有する断面形状を有 る、請求の範囲41に記載のワイヤ繊維予備成形物。 45. 前記凹部は角張った形状又は湾曲形状をする、請求の範囲44に記載のワイ ヤ予備成形物。 46. 前記湾曲形状の凹部は前記繊維の湾曲形状に対応するように寸法決めされて いる、請求の範囲45に記載のワイヤ予備成形物。
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US447,584 | 1995-05-23 | ||
US08/447,584 | 1995-05-23 | ||
US08/447,584 US5763079A (en) | 1995-05-23 | 1995-05-23 | Wire preforms for composite material manufacture and methods of making |
PCT/US1996/006761 WO1996037364A1 (en) | 1995-05-23 | 1996-05-09 | Wire preforms for composite material manufacture and methods of making |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH10511049A true JPH10511049A (ja) | 1998-10-27 |
JP3011771B2 JP3011771B2 (ja) | 2000-02-21 |
Family
ID=23776910
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8535728A Expired - Fee Related JP3011771B2 (ja) | 1995-05-23 | 1996-05-09 | 複合材料の製造用のワイヤ予備成形物及びその製造方法 |
Country Status (8)
Country | Link |
---|---|
US (1) | US5763079A (ja) |
EP (1) | EP0883486B1 (ja) |
JP (1) | JP3011771B2 (ja) |
KR (3) | KR100257646B1 (ja) |
AT (1) | ATE226885T1 (ja) |
DE (1) | DE69624595T2 (ja) |
ES (1) | ES2184862T3 (ja) |
WO (1) | WO1996037364A1 (ja) |
Families Citing this family (9)
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JP4049977B2 (ja) | 2000-09-01 | 2008-02-20 | パイオニア株式会社 | 通信端末装置、および通信端末装置に用いられるレンズアダプタ |
US6568061B2 (en) * | 2001-09-21 | 2003-05-27 | Atlantic Research Corporation | Method for controlling composite preform elements during processing |
KR100466885B1 (ko) * | 2001-11-23 | 2005-01-24 | 김영식 | 실리콘 엠보싱 롤러용 중심봉 및 그 제조방법 |
US7118063B2 (en) * | 2004-07-29 | 2006-10-10 | Sequa Corporation | Wire/fiber ring and method for manufacturing the same |
EP2119544B1 (en) * | 2007-01-26 | 2019-05-08 | Toray Industries, Inc. | Process for producing a preform for molding fiber-reinforced resin beam, apparatus for producing the same, and process for producing fiber-reinforced resin beam |
US20100083790A1 (en) * | 2008-10-06 | 2010-04-08 | Graney Jon P | Flywheel device |
KR20130115254A (ko) | 2010-09-14 | 2013-10-21 | 파워 트리 코포레이션 | 복합재 플라이휠 |
EP2796230A1 (en) * | 2013-04-22 | 2014-10-29 | Gervaux Ltd | Method of manufacturing a metallic component by use of wire winding and hot isostatic pressing |
US20210086471A1 (en) * | 2019-09-20 | 2021-03-25 | United Technologies Corporation | Composite material marking and identification |
Family Cites Families (16)
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US3209533A (en) * | 1961-04-21 | 1965-10-05 | John S Light | Rocket shell construction |
US3371488A (en) * | 1966-02-23 | 1968-03-05 | Thiokol Chemical Corp | Segmented rocket motor |
US3573123A (en) * | 1966-05-11 | 1971-03-30 | United Aircraft Corp | Composite high temperature resistant material and method of fabrication |
US3419952A (en) * | 1966-09-12 | 1969-01-07 | Gen Electric | Method for making composite material |
US3540615A (en) * | 1969-01-30 | 1970-11-17 | T O Paine | Panelized high-performance multilayer insulation |
US3900150A (en) * | 1974-08-22 | 1975-08-19 | United Aircraft Corp | Duplex composite tape |
US4041869A (en) * | 1976-07-15 | 1977-08-16 | The United States Of America As Represented By The Secretary Of The Navy | Cook-off liner component |
US4458482A (en) * | 1982-05-17 | 1984-07-10 | The United States Of America As Represented By The Secretary Of The Navy | Rocket motor |
US4478151A (en) * | 1983-02-28 | 1984-10-23 | The United States Of America As Represented By The Secretary Of The Navy | Pressure vessel penetrator |
US4499156A (en) * | 1983-03-22 | 1985-02-12 | The United States Of America As Represented By The Secretary Of The Air Force | Titanium metal-matrix composites |
GB2233752A (en) * | 1989-07-07 | 1991-01-16 | Shell Int Research | Composite pressure vessel |
US5030277A (en) * | 1990-12-17 | 1991-07-09 | The United States Of America As Represented By The Secretary Of The Air Force | Method and titanium aluminide matrix composite |
US5118025A (en) * | 1990-12-17 | 1992-06-02 | The United States Of America As Represented By The Secretary Of The Air Force | Method to fabricate titanium aluminide matrix composites |
US5170007A (en) * | 1991-10-15 | 1992-12-08 | Atlantic Research Corporation | Tailorable roll-bonded insensitive munitions case |
FR2713663B1 (fr) * | 1993-12-15 | 1996-01-12 | Snecma | Procédé de fabrication de pièces axisymétriques en composite à matrice métallique. |
US5624516A (en) * | 1994-12-20 | 1997-04-29 | Atlantic Research Corporation | Methods of making preforms for composite material manufacture |
-
1995
- 1995-05-23 US US08/447,584 patent/US5763079A/en not_active Expired - Lifetime
-
1996
- 1996-05-09 KR KR1019970708288A patent/KR100257646B1/ko not_active IP Right Cessation
- 1996-05-09 JP JP8535728A patent/JP3011771B2/ja not_active Expired - Fee Related
- 1996-05-09 AT AT96915736T patent/ATE226885T1/de not_active IP Right Cessation
- 1996-05-09 ES ES96915736T patent/ES2184862T3/es not_active Expired - Lifetime
- 1996-05-09 EP EP96915736A patent/EP0883486B1/en not_active Expired - Lifetime
- 1996-05-09 DE DE69624595T patent/DE69624595T2/de not_active Expired - Lifetime
- 1996-05-09 WO PCT/US1996/006761 patent/WO1996037364A1/en active IP Right Grant
-
1999
- 1999-11-25 KR KR1019997010954A patent/KR100311743B1/ko not_active IP Right Cessation
- 1999-11-25 KR KR1019997010953A patent/KR100311744B1/ko not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
ES2184862T3 (es) | 2003-04-16 |
KR100257646B1 (ko) | 2000-07-01 |
DE69624595T2 (de) | 2003-03-20 |
ATE226885T1 (de) | 2002-11-15 |
EP0883486B1 (en) | 2002-10-30 |
WO1996037364A1 (en) | 1996-11-28 |
KR100311743B1 (ko) | 2001-10-18 |
US5763079A (en) | 1998-06-09 |
EP0883486A2 (en) | 1998-12-16 |
DE69624595D1 (de) | 2002-12-05 |
KR100311744B1 (ko) | 2001-10-18 |
JP3011771B2 (ja) | 2000-02-21 |
KR19990014942A (ko) | 1999-02-25 |
EP0883486A4 (en) | 1999-12-22 |
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