JP2010516512A - 減衰中間層を有する複合積層板及びその作製方法 - Google Patents
減衰中間層を有する複合積層板及びその作製方法 Download PDFInfo
- Publication number
- JP2010516512A JP2010516512A JP2009547244A JP2009547244A JP2010516512A JP 2010516512 A JP2010516512 A JP 2010516512A JP 2009547244 A JP2009547244 A JP 2009547244A JP 2009547244 A JP2009547244 A JP 2009547244A JP 2010516512 A JP2010516512 A JP 2010516512A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- composite laminate
- layers
- viscoelastic material
- damping
- 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
- 239000002131 composite material Substances 0.000 title claims abstract description 66
- 238000013016 damping Methods 0.000 title claims abstract description 59
- 238000004519 manufacturing process Methods 0.000 title claims description 3
- 239000003190 viscoelastic substance Substances 0.000 claims abstract description 111
- 239000000835 fiber Substances 0.000 claims abstract description 70
- 239000000463 material Substances 0.000 claims abstract description 57
- 230000002787 reinforcement Effects 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims description 26
- 230000009477 glass transition Effects 0.000 claims description 22
- 229920005989 resin Polymers 0.000 claims description 20
- 239000011347 resin Substances 0.000 claims description 20
- 239000004917 carbon fiber Substances 0.000 claims description 17
- 230000003014 reinforcing effect Effects 0.000 claims description 16
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 15
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 12
- 230000004888 barrier function Effects 0.000 claims description 10
- 239000012528 membrane Substances 0.000 claims description 10
- 239000002245 particle Substances 0.000 claims description 10
- 239000004918 carbon fiber reinforced polymer Substances 0.000 claims description 9
- 239000003822 epoxy resin Substances 0.000 claims description 8
- 229920000647 polyepoxide Polymers 0.000 claims description 8
- 229920002994 synthetic fiber Polymers 0.000 claims description 7
- 239000012783 reinforcing fiber Substances 0.000 claims description 6
- 239000004433 Thermoplastic polyurethane Substances 0.000 claims description 5
- 239000012209 synthetic fiber Substances 0.000 claims description 5
- 229920002803 thermoplastic polyurethane Polymers 0.000 claims description 5
- 239000002121 nanofiber Substances 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000002071 nanotube Substances 0.000 claims description 3
- 239000012815 thermoplastic material Substances 0.000 claims description 3
- 238000005452 bending Methods 0.000 claims description 2
- 239000000919 ceramic Substances 0.000 claims description 2
- 239000002105 nanoparticle Substances 0.000 claims description 2
- 239000007788 liquid Substances 0.000 claims 3
- 238000003825 pressing Methods 0.000 claims 2
- 238000000151 deposition Methods 0.000 claims 1
- 239000002759 woven fabric Substances 0.000 claims 1
- 239000012779 reinforcing material Substances 0.000 abstract description 6
- 239000010410 layer Substances 0.000 description 146
- 239000010408 film Substances 0.000 description 12
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 11
- 239000011159 matrix material Substances 0.000 description 10
- 229910052799 carbon Inorganic materials 0.000 description 9
- 239000004744 fabric Substances 0.000 description 9
- 239000011229 interlayer Substances 0.000 description 8
- 239000004593 Epoxy Substances 0.000 description 7
- 239000012071 phase Substances 0.000 description 5
- 229920000642 polymer Polymers 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 239000003365 glass fiber Substances 0.000 description 4
- 229920001169 thermoplastic Polymers 0.000 description 3
- 239000004416 thermosoftening plastic Substances 0.000 description 3
- 238000007796 conventional method Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000007779 soft material Substances 0.000 description 2
- 229920002725 thermoplastic elastomer Polymers 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 101150082208 DIABLO gene Proteins 0.000 description 1
- 102100033189 Diablo IAP-binding mitochondrial protein Human genes 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- 229920000800 acrylic rubber Polymers 0.000 description 1
- 230000009471 action Effects 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
- 239000008346 aqueous phase Substances 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000011074 autoclave method Methods 0.000 description 1
- 238000009727 automated fiber placement Methods 0.000 description 1
- 238000009786 automated tape laying Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000012966 insertion method Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000009940 knitting Methods 0.000 description 1
- 229920000126 latex Polymers 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
- 239000002048 multi walled nanotube Substances 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000021715 photosynthesis, light harvesting Effects 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 230000036316 preload Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000002109 single walled nanotube Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Images
Classifications
-
- 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
- B29C70/04—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
- B29C70/086—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 and with one or more layers of pure plastics material, e.g. foam 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
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin 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
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/144—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers using layers with different mechanical or chemical conditions or properties, e.g. layers with different thermal shrinkage, layers under tension during bonding
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/15—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer being manufactured and immediately laminated before reaching its stable state, e.g. in which a layer is extruded and laminated while in semi-molten state
-
- 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
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/08—Impregnating
-
- 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
-
- 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
- B32B5/28—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 impregnated with or embedded in a plastic substance
-
- 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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/02—Physical, chemical or physicochemical properties
- B32B7/027—Thermal properties
-
- 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
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2075/00—Use of PU, i.e. polyureas or polyurethanes or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
- B29K2307/04—Carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0001—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular acoustical properties
- B29K2995/0002—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular acoustical properties insulating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0046—Elastic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0082—Flexural strength; Flexion stiffness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0091—Damping, energy absorption
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- 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
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B2038/0052—Other operations not otherwise provided for
- B32B2038/0076—Curing, vulcanising, cross-linking
-
- 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
- B32B2250/00—Layers arrangement
- B32B2250/40—Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
-
- 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
-
- 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
-
- 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
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/10—Properties of the layers or laminate having particular acoustical properties
- B32B2307/102—Insulating
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/51—Elastic
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/546—Flexural strength; Flexion stiffness
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/56—Damping, energy absorption
-
- 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
- B32B2313/00—Elements other than metals
- B32B2313/04—Carbon
-
- 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
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—Composite web or sheet
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
- Y10T428/24488—Differential nonuniformity at margin
-
- 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/24995—Two or more layers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Fluid Mechanics (AREA)
- Laminated Bodies (AREA)
- Vibration Prevention Devices (AREA)
- Reinforced Plastic Materials (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
実施形態のこれらの及び更なる特徴、態様及び利点は、下記の図面、説明及び請求項を参照することにより、より良く理解される。
Claims (47)
- カーボン繊維強化プラスチック材料の少なくとも第1及び第2層、及び
第1及び第2層の間に配置され第1及び第2層に同時硬化される、減衰材料及び強化媒体を含む第3層
を含む減衰複合積層板。 - 減衰材料が粘弾性材料を含む、請求項1に記載の減衰複合積層板。
- 第3層の全ての側面が第1及び第2層で囲まれている、請求項1に記載の減衰複合積層板。
- 強化媒体が粘弾性材料に組み込まれた繊維を含む、請求項2に記載の減衰複合積層板。
- 繊維の長さが第1及び第2層の面に対しておおむね直角の方向に延びている、請求項4に記載の減衰複合積層板。
- 繊維がZ繊維である、請求項5に記載の減衰複合積層板。
- 繊維が第1及び第2層に同時硬化される、請求項4に記載の減衰複合積層板。
- 減衰材料が、第1ガラス転移温度を有する第1粘弾性材料を含み、
強化媒体が、第1ガラス転移温度よりも高い第2ガラス転移温度を有する第2粘弾性材料で含浸された繊維を含む
請求項1に記載の減衰複合積層板。 - 減衰材料が、第1ガラス転移温度を有する第1粘弾性材料を含み、
強化媒体が、第1粘弾性材料の中に組み込まれた第2粘弾性材料の粗目織物を含み、第2粘弾性材料のガラス転移温度が、第1粘弾性材料のガラス転移温度よりも高い、
請求項1に記載の減衰複合積層板。 - 強化媒体が減衰材料の中に含まれる含有物を含む、請求項1に記載の減衰複合積層板。
- 含有物が、
細断したカーボン繊維、
繊維房、
Z繊維、
繊維強化樹脂の分割テープ、
セラミックマイクロバルーン、
ナノ繊維、
ナノチューブ
のいずれか1つを含む、請求項10に記載の減衰複合積層板。 - 第1層及び第3層の間に配置される第1バリアと、第2層及び第3層の間に配置される第2バリアとを更に含む、請求項1に記載の減衰複合積層板。
- 強化媒体が第1粘弾性材料からできた網を含む、請求項1に記載の減衰複合積層板。
- 減衰材料が第2粘弾性材料からできており、網に第2粘弾性材料を含浸させている、請求項13に記載の減衰複合積層板。
- 強化媒体が第2及び第3層の間の硬い結合部を含んでいる、請求項1に記載の減衰複合積層板。
- 第3層が穿孔を含み、
硬い接続部が、穿孔内に配置され第1及び第2層の間に延びている樹脂を含む、
請求項15に記載の減衰複合積層板。 - 繊維強化樹脂の少なくとも第1及び第2層、
第1及び第2層の間の粘弾性材料の第3層、ならびに
第3層の中の繊維強化材
を含む、複合積層板構造。 - 粘弾性材料が熱可塑性ポリウレタンである、請求項17に記載の複合積層板構造。
- 繊維強化材が、第1及び第2層に対しておおむね平行である粘弾性材料を通って延びる繊維網を含む、請求項17に記載の複合積層板構造。
- 繊維網に粘弾性材料及びエポキシ樹脂の内の1つを含浸させている、請求項19に記載の複合積層板構造。
- 繊維強化材が、粘弾性材料の中に分散された単繊維を含む、請求項17に記載の複合積層板構造。
- 繊維強化材が、粘弾性材料を強化するための、第1及び第2層の間に延びている複数のZ繊維を含む、請求項17に記載の複合積層板構造。
- 繊維強化材が、第1及び第2層に同時硬化される、請求項17に記載の複合積層板構造。
- 粘弾性材料が第1ガラス転移温度を有し、
繊維強化材が、第1ガラス転移温度よりも高い第2ガラス転移温度を有する粘弾性材料を含む、
請求項17に記載の複合積層板構造。 - 第3層が第1及び第2層に同時硬化される、請求項17に記載の複合積層板構造。
- 第1及び第3層の間に配置される第1バリア層と、第2及び第3層の間に配置される第2バリア層を更に備える、請求項17に記載の複合積層板構造。
- 下記のステップ:
(A)強化媒体を減衰材料の層に組み込むステップ
(B)繊維強化樹脂材料の第1及び第2層の間に減衰材料の層を配置するステップ
(C)減衰材料の層を第1及び第2層と共に同時硬化させるステップ
を含む、減衰複合積層板構造を作製する方法。 - ステップ(C)が、第1及び第2層と、減衰材料の層を圧縮するステップを含む、請求項27に記載の方法。
- ステップ(B)が、
減衰材料の層を第1層に付着させるステップ、及び
その後に、第2層を減衰材料の層の上に形成するステップ
を含む、請求項27に記載の方法。 - ステップ(A)が、強化含有物を液状の粘弾性材料の中に混合させるステップを含む、請求項27に記載の方法。
- ステップ(A)が、強化媒体に粘弾性材料を注入するステップを含む、請求項27に記載の方法。
- ステップ(A)が、
強化合成繊維ウェブを提供するステップ、及び
粘弾性材料膜をウェブにプレスするステップ
を含む、請求項27に記載の方法。 - ステップ(A)が、
強化合成繊維を提供するステップ、及び
繊維に粘弾性材料をコーティングするステップ
を含む、請求項27に記載の方法。 - ステップ(A)が、
第1ガラス転移温度を有する粘弾性材料ウェブを提供するステップ、及び
ウェブに第1ガラス転移温度よりも低い第2ガラス転移温度を有する粘弾性材料を含浸させるステップ
を含む、請求項27に記載の方法。 - ステップ(A)が、ナノ粒子を液状の粘弾性材料に取り入れるステップを含む、請求項27に記載の方法。
- ステップ(A)が、Z繊維を第1及び第2層の間に配置して曲げ剛性を増加させるステップを含む、請求項27に記載の方法。
- ステップ(A)が、ステップ(A)を行う前に、Z繊維を粘弾性膜に挿入するステップを含む、請求項27に記載の方法。
- (A)第1及び第2プリプレグを形成するステップ、
(B)構造に減衰特性を付与する減衰材料層を形成するステップ、
(C)強化媒体を減衰材料層に取り入れるステップ、
(D)第1及び第2プリプレグの間に強化減衰材料の層を配置することによって積層体を形成するステップ
(E)積層体を同時硬化させるステップ
を含む、複合積層板構造を作製する方法。 - (F)ステップ(E)が行われている間に、第1及び第2プリプレグと減衰層を圧縮させる
ステップを更に含む、請求項38に記載の方法。 - ステップ(A)が、カーボン繊維強化樹脂材料の複数の層を積み重ねるステップを含む、請求項38に記載の方法。
- ステップ(B)と(C)が、熱可塑性物質をコーティングした強化繊維のプリプレグを形成することによって行われる、請求項38に記載の方法。
- 強化繊維のプリプレグが、強化繊維ウェブを形成し、このウェブを液状の熱可塑性材料の槽に通すことにより形成される、請求項41に記載の方法。
- ステップ(C)が、分散した強化粒子を含む膜を提供するステップを含み、
ステップ(B)が、膜を第1プリプレグと直接接触させて、膜を第1プリプレグと結合させるステップを含む、
請求項38に記載の方法。 - ステップ(C)が、粘弾性材料膜を強化合成繊維ウェブ上にプレスするステップを含む、請求項38に記載の方法。
- ステップ(C)が、
強化合成繊維を提供し、
繊維を粘弾性材料でコーティングする
ステップを含む、請求項38に記載の方法。 - ステップ(C)が、
第1ガラス転移温度を有する粘弾性材料ウェブを提供し、
ウェブに、第1ガラス転移温度よりも低い第2ガラス転移温度を有する粘弾性材料を含浸させる
ステップを含む、請求項38に記載の方法。 - ステップ(C)が、Z繊維で第1及び第2プリプレグの間を橋渡しするステップを含む、請求項38に記載の方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/656,626 | 2007-01-23 | ||
US11/656,626 US9511571B2 (en) | 2007-01-23 | 2007-01-23 | Composite laminate having a damping interlayer and method of making the same |
PCT/US2007/087267 WO2008115301A2 (en) | 2007-01-23 | 2007-12-12 | Composite laminate having a damping interlayer and method of making the same |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2010516512A true JP2010516512A (ja) | 2010-05-20 |
JP2010516512A5 JP2010516512A5 (ja) | 2013-09-05 |
JP5460333B2 JP5460333B2 (ja) | 2014-04-02 |
Family
ID=39766651
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2009547244A Active JP5460333B2 (ja) | 2007-01-23 | 2007-12-12 | 減衰中間層を有する複合積層板及びその作製方法 |
Country Status (4)
Country | Link |
---|---|
US (2) | US9511571B2 (ja) |
EP (1) | EP2121300B1 (ja) |
JP (1) | JP5460333B2 (ja) |
WO (1) | WO2008115301A2 (ja) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012514545A (ja) * | 2009-01-07 | 2012-06-28 | ヘクセル コンポジット、リミテッド | 改善された複合材料 |
JP2014208457A (ja) * | 2013-03-28 | 2014-11-06 | 福井県 | 積層成形体 |
JP2018138379A (ja) * | 2017-02-24 | 2018-09-06 | 三菱ケミカル株式会社 | 成形品およびその製造方法 |
JP2018206090A (ja) * | 2017-06-05 | 2018-12-27 | 株式会社岩間工業所 | 複合構造体の設計方法及び複合構造体 |
JP2019112053A (ja) * | 2017-12-21 | 2019-07-11 | エアバス オペレーションズ リミテッドAirbus Operations Limited | 空気力学的表面用シールプレート |
WO2019159443A1 (ja) * | 2018-02-13 | 2019-08-22 | 三菱重工業株式会社 | 複合材料の製造方法及び複合材料 |
Families Citing this family (78)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
US10065393B2 (en) | 2006-03-25 | 2018-09-04 | Hexcel Composites Limited | Structured thermoplastic in composite interleaves |
US10618227B2 (en) | 2006-03-25 | 2020-04-14 | Hexcel Composites, Ltd. | Structured thermoplastic in composite interleaves |
US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
US8951923B2 (en) * | 2007-05-23 | 2015-02-10 | The Boeing Company | Hybrid composite structure having damped metallic fibers |
US8029642B2 (en) | 2007-07-27 | 2011-10-04 | The Boeing Company | Tape removal apparatus and process |
US8345269B2 (en) | 2007-09-22 | 2013-01-01 | The Boeing Company | Method and apparatus for measuring the width of composite tape |
US7922856B2 (en) | 2008-01-02 | 2011-04-12 | The Boeing Company | Graphite tape supply and backing paper take-up apparatus |
US8056850B2 (en) * | 2008-01-18 | 2011-11-15 | The Boeing Company | Particle-filled wing-to-body fairing and method for reducing fairing vibrations |
US8292214B2 (en) * | 2008-01-18 | 2012-10-23 | The Boeing Company | Vibration damping for wing-to-body aircraft fairing |
US8557074B2 (en) | 2008-02-27 | 2013-10-15 | The Boeing Company | Reduced complexity automatic fiber placement apparatus and method |
US8986482B2 (en) * | 2008-07-08 | 2015-03-24 | The Boeing Company | Method and apparatus for producing composite structures |
EP2358521B1 (en) | 2008-11-19 | 2016-05-04 | BAE Systems PLC | Fibre reinforced composite |
KR20160149327A (ko) * | 2008-11-26 | 2016-12-27 | 쓰리엠 이노베이티브 프로퍼티즈 컴파니 | 복합 구조체용 표면처리 필름 |
US7981501B2 (en) | 2008-12-02 | 2011-07-19 | GM Global Technology Operations LLC | Laminated composites and methods of making the same |
US20100136866A1 (en) * | 2008-12-02 | 2010-06-03 | Gm Global Technology Operations, Inc. | Laminated composites and methods of making the same |
EP2370250A1 (en) * | 2008-12-15 | 2011-10-05 | 3M Innovative Properties Company | Composite article including viscoelastic layer with barrier layer |
CA2746455C (en) * | 2008-12-15 | 2017-01-03 | 3M Innovative Properties Company | Surfacing film for composites with barrier layer |
MY155107A (en) * | 2009-01-06 | 2015-09-15 | Cytec Tech Corp | Structural composite material with improved acoustic and vibrational damping properties |
US8308101B2 (en) | 2009-03-09 | 2012-11-13 | The Boeing Company | Simplified fiber tensioning for automated fiber placement machines |
US8425710B2 (en) | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
US8454788B2 (en) * | 2009-03-13 | 2013-06-04 | The Boeing Company | Method and apparatus for placing short courses of composite tape |
WO2010118359A2 (en) | 2009-04-10 | 2010-10-14 | Saint-Gobain Performance Plastics Corporation | Acoustic damping composition having elastomeric particulate |
TWI408169B (zh) | 2009-04-10 | 2013-09-11 | Saint Gobain Performance Plast | 聲阻尼組合物 |
DE102009020452B4 (de) * | 2009-05-08 | 2017-12-28 | Airbus Defence and Space GmbH | Verbundbauteil mit Nanoröhren, Verfahren zu dessen Herstellung, Verwendung des Verbundbauteils in einem Transportmittel und Transportmittel mit diesem Verbundbauteil |
BRPI0924616A2 (pt) | 2009-06-11 | 2016-03-01 | Saab Ab | junta compósita para estrutura de avião |
WO2011020841A1 (de) * | 2009-08-17 | 2011-02-24 | Quadrant Plastic Composites Ag | Spritzgiessverfahren zur herstellung von bauteilen |
IT1395375B1 (it) * | 2009-09-04 | 2012-09-14 | Imast S C A R L | Laminati a base di compositi comprendenti materiale viscoelastico, metodo di preparazione degli stessi e loro impiego |
JP2013514439A (ja) * | 2009-12-15 | 2013-04-25 | スリーエム イノベイティブ プロパティズ カンパニー | エポキシ接着剤を有するフルオロポリマーフィルム |
GB2477091A (en) | 2010-01-20 | 2011-07-27 | Hexcel Composites Ltd | Structureal laminate comprising face sheets, core and open-structured sheet |
KR20130056210A (ko) * | 2010-03-04 | 2013-05-29 | 신슈 다이가쿠 | 탄소 섬유 강화 플라스틱 성형체 |
WO2011108676A1 (ja) * | 2010-03-04 | 2011-09-09 | Jx日鉱日石エネルギー株式会社 | ロボットハンド |
US9868265B2 (en) | 2010-05-27 | 2018-01-16 | Hexcel Composites, Limited | Structured thermoplastic in composite interleaves |
US8479880B2 (en) * | 2010-09-15 | 2013-07-09 | The Boeing Company | Multifunctional nano-skin articles and methods |
US20130312862A1 (en) * | 2010-12-14 | 2013-11-28 | Deepflex Inc. | Spoolable pipe with increased compressive strength and method of manufacture |
ES2386176B1 (es) * | 2010-12-27 | 2013-06-21 | Airbus Operations, S.L. | Material compuesto multifuncional con intercapa visco-elástica. |
US8796164B2 (en) | 2010-12-28 | 2014-08-05 | Cytec Technology Corp. | Multilayer and composition gradient structures with improved damping properties |
US20140134354A1 (en) * | 2011-06-08 | 2014-05-15 | Goodrich Corporation | Barrier layer for inflatable structures |
CN103906795B (zh) | 2011-06-13 | 2018-04-24 | 古德里奇公司 | 具有改进的振动阻尼的聚合物复合材料 |
US8808490B2 (en) | 2011-08-04 | 2014-08-19 | The Boeing Company | Methods for laminating composites |
US8937254B2 (en) * | 2012-05-29 | 2015-01-20 | Aurora Flight Sciences Corporation | Apparatus and method for an aircraft conductor sandwich assembly embedded to an aircraft structure |
US9833930B2 (en) * | 2012-10-23 | 2017-12-05 | Albany Engineered Composites, Inc. | Circumferential stiffeners for composite fancases |
US9067374B2 (en) | 2012-11-30 | 2015-06-30 | The Boeing Company | Method and apparatus for applying film material to elongate members |
US9676160B2 (en) | 2012-11-30 | 2017-06-13 | The Boeing Company | Holding system for elongate members |
EP2746149B1 (en) * | 2012-12-19 | 2019-06-19 | Airbus Operations GmbH | Method for the production of a connecting element, connecting element, and aircraft or spacecraft |
US20140186166A1 (en) * | 2012-12-27 | 2014-07-03 | General Electric Company | Hybrid Continuous Fiber Chopped Fiber Polymer Composite Structure |
US20140186600A1 (en) * | 2012-12-28 | 2014-07-03 | Thercom Holdings, Llc | Low pressure thermoplastic molding materials for fiber-reinforced composite structures |
GB201305325D0 (en) * | 2013-03-22 | 2013-05-08 | Hexcel Composites Ltd | Composite material |
GB201306481D0 (en) | 2013-04-10 | 2013-05-22 | Rolls Royce Plc | A method of manufacturing a composite material including a thermoplastic coated reinforcing element |
WO2015011549A1 (en) * | 2013-07-24 | 2015-01-29 | Toray Industries, Inc. | Fiber reinforced polymer composition with interlaminar hybridized tougheners |
AT515022B1 (de) * | 2013-10-28 | 2016-06-15 | Greiner Perfoam Gmbh | Kfz.-Innenverkleidungsteil |
DE102013114253A1 (de) * | 2013-12-17 | 2015-06-18 | Airbus Defence and Space GmbH | Akustik-Kabinenpaneel |
US9685710B1 (en) | 2014-01-22 | 2017-06-20 | Space Systems/Loral, Llc | Reflective and permeable metalized laminate |
DE102014004387A1 (de) * | 2014-03-26 | 2015-10-01 | GM Global Technology Operations, LLC (n.d. Ges. d. Staates Delaware) | Verbundbauteil und Verfahren zu dessen Herstellung |
US9725154B2 (en) * | 2014-05-13 | 2017-08-08 | The Boeing Company | Method and apparatus for reducing structural vibration and noise |
US10167550B2 (en) | 2014-06-03 | 2019-01-01 | Aurora Flight Sciences Corporation | Multi-functional composite structures |
US10368401B2 (en) | 2014-06-03 | 2019-07-30 | Aurora Flight Sciences Corporation | Multi-functional composite structures |
US10350863B2 (en) * | 2014-07-30 | 2019-07-16 | The Boeing Company | Methods and systems for damping a cabin air compressor inlet |
JP5944457B2 (ja) * | 2014-09-12 | 2016-07-05 | 本田技研工業株式会社 | 自動二輪車 |
US10285219B2 (en) | 2014-09-25 | 2019-05-07 | Aurora Flight Sciences Corporation | Electrical curing of composite structures |
CN105522788B (zh) * | 2014-11-24 | 2017-11-21 | 比亚迪股份有限公司 | 一种纤维金属层合板及其制备方法 |
EP3076245B1 (fr) * | 2015-04-02 | 2021-03-17 | CSEM Centre Suisse D'electronique Et De Microtechnique SA | Dispositif amortisseur notamment pour composant micromécanique horloger |
JP6516693B2 (ja) * | 2016-02-15 | 2019-05-22 | 三菱重工業株式会社 | 構造体の設計方法 |
DE112017002542T5 (de) * | 2016-05-19 | 2019-02-21 | Figaro Crowns Inc. | Glasfaser-Zahnkronen |
ES2822933T3 (es) * | 2016-11-04 | 2021-05-05 | Airbus Operations Sl | Estructura de panel para una aeronave y procedimiento de fabricación de la misma |
EP3619768A4 (en) * | 2017-05-03 | 2021-01-20 | NSL Comm Ltd | DEVICE AND METHOD FOR FOLDED DEPLOYABLE WAVEGUIDE |
US10843788B2 (en) * | 2017-06-29 | 2020-11-24 | Textron Innovations Inc. | Damping structures for tiltrotor aircraft wings |
DE102017009520A1 (de) * | 2017-10-11 | 2019-04-11 | Eissmann Cotesa Gmbh | Elastischer Verbundkörper und Verfahren zu dessen Herstellung |
DE202017107958U1 (de) * | 2017-12-29 | 2018-01-25 | Airbus Operations Gmbh | Faserverbundsandwichmaterial enthaltend Formgedächtnislegierungen |
JPWO2019208823A1 (ja) * | 2018-04-27 | 2021-04-30 | 株式会社ブリヂストン | 強化繊維複合樹脂、コンポジットプリプレグおよび積層体 |
CA3147472A1 (en) * | 2018-09-21 | 2020-03-21 | Bauer Hockey Ltd. | Hockey stick with nanofiber reinforcement |
US20200187670A1 (en) * | 2018-12-18 | 2020-06-18 | Dreamwell, Ltd. | Active comfort controlled bedding systems |
FR3090702B1 (fr) * | 2018-12-21 | 2022-06-24 | Safran | Texture fibreuse tissée |
US11459085B2 (en) * | 2019-04-30 | 2022-10-04 | Textron Innovations Inc. | Energy attenuation stabilizers and methods |
CN110406194A (zh) * | 2019-08-30 | 2019-11-05 | 南京思甲宁新材料科技有限公司 | 阻尼减震式增强型碳纤维复合材料及碳纤维螺旋桨叶 |
US11028732B2 (en) | 2019-09-05 | 2021-06-08 | Rolls-Royce North American Technologies Inc. | High temperature panel damper for sheet metal structures |
CN114957741B (zh) * | 2021-12-29 | 2024-01-02 | 江苏志纤复能科技有限公司 | 一种低温共固化高阻尼复合材料及其制备方法 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04125136A (ja) * | 1990-01-26 | 1992-04-24 | Nec Corp | 繊維強化複合材料 |
JPH04341837A (ja) * | 1991-05-17 | 1992-11-27 | Ishikawajima Harima Heavy Ind Co Ltd | Frp積層板 |
JP2002519607A (ja) * | 1998-07-01 | 2002-07-02 | スリーエム イノベイティブ プロパティズ カンパニー | スプリングバックを低減し、締結具力残率を改良した、スルーホールおよび/または縁部を溶着した減衰ラミネート、およびその製造方法 |
JP2004291408A (ja) * | 2003-03-27 | 2004-10-21 | Cci Corp | 制振性複合材料 |
JP2005035287A (ja) * | 2003-07-15 | 2005-02-10 | Boeing Co:The | 複合積層構造および積層構造を製造する方法 |
JP2005262613A (ja) * | 2004-03-18 | 2005-09-29 | Toray Ind Inc | Frp構造体用中間基材および該基材を用いたfrp構造体 |
JP2006192904A (ja) * | 2001-08-02 | 2006-07-27 | Ebert Composites Corp | Z軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法 |
Family Cites Families (129)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2819032A (en) | 1953-10-20 | 1958-01-07 | Douglas Aircraft Co Inc | Aircraft fuselage having panel damping material |
US3020986A (en) | 1958-08-18 | 1962-02-13 | Gen Dynamics Corp | Composite structural panel |
US3088561A (en) | 1958-11-06 | 1963-05-07 | Wright Barry Corp | Damped structures |
US3078969A (en) | 1959-06-15 | 1963-02-26 | Lord Mfg Co | Damped beam |
US3078971A (en) | 1960-01-11 | 1963-02-26 | Lord Mfg Co | Damped beam |
US3159249A (en) | 1960-01-27 | 1964-12-01 | Univ Minnesota | Damping means |
US3160549A (en) | 1960-12-29 | 1964-12-08 | Minnesota Mining & Mfg | Vibration damping structures |
US3193049A (en) | 1963-05-27 | 1965-07-06 | Daubert Chemical Co | Sound damping tape |
US3832955A (en) | 1972-09-01 | 1974-09-03 | Jered Prod Inc | Reinforced plastic panel |
SE420750B (sv) | 1978-11-17 | 1981-10-26 | Ingemanssons Ingenjorsbyra Ab | Ljudisolerande byggnadselement med stor styvhet |
US4182495A (en) | 1978-12-04 | 1980-01-08 | The United States Of America As Represented By The Secretary Of The Navy | Graphite or carbon fiber composite structure, low temperature cure |
FR2457981A1 (fr) | 1979-06-02 | 1980-12-26 | Nissan Motor | Couvercle reducteur de bruits pour moteur a combustion interne |
US4828202A (en) | 1979-09-27 | 1989-05-09 | The Boeing Company | Method and apparatus for wideband vibration damping of reinforced skin structures |
US4635882A (en) | 1980-11-14 | 1987-01-13 | The Boeing Company | Method and apparatus for reducing low to mid frequency interior noise |
US4591402A (en) | 1981-06-22 | 1986-05-27 | Ltv Aerospace And Defense Company | Apparatus and method for manufacturing composite structures |
US4428454A (en) | 1981-09-24 | 1984-01-31 | Capaul Raymond W | Acoustical panel construction |
US4556439A (en) | 1981-09-25 | 1985-12-03 | The Boeing Company | Method of sealing and bonding laminated epoxy plates |
US4463044A (en) | 1981-09-28 | 1984-07-31 | The Boeing Company | Composite panel of varied thickness |
US4401495A (en) | 1981-09-28 | 1983-08-30 | The Boeing Company | Method of winding composite panels |
US4416349A (en) | 1981-09-30 | 1983-11-22 | The Boeing Company | Viscoelastically damped reinforced skin structures |
US4425980A (en) | 1981-12-14 | 1984-01-17 | The Boeing Company | Beam dampers for damping the vibrations of the skin of reinforced structures |
US4553631A (en) | 1983-05-19 | 1985-11-19 | United Mcgill Corporation | Sound absorption method and apparatus |
US4851501A (en) | 1983-06-17 | 1989-07-25 | The Boeing Company | Polyethersulfone prepregs, composites, and blends |
US4477304A (en) | 1983-07-01 | 1984-10-16 | International Business Machines Corporation | Application tool |
WO1985003032A1 (en) | 1984-01-09 | 1985-07-18 | The Boeing Company | Composite material structure with integral fire protection |
JPS6112334A (ja) | 1984-06-29 | 1986-01-20 | 川崎製鉄株式会社 | 複合型制振積層体 |
US4877471A (en) | 1984-08-24 | 1989-10-31 | The Boeing Company | Method and apparatus for delivering a resin-impregnated, multifilament band |
US4608220A (en) | 1984-12-20 | 1986-08-26 | The Boeing Company | Method of forming composite material articles |
US4966802A (en) | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US4786343A (en) | 1985-05-10 | 1988-11-22 | The Boeing Company | Method of making delamination resistant composites |
US4611687A (en) | 1985-07-23 | 1986-09-16 | Nixon Michael T | Three-function acoustical panel |
JPS62111837U (ja) | 1985-12-28 | 1987-07-16 | ||
US4699683A (en) | 1986-02-07 | 1987-10-13 | The Boeing Company | Multiroving fiber laminator |
DE3614365A1 (de) | 1986-04-28 | 1987-10-29 | Messerschmitt Boelkow Blohm | Vorrichtung zum ablegen eines vorimpraegnierten faserbandes |
US4860851A (en) | 1987-01-27 | 1989-08-29 | Raychem Corporation | Dimensionally-recoverable damping article |
US5151311A (en) | 1987-11-02 | 1992-09-29 | Grumman Aerospace Corporation | Acoustic attenuating liner and method of making same |
JPH0673935B2 (ja) | 1988-04-01 | 1994-09-21 | ニチアス株式会社 | 制振材および制振材を用いた防音構造体 |
FR2632604B1 (fr) | 1988-06-08 | 1991-07-12 | Aerospatiale | Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication |
US5232073A (en) | 1988-12-09 | 1993-08-03 | Trw Inc. | Process for damping dynamic load |
US5106668A (en) | 1989-06-07 | 1992-04-21 | Hexcel Corporation | Multi-layer honeycomb structure |
JP2554063Y2 (ja) | 1989-10-17 | 1997-11-12 | 財団法人日本航空機開発協会 | 胴体壁内装板 |
US5277958A (en) | 1990-01-02 | 1994-01-11 | Tomkins Keith A | Multiple-layer structures and joining method for honeycomb, foam and lightweight materials |
DE4002087A1 (de) | 1990-01-25 | 1991-08-08 | Messerschmitt Boelkow Blohm | Ablegen von faserbaendern auf doppelt gekruemmten koerpern oder flaechen |
US5087491A (en) | 1990-02-09 | 1992-02-11 | The United States Of America As Represented By The Secretary Of The Navy | Vibration-damping structural member |
US5178717A (en) | 1991-03-06 | 1993-01-12 | Rodriguez Peter A | Adhesive applicator |
US5268055A (en) | 1991-10-31 | 1993-12-07 | Bales John L | Method for making perforated composite laminates |
US5256223A (en) | 1991-12-31 | 1993-10-26 | The Center For Innovative Technology | Fiber enhancement of viscoelastic damping polymers |
US5262232A (en) * | 1992-01-22 | 1993-11-16 | Minnesota Mining And Manufacturing Company | Vibration damping constructions using acrylate-containing damping materials |
US5445861A (en) | 1992-09-04 | 1995-08-29 | The Boeing Company | Lightweight honeycomb panel structure |
US5308675A (en) | 1992-09-15 | 1994-05-03 | The United States Of America As Represented By The Secretary Of The Navy | Flexible high damping structure |
US5744221A (en) | 1992-09-15 | 1998-04-28 | The United States Of America As Represented By The Secretary Of The Navy | Flexible high-damping composite structures and fabrication thereof |
US5337288A (en) * | 1992-09-30 | 1994-08-09 | The United States Of America As Represented By The Secretary Of The Navy | Acoustic and vibration attenuation composite material |
US5354195A (en) | 1992-12-23 | 1994-10-11 | United Technologies Corporation | Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores |
US5916954A (en) | 1993-01-27 | 1999-06-29 | Trw Inc. | Fiber reinforced viscoelastic material composites for passive damping |
US5368914A (en) | 1993-03-03 | 1994-11-29 | The United States Of America As Represented By The Secretary Of The Navy | Vibration-damping structural component |
US5902755A (en) | 1993-05-03 | 1999-05-11 | Tox-Wastech, Inc. | High Strength composite materials |
CA2162171A1 (en) | 1993-05-05 | 1994-11-10 | Frederick S. Campbell | Composite sandwich element |
US5507477A (en) | 1994-07-28 | 1996-04-16 | Trw Inc. | Composite damping structures and related method |
US5622733A (en) | 1994-10-04 | 1997-04-22 | Rockwell International Corporation | Tooling for the fabrication of composite hollow crown-stiffened skins and panels |
US5567499A (en) | 1995-01-03 | 1996-10-22 | The Boeing Company | Resin transfer molding in combination with honeycomb core |
US5667866A (en) | 1995-05-02 | 1997-09-16 | The Nordam Group, Inc. | Multi-layered, unbalanced sandwich panel |
US5710396A (en) | 1996-01-02 | 1998-01-20 | Rogers; Lynn C. | Energy-dissipating vibration damping structure |
US5866272A (en) | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US5700347A (en) | 1996-01-11 | 1997-12-23 | The Boeing Company | Thermoplastic multi-tape application head |
US5604010A (en) | 1996-01-11 | 1997-02-18 | Hartz; Dale E. | Composite honeycomb sandwich structure |
DE69610830T2 (de) | 1996-07-22 | 2001-05-17 | Hexcel Corp | Wabenförmige Kernmaterialien mit partikelförmiger Verstärkung |
US5895013A (en) | 1996-10-02 | 1999-04-20 | Mcdonnell Douglas Corp. | Low frequency noise suppression system |
US5904318A (en) | 1996-12-18 | 1999-05-18 | Towfiq; Foad | Passive reduction of aircraft fuselage noise |
US5958556A (en) | 1996-12-19 | 1999-09-28 | Minnesota Mining And Manufacturing Company | Vibration damped and stiffened circuit articles |
DE19653850C2 (de) | 1996-12-21 | 1999-01-28 | Daimler Benz Aerospace Airbus | Wandelement |
US6171705B1 (en) | 1997-02-10 | 2001-01-09 | Dofasco, Inc. | Structural panel and method of manufacture |
US5902535A (en) * | 1997-07-30 | 1999-05-11 | Mcdonnell Douglas Corporation | Resin film infusion mold tooling and molding method |
US7906191B2 (en) * | 1997-11-14 | 2011-03-15 | William F. Pratt | Wavy composite structures |
US6453962B1 (en) * | 1997-11-14 | 2002-09-24 | William F. Pratt | Dual-axis method and machine for producing pre-preg |
DE19804718C2 (de) | 1998-02-06 | 2001-09-13 | Eurocopter Deutschland | Schall absorbierende Sandwichwand |
US6458309B1 (en) | 1998-06-01 | 2002-10-01 | Rohr, Inc. | Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel |
US6110985A (en) | 1998-10-30 | 2000-08-29 | Soundwich, Inc. | Constrained layer damping compositions |
DE19901965A1 (de) * | 1999-01-19 | 2000-07-20 | Giesecke & Devrient Gmbh | Tragbarer Datenträger mit ausbrechbarer Minichipkarte |
GB9905145D0 (en) | 1999-03-06 | 1999-04-28 | Bolton Inst Higher Education | Auxetic materials |
US6510961B1 (en) | 1999-04-14 | 2003-01-28 | A&P Technology | Integrally-reinforced braided tubular structure and method of producing the same |
US6755998B1 (en) | 1999-10-26 | 2004-06-29 | Compsys, Inc. | Composite panel adapted for point compressive loads and method for making same |
BR9905840B1 (pt) * | 1999-12-14 | 2010-07-13 | sistema dispersor de carga de unidades de craqueamento catalìtico fluido. | |
US6399199B1 (en) | 1999-12-28 | 2002-06-04 | Toray Industries Inc. | Prepeg and carbon fiber reinforced composite materials |
US6655633B1 (en) | 2000-01-21 | 2003-12-02 | W. Cullen Chapman, Jr. | Tubular members integrated to form a structure |
JP4526698B2 (ja) | 2000-12-22 | 2010-08-18 | 富士重工業株式会社 | 複合材成形品及びその製造方法 |
US20050016671A1 (en) | 2001-03-05 | 2005-01-27 | Sharp Terrance M. | Robotic tape applicator and method |
US6497190B1 (en) | 2001-05-29 | 2002-12-24 | Compsys, Inc. | Conformable composite structural member and method therefor |
US6659223B2 (en) | 2001-10-05 | 2003-12-09 | Collins & Aikman Products Co. | Sound attenuating material for use within vehicles and methods of making same |
TW561102B (en) * | 2001-10-22 | 2003-11-11 | Hrl Lab Llc | Preparing composites by using resins |
EP1336469A1 (en) | 2002-02-19 | 2003-08-20 | Alenia Aeronautica S.P.A. | Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element |
GB2390999B (en) | 2002-07-19 | 2005-07-20 | Oxford Magnet Tech | Composite material for acoustic damping |
US7419627B2 (en) | 2002-09-13 | 2008-09-02 | Northrop Grumman Corporation | Co-cured vacuum-assisted resin transfer molding manufacturing method |
US7197852B2 (en) | 2002-09-20 | 2007-04-03 | The Boeing Company | Internally stiffened composite panels and methods for their manufacture |
GB2401346B (en) * | 2003-05-07 | 2005-04-13 | Oxford Magnet Tech | A structural composite material for acoustic damping |
US7213629B2 (en) | 2003-05-14 | 2007-05-08 | The Boeing Company | Vacuum assisted ply placement shoe and method |
US7282107B2 (en) | 2003-08-22 | 2007-10-16 | The Boeing Company | Multiple head automated composite laminating machine for the fabrication of large barrel section components |
US7181891B2 (en) | 2003-09-08 | 2007-02-27 | Quiet Solution, Inc. | Acoustical sound proofing material and methods for manufacturing same |
USD533950S1 (en) | 2004-02-26 | 2006-12-19 | Dan-Pal | Structural panel |
US20050194210A1 (en) | 2004-03-08 | 2005-09-08 | The Boeing Company | Apparatus and method for aircraft cabin noise attenuation via non-obstructive particle damping |
US7083147B2 (en) | 2004-03-11 | 2006-08-01 | The Boeing Company | Modularized insulation, systems, apparatus, and methods |
US7040575B2 (en) | 2004-03-29 | 2006-05-09 | The Boeing Company | Foam composite insulation for aircraft |
US7527222B2 (en) | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
US7134629B2 (en) | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US7160621B2 (en) | 2004-06-28 | 2007-01-09 | General Electric Company | Energy absorbing articles |
US20060040096A1 (en) * | 2004-08-19 | 2006-02-23 | Rajan Eadara | Constrained layer, composite, acoustic damping material |
US7325771B2 (en) | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
US7419031B2 (en) | 2005-11-04 | 2008-09-02 | The Boeing Company | Integrally damped composite aircraft floor panels |
US7503368B2 (en) | 2004-11-24 | 2009-03-17 | The Boeing Company | Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections |
US20060118244A1 (en) | 2004-12-02 | 2006-06-08 | The Boeing Company | Device for laying tape materials for aerospace applications |
US7578468B2 (en) | 2004-12-20 | 2009-08-25 | Sikorsky Aircraft Corporation | Acoustic absorption system for an aircraft airframe |
US7837147B2 (en) | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
US7766063B2 (en) | 2005-04-28 | 2010-08-03 | The Boeing Company | Machine assisted laminator and method |
US7291373B2 (en) | 2005-05-05 | 2007-11-06 | Northrop Grumman Corporation | Thermally insulated structure—full depth sandwich joint concept |
DE102005028765B4 (de) | 2005-06-22 | 2016-01-21 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Verstärkungsprofils |
US7681615B2 (en) | 2005-08-04 | 2010-03-23 | The Boeing Company | Tow width adaptable placement head device and method |
US20070069080A1 (en) | 2005-09-28 | 2007-03-29 | The Boeing Company | Laminated passenger window with a vacuum layer for reduced noise transmission |
ES2449515T3 (es) | 2005-10-06 | 2014-03-20 | Henkel Ag & Co. Kgaa | Reducción de la transferencia de vibraciones |
US9359061B2 (en) | 2005-10-31 | 2016-06-07 | The Boeing Company | Compliant stiffener for aircraft fuselage |
US10086921B2 (en) | 2005-10-31 | 2018-10-02 | The Boeing Company | Aircraft having a forward-facing section that deflects elastically under impact loads |
US20070125474A1 (en) | 2005-12-05 | 2007-06-07 | Huber Engineered Woods L.L.C. | Handheld tape applicator and components thereof, and their methods of use |
EP2006076B1 (en) | 2006-03-31 | 2015-11-18 | Airbus Operations S.L. | Method for producing composite-material structures with collapsible tooling |
CN101448700A (zh) | 2006-05-30 | 2009-06-03 | 空中客车德国有限公司 | 用于运输设施的吸声内覆层、特别是用于航空器机身单元的吸声内覆层的夹芯构件 |
US7931240B2 (en) | 2006-08-11 | 2011-04-26 | Techno-Sciences, Inc. | Cellular support structures used for controlled actuation of fluid contact surfaces |
NL2000232C2 (nl) | 2006-09-12 | 2008-03-13 | Gtm Consulting B V | Huidpaneel voor een vliegtuigromp. |
US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
US8327743B2 (en) | 2007-05-17 | 2012-12-11 | The Boeing Company | Mechanism and method for predetermined angular cutting of a plurality of ply strips |
US8951923B2 (en) | 2007-05-23 | 2015-02-10 | The Boeing Company | Hybrid composite structure having damped metallic fibers |
US7798285B2 (en) | 2008-11-14 | 2010-09-21 | Rohr, Inc. | Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers |
US8425710B2 (en) | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
-
2007
- 2007-01-23 US US11/656,626 patent/US9511571B2/en active Active
- 2007-12-12 JP JP2009547244A patent/JP5460333B2/ja active Active
- 2007-12-12 EP EP07874425.7A patent/EP2121300B1/en active Active
- 2007-12-12 WO PCT/US2007/087267 patent/WO2008115301A2/en active Application Filing
-
2016
- 2016-12-05 US US15/369,857 patent/US20170080681A1/en not_active Abandoned
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04125136A (ja) * | 1990-01-26 | 1992-04-24 | Nec Corp | 繊維強化複合材料 |
JPH04341837A (ja) * | 1991-05-17 | 1992-11-27 | Ishikawajima Harima Heavy Ind Co Ltd | Frp積層板 |
JP2002519607A (ja) * | 1998-07-01 | 2002-07-02 | スリーエム イノベイティブ プロパティズ カンパニー | スプリングバックを低減し、締結具力残率を改良した、スルーホールおよび/または縁部を溶着した減衰ラミネート、およびその製造方法 |
JP2006192904A (ja) * | 2001-08-02 | 2006-07-27 | Ebert Composites Corp | Z軸繊維の頂部端部および底部端部を、複合積層体の頂部表面および底部表面それぞれに締め付ける方法 |
JP2004291408A (ja) * | 2003-03-27 | 2004-10-21 | Cci Corp | 制振性複合材料 |
JP2005035287A (ja) * | 2003-07-15 | 2005-02-10 | Boeing Co:The | 複合積層構造および積層構造を製造する方法 |
JP2005262613A (ja) * | 2004-03-18 | 2005-09-29 | Toray Ind Inc | Frp構造体用中間基材および該基材を用いたfrp構造体 |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012514545A (ja) * | 2009-01-07 | 2012-06-28 | ヘクセル コンポジット、リミテッド | 改善された複合材料 |
JP2014208457A (ja) * | 2013-03-28 | 2014-11-06 | 福井県 | 積層成形体 |
JP2018138379A (ja) * | 2017-02-24 | 2018-09-06 | 三菱ケミカル株式会社 | 成形品およびその製造方法 |
JP2018206090A (ja) * | 2017-06-05 | 2018-12-27 | 株式会社岩間工業所 | 複合構造体の設計方法及び複合構造体 |
JP6989889B2 (ja) | 2017-06-05 | 2022-02-03 | 株式会社岩間工業所 | 複合構造体の設計方法及び複合構造体 |
JP2019112053A (ja) * | 2017-12-21 | 2019-07-11 | エアバス オペレーションズ リミテッドAirbus Operations Limited | 空気力学的表面用シールプレート |
JP7191673B2 (ja) | 2017-12-21 | 2022-12-19 | エアバス オペレーションズ リミテッド | 空気力学的表面用シールプレート |
WO2019159443A1 (ja) * | 2018-02-13 | 2019-08-22 | 三菱重工業株式会社 | 複合材料の製造方法及び複合材料 |
JP2019136970A (ja) * | 2018-02-13 | 2019-08-22 | 三菱重工業株式会社 | 複合材料の製造方法及び複合材料 |
US11383460B2 (en) | 2018-02-13 | 2022-07-12 | Mitsubishi Heavy Industries, Ltd. | Method for producing composite material |
Also Published As
Publication number | Publication date |
---|---|
US9511571B2 (en) | 2016-12-06 |
WO2008115301A2 (en) | 2008-09-25 |
EP2121300B1 (en) | 2016-05-04 |
WO2008115301A3 (en) | 2008-12-31 |
US20170080681A1 (en) | 2017-03-23 |
US20080277057A1 (en) | 2008-11-13 |
EP2121300A2 (en) | 2009-11-25 |
JP5460333B2 (ja) | 2014-04-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5460333B2 (ja) | 減衰中間層を有する複合積層板及びその作製方法 | |
US7419031B2 (en) | Integrally damped composite aircraft floor panels | |
US10343372B2 (en) | Composite article having multifunctional properties and method for its manufacture | |
JP5320742B2 (ja) | 複合プリプレグ基材の製造方法、積層基材および繊維強化プラスチック | |
CA2748926C (en) | Structural composite material with improved acoustic and vibrational damping properties | |
JP2020056148A (ja) | 複合構造体のためのフィラメントネットワーク | |
JP5117779B2 (ja) | 複合材料 | |
EP2006464B1 (en) | Sandwich panel | |
RU2531196C2 (ru) | Усовершенствованные композитные материалы | |
JP2006051813A5 (ja) | ||
JP2023515418A (ja) | 耐衝撃性構造物 | |
KR960000558B1 (ko) | 일방향 프리프렉 및 탄소섬유 강화 복합재료 | |
US20160009051A1 (en) | Veil-stabilized Composite with Improved Tensile Strength | |
KR101659591B1 (ko) | 하이브리드 세라믹 섬유강화 복합재료 제조방법 및 이에 의해 제조된 하이브리드 세라믹 섬유강화 복합재료 | |
JP2008132650A (ja) | 強化繊維積層体およびその製造方法 | |
JP2015502465A (ja) | 構造コア | |
JP6468761B2 (ja) | 開繊されたフィラメントを含む複合材テキスタイル | |
US20160265157A1 (en) | Structured flock fiber reinforced layer | |
JPH0575575B2 (ja) | ||
KR20230131473A (ko) | 복합 재료 및 구조 | |
JP2005262818A (ja) | 強化繊維基材、プリフォームおよび強化繊維基材の製造方法 | |
JP2007090811A (ja) | 繊維強化プラスチック部材および繊維強化プラスチック部材の製造方法 | |
JP6196658B2 (ja) | サンドイッチパネル,一方向プリプレグの製造方法及びサンドイッチパネルの製造方法 | |
JP2006138031A (ja) | 強化繊維基材、プリフォームおよびそれらの製造方法 | |
US9834649B1 (en) | Shaped fiber composites |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20101206 |
|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20101206 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20120509 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20120529 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20120829 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20120905 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20120928 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20130416 |
|
A524 | Written submission of copy of amendment under article 19 pct |
Free format text: JAPANESE INTERMEDIATE CODE: A524 Effective date: 20130716 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20131224 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20140114 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5460333 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |