JP2016514632A - 複合材料 - Google Patents
複合材料 Download PDFInfo
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- JP2016514632A JP2016514632A JP2016503679A JP2016503679A JP2016514632A JP 2016514632 A JP2016514632 A JP 2016514632A JP 2016503679 A JP2016503679 A JP 2016503679A JP 2016503679 A JP2016503679 A JP 2016503679A JP 2016514632 A JP2016514632 A JP 2016514632A
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- composite material
- damping
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- resin
- damped composite
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/04—Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B25/08—Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material of 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
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/10—Layered products comprising a layer of natural or synthetic rubber 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/02—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by a sequence of laminating steps, e.g. by adding new layers at consecutive laminating stations
-
- 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
-
- 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
- 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
- B32B37/26—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 which influences the bonding during the lamination process, e.g. release layers or pressure equalising layers
- B32B2037/268—Release layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more layers
-
- 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
- B32B2262/101—Glass 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
- 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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/07—Parts immersed or impregnated in a matrix
- B32B2305/076—Prepregs
-
- 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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/72—Cured, e.g. vulcanised, cross-linked
-
- 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
- B32B2307/56—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
- B32B2363/00—Epoxy resins
-
- 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
-
- 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
- B32B37/16—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
- B32B37/20—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of continuous webs only
- B32B37/203—One or more of the layers being plastic
Landscapes
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
繊維及び構造用樹脂材料を含む構造層、
ダンピング材料、
接合材料、
並びに表面層
を備える、ダンピング化済み(damped)複合材料を製造するための方法であって、
a) 接合材料をダンピング材料の第1の面と組み合わせるステップ、
b) 接合材料及びダンピング材料の第1の面を構造層と組み合わせるステップ、
c) 表面層をダンピング材料の第2の面と組み合わせるステップ
を含む、上記方法が提供される。
10g/m2が裏当てされている2枚の樹脂フィルム(M21EV、Hexcel Composites、France)を、ロール状の0.1mm型Smacwrap ST(SMAC、France)の両面に施用した。これらのフィルムについては、連接した二組の30cm(12インチ)固結ローラーを用いて、各フィルムを順次施用した。次いで、ロールを、ATL用に適合した幅に切断して、幅3.2mmのテープを形成した。
一組の12インチ型固結ローラーを用いて、厚さ0.1mmのSmacwrap(いずれかの国における登録商標)ST(SMAC SA、Franceから調達)を、M21EV/34%/194/IMAプリプレグ(Hexcel Composites SA、France)に積層した。プリプレグは、Smacwrap(いずれかの国における登録商標)をプリプレグ上に粘着させるのに十分な表面樹脂を有していた。10g/m2が裏当てされているフィルム樹脂(M21EV、Hexcel Composites、France)の粘着性付与フィルムを、さらなる一組の30cm(12インチ)固結ローラーを用いて、Smacwrap層において晒されている表面上に積層した。次いで、複合材料を、ATL用に適合した幅3.2mmのテープ幅に切断した。
Claims (27)
- ダンピング材料、接合材料、並びに、繊維及び構造用樹脂材料を含む構造層を含む、ダンピング化済み複合材料。
- 前記ダンピング材料の第1の面上の前記接合材料が、前記ダンピング材料とプリプレグとの接着を増大させる、請求項1に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、加硫ゴムを含む、請求項1又は2に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、ASTM D1456−86(2010)標準試験法に従って測定したときに300%から800%の間の最大伸びを有する、請求項1から3までのいずれか一項に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、連続シートである、請求項1から4までのいずれか一項に記載のダンピング化済み複合材料。
- 前記接合材料が、熱硬化性樹脂、好ましくはエポキシ樹脂を含む、請求項1から5までのいずれか一項に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、無変形状態において不透過性及び/又は連続的である、請求項1から6までのいずれか一項に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、0.1〜0.2mmの厚さを有する、請求項1から7までのいずれか一項に記載のダンピング化済み複合材料。
- 前記繊維が、ガラス繊維又は炭素繊維を含み、好ましくは一方向への整列を有する、請求項1から8までのいずれか一項に記載のダンピング化済み複合材料。
- 前記構造用樹脂が、熱硬化性樹脂、好ましくはエポキシ樹脂を含む、請求項1から9までのいずれか一項に記載のダンピング化済み複合材料。
- 前記構造用樹脂及び繊維が、プリプレグ又はセミプレグを含む、請求項1から10までのいずれか一項に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、表面紛体又は裏当て層を備える、請求項1から11までのいずれか一項に記載のダンピング化済み複合材料
- 前記ダンピング材料が、樹脂又は硬化剤の表面紛体を含む、請求項12に記載のダンピング化済み複合材料。
- 前記接合材料が、1g/m2から50g/m2までの面積重量を有する熱硬化性樹脂フィルムである、請求項1から13までのいずれか一項に記載のダンピング化済み複合材料。
- ダンピング層が、表面粘着性を増大させるための表面層をさらに含む、請求項1から14までのいずれか一項に記載のダンピング化済み複合材料であって、該表面層が、6g/m2から10g/m2までの面積重量の熱硬化性樹脂フィルムである、上記ダンピング化済み複合材料。
- 前記接合材料が、熱可塑性ベールを含む、請求項1から15までのいずれか一項に記載のダンピング化済み複合材料。
- 表面材料が、熱可塑性ベールを含む、請求項1から16までのいずれか一項に記載のダンピング化済み複合材料。
- 前記ダンピング材料が、テクスチャーアナライザーによって測定したときに2Nから25Nまでのピーク力、好ましくは4Nから10Nまでのピーク力、及び/又はこれらの組合せのピーク力を有する表面粘着性を示す、請求項1から17までのいずれか一項に記載のダンピング化済み複合材料。
- 片面又は両面上にポリマー裏当てを備え、又は、ポリマー裏当てによって紙裏当てを置きかえた後、スリット加工を行う、請求項1から18までのいずれか一項に記載のダンピング化済み複合材料。
- 前記接合材料が、前記構造層の樹脂を含む、請求項1から19までのいずれか一項に記載のダンピング化済み複合材料。
- 繊維及び構造用樹脂材料を含む構造層、
ダンピング材料、
接合材料、
並びに表面層
を備える、(請求項1から20?までのいずれか一項に記載の)ダンピング化済み複合材料を製造するための方法であって、
a) 接合材料を該ダンピング材料の第1の面と組み合わせるステップ;
b)該 接合材料及び該ダンピング材料の第1の面を該構造層と組み合わせるステップ;
c) 表面層を該ダンピング材料の第2の面と組み合わせるステップ
を含む、上記方法。 - 前記ダンピング材料が、紛体塗膜を備え付けられており、前記接合材料及び/又は表面層が、該紛体を取り除くことなく施用される、請求項21に記載のダンピング化済み複合材料を製造するための方法。
- 前記ダンピング材料が、裏当て層を有しており、該ダンピング材料が前記接合材料又は表面層に施用された後に取り除かれる、請求項21に記載のダンピング化済み複合材料を製造するための方法。
- 前記接合材料が、ダンピング材料に施用された後、構造層と組み合わせられる、請求項21に記載のダンピング化済み複合材料を製造するための方法。
- 前記接合材料が、前記構造層に施用された後、前記ダンピング材料と組み合わせられる、請求項21に記載のダンピング化済み複合材料を製造するための方法。
- 前記接合材料の厚さが、前記構造層への施用時における前記ダンピング材料のひずみを予防するように選択される、請求項21に記載のダンピング化済み複合材料を製造するための方法。
- 前記材料が、AFP型又はATL型機械装置における使用のための幅に切断される、請求項21に記載のダンピング化済み複合材料を製造するための方法。
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Application Number | Priority Date | Filing Date | Title |
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GB1305325.1 | 2013-03-22 | ||
GBGB1305325.1A GB201305325D0 (en) | 2013-03-22 | 2013-03-22 | Composite material |
PCT/EP2014/055749 WO2014147243A1 (en) | 2013-03-22 | 2014-03-21 | Composite material |
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JP2016514632A true JP2016514632A (ja) | 2016-05-23 |
JP2016514632A5 JP2016514632A5 (ja) | 2018-04-26 |
JP6535655B2 JP6535655B2 (ja) | 2019-06-26 |
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US (1) | US20160288457A1 (ja) |
EP (1) | EP2976217B1 (ja) |
JP (1) | JP6535655B2 (ja) |
CN (1) | CN105073402B (ja) |
ES (1) | ES2902844T3 (ja) |
GB (2) | GB201305325D0 (ja) |
WO (1) | WO2014147243A1 (ja) |
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JP2019015013A (ja) * | 2017-06-05 | 2019-01-31 | ザ・ボーイング・カンパニーThe Boeing Company | 炭素繊維を製造するための方法及び装置 |
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US10399276B2 (en) | 2015-08-12 | 2019-09-03 | General Electric Company | System and method for controlling at least one variable during layup of a composite part using automated fiber placement |
BR112018007902B1 (pt) * | 2015-10-22 | 2022-10-04 | Wobben Properties Gmbh | Componente compósito em três camadas de hélice de turbina eólica |
US10919233B2 (en) | 2016-01-08 | 2021-02-16 | Sikorsky Aircraft Corporation | Self-clamping self-curing bond method |
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- 2014-03-21 WO PCT/EP2014/055749 patent/WO2014147243A1/en active Application Filing
- 2014-03-21 ES ES14712649T patent/ES2902844T3/es active Active
- 2014-03-21 EP EP14712649.4A patent/EP2976217B1/en active Active
- 2014-03-21 GB GB1405122.1A patent/GB2513479B/en active Active
- 2014-03-21 CN CN201480016784.5A patent/CN105073402B/zh active Active
- 2014-03-21 JP JP2016503679A patent/JP6535655B2/ja active Active
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Publication number | Priority date | Publication date | Assignee | Title |
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JP2019015013A (ja) * | 2017-06-05 | 2019-01-31 | ザ・ボーイング・カンパニーThe Boeing Company | 炭素繊維を製造するための方法及び装置 |
JP7169774B2 (ja) | 2017-06-05 | 2022-11-11 | ザ・ボーイング・カンパニー | 炭素繊維を製造するための方法及び装置 |
US11525193B2 (en) | 2017-06-05 | 2022-12-13 | The Boeing Company | Method and apparatus for manufacturing carbon fibers |
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GB2513479A (en) | 2014-10-29 |
US20160288457A1 (en) | 2016-10-06 |
EP2976217B1 (en) | 2021-12-15 |
CN105073402A (zh) | 2015-11-18 |
GB201305325D0 (en) | 2013-05-08 |
GB201405122D0 (en) | 2014-05-07 |
EP2976217A1 (en) | 2016-01-27 |
CN105073402B (zh) | 2018-03-23 |
GB2513479B (en) | 2016-07-20 |
JP6535655B2 (ja) | 2019-06-26 |
WO2014147243A1 (en) | 2014-09-25 |
ES2902844T3 (es) | 2022-03-30 |
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