JP2011515531A - プリプレグにおける改良 - Google Patents
プリプレグにおける改良 Download PDFInfo
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- JP2011515531A JP2011515531A JP2011500296A JP2011500296A JP2011515531A JP 2011515531 A JP2011515531 A JP 2011515531A JP 2011500296 A JP2011500296 A JP 2011500296A JP 2011500296 A JP2011500296 A JP 2011500296A JP 2011515531 A JP2011515531 A JP 2011515531A
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- Prior art keywords
- prepreg
- laminate
- raised
- matrix
- 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.)
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Classifications
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- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
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- 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
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
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- 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
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/28—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
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
- C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
- C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/74—Moulding material on a relatively small portion of the preformed part, e.g. outsert moulding
- B29C70/747—Applying material, e.g. foam, only in a limited number of places or in a pattern, e.g. to create a decorative effect
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- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
-
- 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.]
- Y10T428/24132—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in different layers or components parallel
-
- 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.]
- Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Medicinal Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Health & Medical Sciences (AREA)
- Inorganic Chemistry (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
面積重量134gm−2の一方向炭素繊維8552プリプレグを0度と90度の方向に交互の層(200mm×200mm)で積層した。この積層で用いたプライの数は、12枚であった。次いで、この集合体を真空下、室温で15分間圧密化した。このプリプレグを真空テーブル上に置き、以下の条件下で硬化させた:傾斜速度1℃/分で110℃に加温し、1時間保持し、次いで、傾斜速度1℃/分で180℃に加温し、2時間保持した。この集合体を室温に冷却させ、真空テーブルから取り出した。
8552プリプレグを寸法(300mm×300mm)に切断し、個々のプライをXenjet4000のOmnidot760GS8プリントヘッド下に置いた。適用したインクは、多官能アクリレート、独自仕様の光開始剤ブレンド及びマゼンダ染料(Xennia製Magenta Vivide X8022 Ink)の混合物から構成された。UVランプ(fusion H bulb)を用いて、159mJ/cm2の最小線量でインクを硬化させた。次いで、必要なパターンを100m/分の速度でプリプレグにプリントした。異なる線高さは、同じプリプレグ上に2回以上プリントすることによって得た。次いで、このプリントプリプレグを0度と90度の方向の交互の層(200mm×200mm)で積層した。この積層に用いたプライの数は、12枚であった。次いで、この集合体を真空下、室温で15分間圧密化した。
M56プリプレグを寸法(300mm×300mm)に切断し、個々のプライを、Xenjet4000のOmnidot760GS8プリントヘッド下に置いた。このインク及びプリント条件は、前の例に記載したとおりであった。この積層に用いたプライの数は10枚であった。次いで、この集合体を真空下、室温で15分間圧密化した。次いで、このプリプレグを前の例におけるとおりに硬化させた。積層体の気孔率は、例1及び例2に記載したとおりに測定した。平均値は、同じ積層体由来の3つの試料の気孔率の測定値に基づいた。
M72プリプレグを、前の例におけるとおりに切断し、プリントした。この積層に用いたプライの数は10枚であった。圧密化及び硬化は、前に記載したとおりであった。積層体の気孔率は、例1及び例2で記載したとおりに測定した。平均値は、3つの試料の気孔率の測定値に基づいた。
Claims (12)
- マトリックス及び繊維を含むプリプレグであって、該マトリックスの表面に対して少なくとも5マイクロメートル隆起させた複数の領域をその上に堆積させた上記プリプレグ。
- マトリックス及び繊維を含むプリプレグを処理する方法であって、該マトリックスの表面に対して少なくとも5マイクロメートル隆起させた複数の領域を堆積させることを含む上記方法。
- 前記隆起領域がプリンティングによって堆積される、請求項1又は2に記載のプリプレグ又は方法。
- 前記プリンティング方法がインクジェットプリンティングである、請求項3に記載のプリプレグ又は方法。
- 前記隆起領域が、熱以外の方法で硬化可能な材料の堆積によって形成される、請求項1から4までのいずれか一項に記載のプリプレグ又は方法。
- 前記材料が紫外線又は可視光線に曝すことによって硬化可能である、請求項5に記載のプリプレグ又は方法。
- 前記隆起領域が直線である、請求項1から6までのいずれか一項に記載のプリプレグ又は方法。
- 前記プリプレグ中の前記繊維が一方向であり、前記隆起領域の線が前記繊維に平行に続いている、請求項7に記載のプリプレグ又は方法。
- 前記領域が、前記マトリックスの表面から5から200マイクロメートル隆起している、請求項1から8までのいずれか一項に記載のプリプレグ又は方法。
- 前記隆起領域が非導電性である、請求項1から9までのいずれか一項に記載のプリプレグ又は方法。
- 請求項1から10までのいずれか一項に記載の複数のプリプレグの積層体を硬化させる方法であって、前記積層体を高温に曝し、硬化複合積層体を形成することを含む上記方法。
- 請求項11に記載の方法によって得られる、複数のプリプレグの硬化積層体。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0805203A GB2460214A (en) | 2008-03-20 | 2008-03-20 | Prepregs for use in making laminates of reduced porosity |
GB0805203.7 | 2008-03-20 | ||
PCT/GB2009/050230 WO2009115832A1 (en) | 2008-03-20 | 2009-03-09 | Improvements in prepregs |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2011515531A true JP2011515531A (ja) | 2011-05-19 |
JP5395889B2 JP5395889B2 (ja) | 2014-01-22 |
Family
ID=39386528
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011500296A Expired - Fee Related JP5395889B2 (ja) | 2008-03-20 | 2009-03-09 | プリプレグにおける改良 |
Country Status (9)
Country | Link |
---|---|
US (1) | US9174394B2 (ja) |
EP (1) | EP2254936B1 (ja) |
JP (1) | JP5395889B2 (ja) |
CN (1) | CN102027051B (ja) |
AU (1) | AU2009227749B2 (ja) |
ES (1) | ES2605431T3 (ja) |
GB (1) | GB2460214A (ja) |
RU (1) | RU2491167C2 (ja) |
WO (1) | WO2009115832A1 (ja) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014038633A1 (ja) | 2012-09-06 | 2014-03-13 | 三菱レイヨン株式会社 | プリプレグ及びその製造方法 |
JP2014051093A (ja) * | 2012-08-31 | 2014-03-20 | Boeing Co | 複合構造体の空隙率を低減するための方法およびシステム |
JP2016074204A (ja) * | 2014-09-23 | 2016-05-12 | ザ・ボーイング・カンパニーThe Boeing Company | 複合ラミネート上へのパターンのプリント |
US9481789B2 (en) | 2011-03-03 | 2016-11-01 | Mitsubishi Rayon Co., Ltd. | Matrix resin composition, prepreg and method for producing the same, and fiber-reinforced composite material |
KR20180025179A (ko) * | 2016-08-29 | 2018-03-08 | 더 보잉 컴파니 | 드라이 프리폼의 수지 침투성에 국부적으로 영향을 주는 방법 |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105581999A (zh) | 2007-02-06 | 2016-05-18 | 安元有限公司 | 用于抑制神经传导的包括萜烯化合物的组合物以及方法 |
FI3164265T3 (fi) * | 2014-07-01 | 2023-12-21 | Isola Usa Corp | Menetelmä laminaattilevyn valmistamiseksi ja tästä seuraavia tuotteita |
US9764532B2 (en) * | 2014-07-01 | 2017-09-19 | Isola Usa Corp. | Prepregs including UV curable resins useful for manufacturing semi-flexible PCBs |
US10661530B2 (en) | 2016-05-12 | 2020-05-26 | The Boeing Company | Methods and apparatus to couple a decorative layer to a panel via a high-bond adhesive layer |
US10173394B2 (en) * | 2016-05-12 | 2019-01-08 | The Boeing Company | Methods and apparatus to vent gas and vapor from a panel via venting channels for a decorative layer |
US11130318B2 (en) | 2016-05-12 | 2021-09-28 | The Boeing Company | Panels having barrier layers and related methods |
US10751982B2 (en) | 2016-05-12 | 2020-08-25 | The Boeing Company | Methods and apparatus to remove gas and vapor from a panel for a decorative layer |
US10647099B2 (en) | 2016-05-12 | 2020-05-12 | The Boeing Company | Methods and apparatus to form venting channels on a panel for a decorative layer |
US10525685B2 (en) | 2016-05-12 | 2020-01-07 | The Boeing Company | Methods and apparatus to couple a decorative composite having a reinforcing layer to a panel |
CN107417944A (zh) * | 2016-05-23 | 2017-12-01 | 广东亚太新材料科技有限公司 | 粗糙毛面纤维毡预浸料、复合材料及复合材料的制备方法 |
CN108749038B (zh) * | 2018-05-02 | 2020-03-24 | 江苏恒神股份有限公司 | 一种真空袋固化碳纤维预浸料的图案化制造技术 |
DE102019000053A1 (de) * | 2019-01-08 | 2020-07-23 | Senvion Gmbh | Pultrudate mit Erhebungen und Rillen |
Citations (8)
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JPH02227212A (ja) * | 1989-02-28 | 1990-09-10 | Mitsubishi Rayon Co Ltd | プリプレグ及びその製造法 |
JPH036093A (ja) * | 1989-06-02 | 1991-01-11 | Hitachi Chem Co Ltd | 多層プリント配線板用プリプレグシート |
JPH04320826A (ja) * | 1991-04-22 | 1992-11-11 | Fuji Heavy Ind Ltd | 複合材料の一体成形方法 |
JPH0581246U (ja) * | 1992-04-06 | 1993-11-05 | 東レ株式会社 | プリプレグ |
JPH09220768A (ja) * | 1996-02-16 | 1997-08-26 | Nissan Motor Co Ltd | Frp製構造体の製造方法 |
JPH11163499A (ja) * | 1997-11-28 | 1999-06-18 | Nitto Boseki Co Ltd | プリント配線板の製造方法及びこの製造方法によるプリント配線板 |
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JP2005238520A (ja) * | 2004-02-24 | 2005-09-08 | Matsushita Electric Works Ltd | プリプレグ及び多層プリント配線板 |
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GB0203823D0 (en) * | 2002-02-19 | 2002-04-03 | Hexcel Composites Ltd | Moulding materials |
US6964723B2 (en) * | 2002-10-04 | 2005-11-15 | The Boeing Company | Method for applying pressure to composite laminate areas masked by secondary features |
GB2433466A (en) * | 2005-12-21 | 2007-06-27 | Advanced Composites Group Ltd | Moulding materials |
RU2307032C1 (ru) * | 2005-12-27 | 2007-09-27 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Способ изготовления рельефного заполнителя |
-
2008
- 2008-03-20 GB GB0805203A patent/GB2460214A/en not_active Withdrawn
-
2009
- 2009-03-09 JP JP2011500296A patent/JP5395889B2/ja not_active Expired - Fee Related
- 2009-03-09 CN CN200980117774XA patent/CN102027051B/zh active Active
- 2009-03-09 US US12/922,884 patent/US9174394B2/en not_active Expired - Fee Related
- 2009-03-09 AU AU2009227749A patent/AU2009227749B2/en not_active Ceased
- 2009-03-09 WO PCT/GB2009/050230 patent/WO2009115832A1/en active Application Filing
- 2009-03-09 ES ES09721734.3T patent/ES2605431T3/es active Active
- 2009-03-09 EP EP09721734.3A patent/EP2254936B1/en active Active
- 2009-03-09 RU RU2010142926/05A patent/RU2491167C2/ru active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02227212A (ja) * | 1989-02-28 | 1990-09-10 | Mitsubishi Rayon Co Ltd | プリプレグ及びその製造法 |
JPH036093A (ja) * | 1989-06-02 | 1991-01-11 | Hitachi Chem Co Ltd | 多層プリント配線板用プリプレグシート |
JPH04320826A (ja) * | 1991-04-22 | 1992-11-11 | Fuji Heavy Ind Ltd | 複合材料の一体成形方法 |
JPH0581246U (ja) * | 1992-04-06 | 1993-11-05 | 東レ株式会社 | プリプレグ |
JPH09220768A (ja) * | 1996-02-16 | 1997-08-26 | Nissan Motor Co Ltd | Frp製構造体の製造方法 |
JPH11163499A (ja) * | 1997-11-28 | 1999-06-18 | Nitto Boseki Co Ltd | プリント配線板の製造方法及びこの製造方法によるプリント配線板 |
JP2004532144A (ja) * | 2001-04-18 | 2004-10-21 | スリーエム イノベイティブ プロパティズ カンパニー | 放射線硬化させたインクジェット印刷画像を含むプライマー処理した基材 |
JP2005238520A (ja) * | 2004-02-24 | 2005-09-08 | Matsushita Electric Works Ltd | プリプレグ及び多層プリント配線板 |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9481789B2 (en) | 2011-03-03 | 2016-11-01 | Mitsubishi Rayon Co., Ltd. | Matrix resin composition, prepreg and method for producing the same, and fiber-reinforced composite material |
JP2014051093A (ja) * | 2012-08-31 | 2014-03-20 | Boeing Co | 複合構造体の空隙率を低減するための方法およびシステム |
WO2014038633A1 (ja) | 2012-09-06 | 2014-03-13 | 三菱レイヨン株式会社 | プリプレグ及びその製造方法 |
EP3121219A1 (en) | 2012-09-06 | 2017-01-25 | Mitsubishi Rayon Co. Ltd. | Prepreg roll |
KR20170012576A (ko) | 2012-09-06 | 2017-02-02 | 미쯔비시 레이온 가부시끼가이샤 | 프리프레그 및 그의 제조 방법 |
US10647828B2 (en) | 2012-09-06 | 2020-05-12 | Mitsubishi Chemical Corporation | Prepreg and method for producing same |
JP2016074204A (ja) * | 2014-09-23 | 2016-05-12 | ザ・ボーイング・カンパニーThe Boeing Company | 複合ラミネート上へのパターンのプリント |
KR20180025179A (ko) * | 2016-08-29 | 2018-03-08 | 더 보잉 컴파니 | 드라이 프리폼의 수지 침투성에 국부적으로 영향을 주는 방법 |
KR102336177B1 (ko) * | 2016-08-29 | 2021-12-08 | 더 보잉 컴파니 | 드라이 프리폼의 수지 침투성에 국부적으로 영향을 주는 방법 |
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Publication number | Publication date |
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CN102027051B (zh) | 2013-07-10 |
CN102027051A (zh) | 2011-04-20 |
EP2254936A1 (en) | 2010-12-01 |
EP2254936B1 (en) | 2016-09-07 |
US9174394B2 (en) | 2015-11-03 |
AU2009227749A1 (en) | 2009-09-24 |
GB0805203D0 (en) | 2008-04-30 |
ES2605431T3 (es) | 2017-03-14 |
RU2491167C2 (ru) | 2013-08-27 |
US20110014419A1 (en) | 2011-01-20 |
RU2010142926A (ru) | 2012-04-27 |
AU2009227749B2 (en) | 2013-07-25 |
JP5395889B2 (ja) | 2014-01-22 |
GB2460214A (en) | 2009-11-25 |
WO2009115832A1 (en) | 2009-09-24 |
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