CN105431286A - 具有通过受控纤维铺放生产的孔图案的复合材料层压板 - Google Patents

具有通过受控纤维铺放生产的孔图案的复合材料层压板 Download PDF

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Publication number
CN105431286A
CN105431286A CN201480042807.XA CN201480042807A CN105431286A CN 105431286 A CN105431286 A CN 105431286A CN 201480042807 A CN201480042807 A CN 201480042807A CN 105431286 A CN105431286 A CN 105431286A
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CN
China
Prior art keywords
plies
tows
fiber
laminate
composite laminate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201480042807.XA
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English (en)
Chinese (zh)
Inventor
G·A·巴特勒
B·A·约翰逊
J·R·休斯
J·H·兰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of CN105431286A publication Critical patent/CN105431286A/zh
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • 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
    • B29C70/22—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 two directions forming a two dimensional structure
    • B29C70/224—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 two directions forming a two dimensional structure the structure being a net
    • 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
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
    • 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
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/022—Non-woven fabric
    • 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
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • 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
    • 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
    • B32B2262/106—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
    • B32B2305/02—Cellular or porous
    • B32B2305/024—Honeycomb
    • 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
    • B32B2605/00—Vehicles
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
CN201480042807.XA 2013-07-29 2014-06-16 具有通过受控纤维铺放生产的孔图案的复合材料层压板 Pending CN105431286A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/953,392 US20150030803A1 (en) 2013-07-29 2013-07-29 Composite Laminates Having Hole Patterns Produced by Controlled Fiber Placement
US13/953,392 2013-07-29
PCT/US2014/042522 WO2015017033A1 (en) 2013-07-29 2014-06-16 Composite laminates having hole patterns produced by controlled fiber placement

Publications (1)

Publication Number Publication Date
CN105431286A true CN105431286A (zh) 2016-03-23

Family

ID=51179162

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201480042807.XA Pending CN105431286A (zh) 2013-07-29 2014-06-16 具有通过受控纤维铺放生产的孔图案的复合材料层压板

Country Status (8)

Country Link
US (1) US20150030803A1 (enExample)
EP (1) EP3027405B1 (enExample)
JP (2) JP6495275B2 (enExample)
CN (1) CN105431286A (enExample)
BR (1) BR112015032418A8 (enExample)
CA (2) CA3112536C (enExample)
RU (2) RU2656657C2 (enExample)
WO (1) WO2015017033A1 (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110461918A (zh) * 2017-03-31 2019-11-15 三菱化学株式会社 预浸料片、其制造方法、带表皮材的单元层、纤维增强复合材料成型品的制造方法、以及纤维增强复合材料成型品
CN110730834A (zh) * 2017-06-13 2020-01-24 霍尼韦尔国际公司 可透气的轻质单向层压体
CN111016301A (zh) * 2020-01-10 2020-04-17 杭州友凯船艇有限公司 纤维复合材料连接孔周边的增强及其制备方案
CN111655452A (zh) * 2017-12-06 2020-09-11 赛峰航空器发动机 用耐磨材料制造声学通道的有序网络的方法

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12316274B2 (en) 2006-12-06 2025-05-27 Solaredge Technologies Ltd. Pairing of components in a direct current distributed power generation system
US9643392B2 (en) 2013-07-29 2017-05-09 The Boeing Company Septumization of honeycomb sandwiches
US9693166B2 (en) 2014-06-24 2017-06-27 The Boeing Company Automated production of acoustic structures
EP3299153B1 (en) * 2015-05-21 2025-10-29 Mitsubishi Electric Corporation Honeycomb core, honeycomb sandwiching structure, and method for producing honeycomb core
EP3180193A4 (en) 2015-08-11 2017-09-13 SABIC Global Technologies B.V. Multiple ply layered composite having low areal weight
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
US10369756B2 (en) * 2015-08-25 2019-08-06 The Boeing Company Method of manufacturing a composite article
FR3074444A1 (fr) * 2017-12-06 2019-06-07 Safran Aircraft Engines Procede de fabrication d'un reseau ordonne de canaux acoustiques en materiau abradable
EP3720711B1 (fr) * 2017-12-06 2024-12-04 Safran Aircraft Engines Procédé de fabrication additive in situ d'un revêtement abradable sur un carter de turbomachine
US11534992B2 (en) 2019-03-04 2022-12-27 The Boeing Company Tooling assembly and associated system and method for manufacturing a porous composite structure
US11413833B2 (en) 2019-03-04 2022-08-16 The Boeing Company Tooling assembly and associated system and method for manufacturing a porous composite structure
JP7249404B2 (ja) * 2019-03-29 2023-03-30 川崎重工業株式会社 複合材料製パネル構造体およびその製造方法
KR102311748B1 (ko) * 2019-08-05 2021-10-13 한국과학기술연구원 흡음 장치 및 그 제조 방법
CN113002008B (zh) * 2021-04-30 2022-02-22 浙江大学 网格交叉处无碳纤维堆积的复合材料格栅结构及制造方法
WO2022234228A2 (fr) * 2021-05-04 2022-11-10 Safran Aircraft Engines Meta-materiau acoustique et procede pour sa fabrication additive
CN117500768A (zh) * 2021-07-13 2024-02-02 极光先进雷射株式会社 复合部件、激光加工方法和复合部件的制造方法
US20230040244A1 (en) * 2021-08-06 2023-02-09 Raytheon Technologies Corporation Composite fan blade airfoil, methods of manufacture thereof and articles comprising the same
US20240401534A1 (en) * 2023-05-31 2024-12-05 Raytheon Technologies Corporation Acoustic treatment made by additive manufacturing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1784300A (zh) * 2003-05-07 2006-06-07 西门子磁体技术有限公司 用于声阻尼的结构复合材料
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
US20100065367A1 (en) * 2008-09-17 2010-03-18 General Electric Company Method of Manufacture of Composite Laminates, an Assembly Therefor, and Related Articles
CN102667916A (zh) * 2009-11-23 2012-09-12 埃尔塞乐公司 用于飞行器的发动机机舱的声学板的声学表层

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3765980A (en) * 1971-09-24 1973-10-16 Combination Eng Inc Method for forming pipe with integral hole or nozzle pattern
US4600619A (en) * 1984-12-31 1986-07-15 The Boeing Company Continuously wound filament structure for use in noise attenuation element
JPH07173824A (ja) * 1993-11-04 1995-07-11 Mitsui Toatsu Chem Inc 地盤補強材
EP1035963B1 (en) * 1997-11-05 2003-03-19 Sikorsky Aircraft Corporation Feed control system for fiber placement machines
US7807005B2 (en) * 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
JP4990181B2 (ja) * 2007-07-06 2012-08-01 三菱電機株式会社 先進グリッド構造体
US9090028B2 (en) * 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) * 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
RU2385231C1 (ru) * 2008-07-21 2010-03-27 Федеральное государственное унитарное предприятие "Обнинское научно-производственное предприятие "Технология" Способ изготовления слоистых изделий из полимерного композиционного материала
US8052826B2 (en) * 2009-03-24 2011-11-08 The Boeing Company Method of making bead-stiffened composite parts and parts made thereby
JP5836885B2 (ja) * 2011-08-05 2015-12-24 三菱電機株式会社 先進グリッド構造体の製造方法、先進グリッド構造体、および先進グリッド構造体を適用した宇宙望遠鏡
US20140081444A1 (en) * 2012-09-18 2014-03-20 Todd W. Rudberg Sequencer system for an automatic tape laying and projection system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1784300A (zh) * 2003-05-07 2006-06-07 西门子磁体技术有限公司 用于声阻尼的结构复合材料
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
US20100065367A1 (en) * 2008-09-17 2010-03-18 General Electric Company Method of Manufacture of Composite Laminates, an Assembly Therefor, and Related Articles
CN102667916A (zh) * 2009-11-23 2012-09-12 埃尔塞乐公司 用于飞行器的发动机机舱的声学板的声学表层

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110461918A (zh) * 2017-03-31 2019-11-15 三菱化学株式会社 预浸料片、其制造方法、带表皮材的单元层、纤维增强复合材料成型品的制造方法、以及纤维增强复合材料成型品
CN110461918B (zh) * 2017-03-31 2022-06-28 三菱化学株式会社 预浸料片及其制造方法、带表皮材的单元层、纤维增强复合材料成型品及其制造方法
US11421089B2 (en) 2017-03-31 2022-08-23 Mitsubishi Chemical Corporation Prepreg sheet, method for manufacturing same, unit layer with a covering material, method for manufacturing fiber-reinforced composite, and fiber-reinforced composite
CN110730834A (zh) * 2017-06-13 2020-01-24 霍尼韦尔国际公司 可透气的轻质单向层压体
CN110730834B (zh) * 2017-06-13 2022-05-10 霍尼韦尔国际公司 可透气的轻质单向层压体
CN111655452A (zh) * 2017-12-06 2020-09-11 赛峰航空器发动机 用耐磨材料制造声学通道的有序网络的方法
CN111655452B (zh) * 2017-12-06 2023-01-17 赛峰航空器发动机 用耐磨材料制造声学通道的有序网络的方法
CN111016301A (zh) * 2020-01-10 2020-04-17 杭州友凯船艇有限公司 纤维复合材料连接孔周边的增强及其制备方案
CN111016301B (zh) * 2020-01-10 2023-11-17 杭州友凯船艇有限公司 纤维复合材料连接孔周边的增强及其制备方案

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CA2916411A1 (en) 2015-02-05
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CA3112536A1 (en) 2015-02-05
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US20150030803A1 (en) 2015-01-29
RU2765421C2 (ru) 2022-01-31
RU2018118625A3 (enExample) 2021-08-16
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