ES2564837T3 - Estructuras compuestas que emplean laminados cuasi-isótropos - Google Patents

Estructuras compuestas que emplean laminados cuasi-isótropos Download PDF

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Publication number
ES2564837T3
ES2564837T3 ES10707416.3T ES10707416T ES2564837T3 ES 2564837 T3 ES2564837 T3 ES 2564837T3 ES 10707416 T ES10707416 T ES 10707416T ES 2564837 T3 ES2564837 T3 ES 2564837T3
Authority
ES
Spain
Prior art keywords
composite
layers
quasi
composite material
aircraft
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.)
Active
Application number
ES10707416.3T
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English (en)
Spanish (es)
Inventor
Eugene A. Dan-Jumbo
Russell L. Keller
Everett A. Westerman
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
Application granted granted Critical
Publication of ES2564837T3 publication Critical patent/ES2564837T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B32B5/12—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
    • 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
    • B29C70/202—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 arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • 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
    • B32B1/00—Layered products having a non-planar shape
    • 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
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • 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
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08—Layered products comprising a layer of synthetic resin 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • 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
    • B32B27/38—Layered products comprising a layer of synthetic resin comprising 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
    • 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
    • B32B5/22—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
    • 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
    • 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
    • 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
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • 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
    • B29K2995/0045—Isotropic
    • 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
    • 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
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • 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
    • B32B2307/70—Other properties
    • B32B2307/708—Isotropic
    • 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
    • B32B2307/70—Other properties
    • B32B2307/718—Weight, e.g. weight per square meter
    • 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
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
ES10707416.3T 2009-03-10 2010-03-04 Estructuras compuestas que emplean laminados cuasi-isótropos Active ES2564837T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/401,541 US20100233424A1 (en) 2009-03-10 2009-03-10 Composite structures employing quasi-isotropic laminates
US401541 2009-03-10
PCT/US2010/026229 WO2010104741A1 (en) 2009-03-10 2010-03-04 Composite structures employing quasi-isotropic laminates

Publications (1)

Publication Number Publication Date
ES2564837T3 true ES2564837T3 (es) 2016-03-29

Family

ID=42136041

Family Applications (1)

Application Number Title Priority Date Filing Date
ES10707416.3T Active ES2564837T3 (es) 2009-03-10 2010-03-04 Estructuras compuestas que emplean laminados cuasi-isótropos

Country Status (5)

Country Link
US (1) US20100233424A1 (enExample)
EP (1) EP2406071B1 (enExample)
JP (3) JP2012520205A (enExample)
ES (1) ES2564837T3 (enExample)
WO (1) WO2010104741A1 (enExample)

Families Citing this family (48)

* Cited by examiner, † Cited by third party
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
US8617694B1 (en) 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
US8409384B2 (en) * 2009-03-09 2013-04-02 The Boeing Company Predictable bonded rework of composite structures
US9492975B2 (en) 2009-03-09 2016-11-15 The Boeing Company Structural bonded patch with tapered adhesive design
US8524356B1 (en) 2009-03-09 2013-09-03 The Boeing Company Bonded patch having multiple zones of fracture toughness
US8540909B2 (en) 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
US8449703B2 (en) 2009-03-09 2013-05-28 The Boeing Company Predictable bonded rework of composite structures using tailored patches
US8857128B2 (en) * 2009-05-18 2014-10-14 Apple Inc. Reinforced device housing
US8815132B2 (en) * 2010-01-18 2014-08-26 The Boeing Company Method of configuring a patch body
BR112012028784A2 (pt) * 2010-05-11 2016-07-19 Saab Ab artigo compósito que compreende partículas e método para formação de um artigo compósito
US8372495B2 (en) 2010-05-26 2013-02-12 Apple Inc. Electronic device enclosure using sandwich construction
US8765042B2 (en) 2010-06-11 2014-07-01 Airbus Operations Gmbh Fuselage section of an aircraft and method for the production of the fuselage section
DE102010023496B4 (de) * 2010-06-11 2017-02-23 Airbus Operations Gmbh Rumpfsegment eines Flugzeugs
US9120272B2 (en) 2010-07-22 2015-09-01 Apple Inc. Smooth composite structure
US9011623B2 (en) 2011-03-03 2015-04-21 Apple Inc. Composite enclosure
US20140355194A1 (en) * 2012-01-16 2014-12-04 Nec Casio Mobile Communications, Ltd. Portable terminal device
US9545757B1 (en) 2012-02-08 2017-01-17 Textron Innovations, Inc. Composite lay up and method of forming
EP2831328A4 (en) * 2012-03-26 2015-12-02 Saint Gobain Adfors Canada Ltd FABRIC WITH ABORED ANGLES
US20130280477A1 (en) * 2012-03-26 2013-10-24 Peter C. Davis Off-angle laid scrims
US9964096B2 (en) * 2013-01-10 2018-05-08 Wei7 Llc Triaxial fiber-reinforced composite laminate
US20160009368A1 (en) * 2013-02-28 2016-01-14 The Boeing Company Composite laminated plate having reduced crossply angle
US10407955B2 (en) 2013-03-13 2019-09-10 Apple Inc. Stiff fabric
US9314979B1 (en) 2013-07-16 2016-04-19 The Boeing Company Trapezoidal rework patch
CN204608330U (zh) 2013-12-20 2015-09-02 苹果公司 编织纤维带
EP2910365B1 (en) * 2014-02-21 2017-04-26 Airbus Operations GmbH Composite structural element and torsion box
US9850173B2 (en) 2015-01-09 2017-12-26 The Boeing Company Hybrid sandwich ceramic matrix composite
DE102015010436B4 (de) * 2015-08-14 2019-01-24 Airbus Defence and Space GmbH Wabenkern für dimensionsstabile Sandwichbauteile, dessen Verwendung, Sandwichplatte mit diesem Wabenkern und Verfahren zur Herstellung des Wabenkerns
US10005267B1 (en) 2015-09-22 2018-06-26 Textron Innovations, Inc. Formation of complex composite structures using laminate templates
FR3061129B1 (fr) * 2016-12-22 2019-05-31 Airbus Operations Procede de fabrication d'un module d'isolation thermophonique pour aeronef comprenant une etape de cintrage
RU179119U1 (ru) * 2017-09-14 2018-04-26 Российская Федерация, от имени которой выступает ФОНД ПЕРСПЕКТИВНЫХ ИССЛЕДОВАНИЙ Устройство выхода волоконно-оптического датчика из композита
US10864686B2 (en) 2017-09-25 2020-12-15 Apple Inc. Continuous carbon fiber winding for thin structural ribs
US11400657B2 (en) * 2017-10-02 2022-08-02 The Boeing Company Methods of fabrication of composite repair parts and related kits
US12473956B2 (en) * 2019-01-10 2025-11-18 Avient Corporation Resiliently flexible composite articles with overmolded rigid portions
US11318705B2 (en) * 2019-08-26 2022-05-03 The Boeing Company Ply stackings for solid laminate stiffened panel
CN114341289A (zh) 2019-09-25 2022-04-12 3M创新有限公司 多相粘合剂制品及其方法
WO2021106650A1 (ja) * 2019-11-29 2021-06-03 東レ株式会社 繊維強化複合材料およびサンドイッチ構造体
CN114761212B (zh) * 2019-11-29 2024-11-12 东丽株式会社 纤维增强复合材料及夹层结构体
JP2023515929A (ja) * 2020-03-18 2023-04-17 ザ ボード オブ トラスティーズ オブ ザ レランド スタンフォード ジュニア ユニバーシティー 有限サイズの複合積層カード、それから形成されるテーパリングされた複合積層構造、ならびに、その製造方法および使用方法
EP4008538A1 (en) 2020-12-01 2022-06-08 The Boeing Company Rework part for composite structure
WO2022145005A1 (ja) * 2020-12-28 2022-07-07 三菱重工業株式会社 繊維強化シート積層体並びに繊維強化シート積層体の製造方法及び構造体の製造方法
US11969953B2 (en) * 2022-07-26 2024-04-30 The Boeing Company Prepreg charge optimized for forming contoured composite laminate structures
US12049048B2 (en) 2022-07-26 2024-07-30 The Boeing Company Method for high rate production of composite laminate structures
US12630282B2 (en) * 2023-03-03 2026-05-19 Jetzero, Inc. Aircraft with carbon fiber material and a method of manufacture
US12654835B2 (en) * 2023-09-07 2026-06-16 Jetzero, Inc. Dry fiber construction of a blended wing body aircraft and method of manufacture
US12559230B2 (en) 2024-01-18 2026-02-24 Jetzero, Inc. Blended wing body aircraft with landing gear aft of a rear spar
US12187425B1 (en) 2024-01-19 2025-01-07 Jetzero, Inc. Aircraft component with structural foam
US12534177B2 (en) 2024-01-19 2026-01-27 Jetzero, Inc. Centerbody pressure vessel with an arched compression surface

Family Cites Families (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3995080A (en) * 1974-10-07 1976-11-30 General Dynamics Corporation Filament reinforced structural shapes
US4352707A (en) * 1981-04-23 1982-10-05 Grumman Aerospace Corporation Composite repair apparatus
US4497404A (en) * 1983-09-30 1985-02-05 Lowrance William T Protective device for a golf club
US4588853A (en) * 1984-06-21 1986-05-13 Roll Form Products, Inc. Electrical trench grommet member
US4967799A (en) * 1984-08-15 1990-11-06 Dayco Products, Inc. Plastic abrasion-resistant protective sleeve for hose and method of protecting hose
US4588626A (en) * 1984-10-29 1986-05-13 The Boeing Company Blind-side panel repair patch
US5034254A (en) * 1984-10-29 1991-07-23 The Boeing Company Blind-side panel repair patch
US4961799A (en) * 1984-10-29 1990-10-09 The Boeing Company Blind-side panel repair method
US4820564A (en) * 1984-10-29 1989-04-11 The Boeing Company Blind-side repair patch kit
US4916880A (en) * 1986-07-21 1990-04-17 The Boeing Company Apparatus for repairing a hole in a structural wall of composite material
US4978404A (en) * 1986-07-21 1990-12-18 The Boeing Company Method for repairing a hole in a structural wall of composite material
US4912594A (en) * 1986-11-03 1990-03-27 The Boeing Company Integral lightning protection repair system and method for its use
US4824500A (en) * 1987-11-03 1989-04-25 The Dow Chemical Company Method for repairing damaged composite articles
US4808253A (en) * 1987-11-06 1989-02-28 Grumman Aerospace Corporation Method and apparatus for performing a repair on a contoured section of a composite structure
US4858853A (en) * 1988-02-17 1989-08-22 The Boeing Company Bolted repair for curved surfaces
US5207541A (en) * 1988-12-13 1993-05-04 The Boeing Company Scarfing apparatus
US5023987A (en) * 1989-08-28 1991-06-18 The Boeing Company Strato streak flush patch
US5190611A (en) * 1991-02-13 1993-03-02 The Boeing Company Bearing load restoration method for composite structures
JPH04341837A (ja) * 1991-05-17 1992-11-27 Ishikawajima Harima Heavy Ind Co Ltd Ｆｒｐ積層板
US5214307A (en) * 1991-07-08 1993-05-25 Micron Technology, Inc. Lead frame for semiconductor devices having improved adhesive bond line control
US5232962A (en) * 1991-10-09 1993-08-03 Quantum Materials, Inc. Adhesive bonding composition with bond line limiting spacer system
US5344515A (en) * 1993-03-01 1994-09-06 Argo-Tech Corporation Method of making a pump housing
US5374388A (en) * 1993-04-22 1994-12-20 Lockheed Corporation Method of forming contoured repair patches
WO1994025180A1 (en) * 1993-05-05 1994-11-10 Albany International Research Co. Composite sandwich element
US5620768A (en) * 1993-10-15 1997-04-15 Pro Patch Systems, Inc. Repair patch and method of manufacturing thereof
US5601676A (en) * 1994-02-25 1997-02-11 The Board Of Trustees Operating Michigan State University Composite joining and repair
US5709469A (en) * 1995-03-13 1998-01-20 The United States Of America As Represented By The Secretary Of The Air Force Process for testing integrity of bonds between epoxy patches and aircraft structural materials
US5626934A (en) * 1995-10-20 1997-05-06 United States Of America Enhancing damage tolerance of adhesive bonds
US5868886A (en) * 1995-12-22 1999-02-09 Alston; Mark S. Z-pin reinforced bonded composite repairs
US5732743A (en) * 1996-06-14 1998-03-31 Ls Technology Inc. Method of sealing pipes
GB9622780D0 (en) * 1996-11-01 1997-01-08 British Aerospace Repair of composite laminates
FR2763882B1 (fr) * 1997-05-29 1999-08-20 Aerospatiale Outillage de reparation sur site d'une structure composite presentant une zone endommagee et procede correspondant
US5993934A (en) * 1997-08-06 1999-11-30 Eastman Kodak Company Near zero CTE carbon fiber hybrid laminate
US6265333B1 (en) * 1998-06-02 2001-07-24 Board Of Regents, University Of Nebraska-Lincoln Delamination resistant composites prepared by small diameter fiber reinforcement at ply interfaces
JP2001183833A (ja) * 1999-12-27 2001-07-06 Sumitomo Chem Co Ltd レジスト組成物
BR0117299B1 (pt) * 2000-03-03 2014-11-25 Quickstep Technologies Pty Ltd Métodos para unir componentes compósitos
US6472758B1 (en) * 2000-07-20 2002-10-29 Amkor Technology, Inc. Semiconductor package including stacked semiconductor dies and bond wires
EP1473130B1 (en) * 2001-12-06 2011-08-24 Toray Industries, Inc. Fiber-reinforced composite material and method for production thereof
US6656299B1 (en) * 2001-12-19 2003-12-02 Lockheed Martin Corporation Method and apparatus for structural repair
US6761783B2 (en) * 2002-04-09 2004-07-13 The Boeing Company Process method to repair bismaleimide (BMI) composite structures
US6758924B1 (en) * 2002-04-15 2004-07-06 The United States Of America As Represented By The Secretary Of The Air Force Method of repairing cracked aircraft structures
NL1022706C2 (nl) * 2003-02-17 2004-08-19 Stichting Fmlc Laminaat uit metaalplaten en elkaar kruisende dradenlagen uit verschillende materialen in kunststof.
US8246882B2 (en) * 2003-05-02 2012-08-21 The Boeing Company Methods and preforms for forming composite members with interlayers formed of nonwoven, continuous materials
US6764754B1 (en) * 2003-07-15 2004-07-20 The Boeing Company Composite material with improved damping characteristics and method of making same
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
JP4118264B2 (ja) * 2004-07-15 2008-07-16 本田技研工業株式会社 衝撃吸収部材
US20060029807A1 (en) * 2004-08-04 2006-02-09 Peck Scott O Method for the design of laminated composite materials
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
EP1683627A1 (en) * 2005-01-25 2006-07-26 Saab Ab Method and apparatus for repairing a composite article
US8444087B2 (en) * 2005-04-28 2013-05-21 The Boeing Company Composite skin and stringer structure and method for forming the same
JP2007016122A (ja) * 2005-07-07 2007-01-25 Toray Ind Inc 炭素繊維強化複合材料
US20070095457A1 (en) * 2005-11-02 2007-05-03 The Boeing Company Fast line maintenance repair method and system for composite structures
US7398698B2 (en) * 2005-11-03 2008-07-15 The Boeing Company Smart repair patch and associated method
US7935205B2 (en) * 2006-06-19 2011-05-03 United Technologies Corporation Repair of composite sandwich structures
US7628879B2 (en) * 2007-08-23 2009-12-08 The Boeing Company Conductive scrim embedded structural adhesive films
GB0721546D0 (en) * 2007-11-01 2007-12-12 Rolls Royce Plc Composite material repair
US8540909B2 (en) * 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
US8617694B1 (en) * 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
US8409384B2 (en) * 2009-03-09 2013-04-02 The Boeing Company Predictable bonded rework of composite structures
US8449703B2 (en) * 2009-03-09 2013-05-28 The Boeing Company Predictable bonded rework of composite structures using tailored patches

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JP6162186B2 (ja) 2017-07-12
EP2406071B1 (en) 2016-03-02
WO2010104741A1 (en) 2010-09-16
US20100233424A1 (en) 2010-09-16
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JP2012520205A (ja) 2012-09-06
JP2016020206A (ja) 2016-02-04

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