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RU2015109128A - Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата - Google Patents

Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата Download PDF

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RU2015109128A
RU2015109128A RU2015109128A RU2015109128A RU2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A
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structural
fuel tank
structural elements
main wing
elements according
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RU2015109128A
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RU2605716C2 (ru
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Нобуюки КАМИХАРА
Тосио АБЭ
Акихиса ОКУДА
Акира ИКАДА
Масаюки ЯМАСИТА
Кадзуаки КИСИМОТО
Юйтиро КАМИНО
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Мицубиси Хеви Индастрис, Лтд.
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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
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • B64D37/04—Arrangement thereof in or on aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • B64D37/06—Constructional adaptations thereof
    • B64D37/08—Internal partitioning
    • 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
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
    • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
    • 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
    • C08J7/00—Chemical treatment or coating of shaped articles made of macromolecular substances
    • C08J7/04—Coating
    • C08J7/0427—Coating with only one layer of a composition containing a polymer binder
    • 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
    • C08J7/00—Chemical treatment or coating of shaped articles made of macromolecular substances
    • C08J7/04—Coating
    • C08J7/044—Forming conductive coatings; Forming coatings having anti-static 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/34—Tanks constructed integrally with wings, e.g. for fuel or water
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/02—Lightning protectors; Static dischargers
    • 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
    • C08J2300/00—Characterised by the use of unspecified polymers
    • 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
    • C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
    • 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
    • C08J2367/00—Characterised by the use of polyesters obtained by reactions forming a carboxylic ester link in the main chain; Derivatives of such polymers
    • C08J2367/06—Unsaturated polyesters
    • 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
    • C08J2400/00—Characterised by the use of unspecified polymers
    • C08J2400/12—Polymers characterised by physical features, e.g. anisotropy, viscosity or electrical conductivity
    • 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
    • C08J7/00—Chemical treatment or coating of shaped articles made of macromolecular substances
    • C08J7/04—Coating
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31511—Of epoxy ether
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31786—Of polyester [e.g., alkyd, etc.]

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Polymers & Plastics (AREA)
  • Health & Medical Sciences (AREA)
  • Organic Chemistry (AREA)
  • Medicinal Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
  • Coating Of Shaped Articles Made Of Macromolecular Substances (AREA)

Abstract

1. Конструкционный материал для конструкций, содержащий:пластик, армированный углеродным волокном, в котором армирующий материал включает в себя углеродные волокна, а матрица включает в себя пластик;материал для защиты поверхности, обладающий низкой вязкостью, которому придана электропроводность за счет нанесения пластика, армированного углеродным волокном, на поверхность, на которой выступают окончания углеродных волокон.2. Конструкционный материал для элементов конструкции по п. 1, в котором матрице придана электропроводность.3. Конструкционный материал для элементов конструкции по п. 1, в котором удельное объемное сопротивление составляет 0,5 Ом·см и менее.4. Топливный бак, включающий в себя конструкционный материал для элементов конструкции по любому из пп. 1-3, в котором на поверхность, обращенную внутрь топливного бака, где хранится топливо, нанесен материал для защиты поверхности.5. Основное крыло, включающее в себя топливный бак по п. 4, который представляет собой элемент конструкции.6. Летательный аппарат, включающий в себя основное крыло по п. 5.

Claims (6)

1. Конструкционный материал для конструкций, содержащий:
пластик, армированный углеродным волокном, в котором армирующий материал включает в себя углеродные волокна, а матрица включает в себя пластик;
материал для защиты поверхности, обладающий низкой вязкостью, которому придана электропроводность за счет нанесения пластика, армированного углеродным волокном, на поверхность, на которой выступают окончания углеродных волокон.
2. Конструкционный материал для элементов конструкции по п. 1, в котором матрице придана электропроводность.
3. Конструкционный материал для элементов конструкции по п. 1, в котором удельное объемное сопротивление составляет 0,5 Ом·см и менее.
4. Топливный бак, включающий в себя конструкционный материал для элементов конструкции по любому из пп. 1-3, в котором на поверхность, обращенную внутрь топливного бака, где хранится топливо, нанесен материал для защиты поверхности.
5. Основное крыло, включающее в себя топливный бак по п. 4, который представляет собой элемент конструкции.
6. Летательный аппарат, включающий в себя основное крыло по п. 5.
RU2015109128/05A 2012-10-09 2013-10-09 Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата RU2605716C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2012224141 2012-10-09
JP2012-224141 2012-10-09
PCT/JP2013/077434 WO2014057960A1 (ja) 2012-10-09 2013-10-09 構造体用構造材、燃料タンク、主翼及び航空機

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RU2015109128A true RU2015109128A (ru) 2016-12-10
RU2605716C2 RU2605716C2 (ru) 2016-12-27

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JP (1) JP5852255B2 (ru)
CN (1) CN104640913B (ru)
BR (1) BR112015006133A2 (ru)
CA (1) CA2885204C (ru)
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WO (1) WO2014057960A1 (ru)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160196891A1 (en) * 2014-09-26 2016-07-07 The Boeing Company Method for mitigating edge glow
JP6580359B2 (ja) * 2015-03-31 2019-09-25 三菱重工業株式会社 構造体製造方法および構造体
US10472473B2 (en) * 2015-05-26 2019-11-12 The Boeing Company Enhancing z-conductivity in carbon fiber reinforced plastic composite layups
KR20180089449A (ko) * 2015-11-30 2018-08-08 사이텍 인더스트리스 인코포레이티드 복합 구조용 표면 재료
CN109789662A (zh) 2016-09-27 2019-05-21 3M创新有限公司 保护膜
CN109131904A (zh) * 2018-09-28 2019-01-04 成都飞机工业（集团）有限责任公司 一种抗冲击的飞机整体油箱
US11038334B2 (en) * 2019-01-14 2021-06-15 The Boeing Company Aircraft wing composite ribs having electrical grounding paths
US10913548B2 (en) 2019-01-14 2021-02-09 The Boeing Company Metallic fittings for coupling composite ribs to skin panels of aircraft wings
CN111196733B (zh) * 2020-01-09 2021-06-04 青岛理工大学 一种氧化致型形状记忆纤维及其制备方法和应用
JP2021178415A (ja) * 2020-05-12 2021-11-18 パナソニックＩｐマネジメント株式会社 樹脂成形品
JP2023073774A (ja) * 2021-11-16 2023-05-26 三菱重工業株式会社 複合材料構造体及び複合材料構造体の製造方法

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4556591A (en) * 1981-09-25 1985-12-03 The Boeing Company Conductive bonded/bolted joint seals for composite aircraft
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
JPH0263725A (ja) 1988-05-27 1990-03-05 Mitsubishi Heavy Ind Ltd 炭素繊維強化プラスチツク部材の組立方法
US6086975A (en) 1991-01-16 2000-07-11 The Boeing Company Lighting protection for electrically conductive or insulating skin and core for honeycomb structure
JPH0616846A (ja) 1992-07-03 1994-01-25 Hitachi Zosen Corp 導電性を有する繊維強化合成樹脂
CA2125378A1 (en) 1993-06-09 1994-12-10 James A. E. Bell Composition for lightning strike protection and improved electrical conductivity
GB9419765D0 (en) * 1994-09-30 1994-11-16 Symons Richard D Storage of sensitive media
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US6327132B1 (en) * 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
JP2003154591A (ja) 2001-09-04 2003-05-27 Toray Ind Inc 繊維強化熱可塑性プラスチック
US20050175813A1 (en) * 2004-02-10 2005-08-11 Wingert A. L. Aluminum-fiber laminate
ES2279664B1 (es) * 2004-12-30 2008-08-01 Airbus España S.L. Dispositivo de proteccion contra descargas electricas en aeronaves.
WO2008048705A2 (en) 2006-03-10 2008-04-24 Goodrich Corporation Low density lightning strike protection for use in airplanes
JP4972341B2 (ja) 2006-05-11 2012-07-11 富士重工業株式会社 ３次元繊維強化樹脂複合材
US20080012681A1 (en) * 2006-05-26 2008-01-17 Paul Kadar Thermally protected electrical wiring device
JP4969363B2 (ja) 2006-08-07 2012-07-04 東レ株式会社 プリプレグおよび炭素繊維強化複合材料
GB0622060D0 (en) * 2006-11-06 2006-12-13 Hexcel Composites Ltd Improved composite materials
US7599164B2 (en) * 2006-12-07 2009-10-06 The Boeing Company Lightning protection system for aircraft composite structure
RU2381242C2 (ru) 2008-04-15 2010-02-10 Институт химии и химической технологии СО РАН Композиционный износостойкий материал на основе сверхвысокомолекулярного полиэтилена (свмпэ)
JP5155833B2 (ja) * 2008-12-01 2013-03-06 三菱重工業株式会社 航空機の燃料タンク
JP2010194749A (ja) * 2009-02-23 2010-09-09 Mitsubishi Heavy Ind Ltd 樹脂基複合材の製造方法
JP5101554B2 (ja) * 2009-03-30 2012-12-19 三菱重工業株式会社 航空機の燃料タンク
JP5237170B2 (ja) * 2009-03-30 2013-07-17 三菱重工業株式会社 複合材タンク、翼、および、複合材タンクの製造方法
GB0912016D0 (en) * 2009-07-10 2009-08-19 Airbus Operations Ltd Edge glow protection for composite component
CN101984009B (zh) * 2010-10-26 2012-10-31 浙江大学 一种抗雷击导电涂料及其制备方法
JP5773679B2 (ja) 2011-02-16 2015-09-02 三菱重工業株式会社 炭素繊維強化プラスチック構造体及びその製造方法
US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler

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US9776732B2 (en) 2017-10-03
CA2885204C (en) 2017-02-28
JPWO2014057960A1 (ja) 2016-09-05
JP5852255B2 (ja) 2016-02-03
WO2014057960A1 (ja) 2014-04-17
CA2885204A1 (en) 2014-04-17
BR112015006133A2 (pt) 2019-11-19
RU2605716C2 (ru) 2016-12-27
US20150274316A1 (en) 2015-10-01
CN104640913A (zh) 2015-05-20
CN104640913B (zh) 2017-12-12

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