RU2641404C2 - Топливный бак, основные крылья, корпус летательного аппарата, летательный аппарат и транспортное средство - Google Patents

Топливный бак, основные крылья, корпус летательного аппарата, летательный аппарат и транспортное средство Download PDF

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Publication number
RU2641404C2
RU2641404C2 RU2015140425A RU2015140425A RU2641404C2 RU 2641404 C2 RU2641404 C2 RU 2641404C2 RU 2015140425 A RU2015140425 A RU 2015140425A RU 2015140425 A RU2015140425 A RU 2015140425A RU 2641404 C2 RU2641404 C2 RU 2641404C2
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RU
Russia
Prior art keywords
fuel tank
cfrp
bolt
fuel
structural element
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RU2015140425A
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English (en)
Russian (ru)
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RU2015140425A (ru
Inventor
Нобуюки КАМИХАРА
Кадзуаки КИСИМОТО
Тосио АБЭ
Юйтиро КАМИНО
Original Assignee
Мицубиси Хеви Индастрис, Лтд.
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    • 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
    • B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
    • 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
    • B32B7/08—Interconnection of layers by mechanical means
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal 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
    • B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • 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
    • B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • 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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
    • 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
    • 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
    • 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
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Fuel Cell (AREA)
RU2015140425A 2013-03-26 2014-01-28 Топливный бак, основные крылья, корпус летательного аппарата, летательный аппарат и транспортное средство RU2641404C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2013064444A JP6113544B2 (ja) 2013-03-26 2013-03-26 燃料タンク、主翼、航空機胴体、航空機及び移動体
JP2013-064444 2013-03-26
PCT/JP2014/051831 WO2014156274A1 (ja) 2013-03-26 2014-01-28 燃料タンク、主翼、航空機胴体、航空機及び移動体

Publications (2)

Publication Number Publication Date
RU2015140425A RU2015140425A (ru) 2017-04-27
RU2641404C2 true RU2641404C2 (ru) 2018-01-17

Family

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RU2015140425A RU2641404C2 (ru) 2013-03-26 2014-01-28 Топливный бак, основные крылья, корпус летательного аппарата, летательный аппарат и транспортное средство

Country Status (8)

Country Link
US (1) US20160052638A1 (enExample)
EP (1) EP2979977B1 (enExample)
JP (1) JP6113544B2 (enExample)
CN (1) CN105102319B (enExample)
BR (1) BR112015024865A8 (enExample)
CA (1) CA2907845C (enExample)
RU (1) RU2641404C2 (enExample)
WO (1) WO2014156274A1 (enExample)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6139582B2 (ja) * 2015-02-23 2017-05-31 株式会社Ｓｕｂａｒｕ 航空機用構造体、航空機用構造体の製造方法及び航空機用構造体の設計情報の作成方法
JP2016190627A (ja) * 2015-03-31 2016-11-10 三菱重工業株式会社 構造体製造装置、構造体製造方法、および構造体
CN105501450B (zh) * 2015-11-30 2020-09-18 中国航空工业集团公司沈阳飞机设计研究所 一种无人机复合材料整体油箱密封方法
EP3252842B1 (en) * 2016-06-01 2025-11-19 Airbus Operations GmbH Structural composite component and method for configuring a structural composite component
GB2551560A (en) * 2016-06-22 2017-12-27 Airbus Operations Ltd A method of forming a structural portion of a fuel tank for an aircraft
US10052847B2 (en) * 2016-09-16 2018-08-21 The Boeing Company Method for promoting electrical conduction between metallic components and composite materials
CN106585957B (zh) * 2016-12-14 2023-03-31 中航通飞研究院有限公司 一种复合材料机翼整体油箱及其制造方法
CN107140178A (zh) * 2017-06-05 2017-09-08 芜湖中科飞机制造有限公司 基础教练机的机翼结构
CN107264817A (zh) * 2017-06-05 2017-10-20 芜湖中科飞机制造有限公司 机翼油箱
JP6778221B2 (ja) 2018-01-15 2020-10-28 株式会社Ｓｕｂａｒｕ 締結構造
JP6770987B2 (ja) 2018-03-12 2020-10-21 株式会社Ｓｕｂａｒｕ 複合材構造体、航空機及び雷電流の誘導方法
US11046416B2 (en) * 2018-08-03 2021-06-29 Aurora Flight Sciences Corporation Combination flight and ground apparatus for a vehicle
US11038334B2 (en) * 2019-01-14 2021-06-15 The Boeing Company Aircraft wing composite ribs having electrical grounding paths
CN111113947A (zh) * 2019-12-18 2020-05-08 华侨大学 一种fase赛车pmi翼片及一种fase赛车pmi翼片成型工艺
CN112072335B (zh) * 2020-09-25 2022-06-24 中国直升机设计研究所 一种复合材料结构件之间导电结构及导电处理方法
CN113415430A (zh) * 2021-07-30 2021-09-21 天津爱思达新材料科技有限公司 飞机副油箱吊耳梁结构
CN116424545A (zh) * 2023-05-10 2023-07-14 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种机翼油箱及其生产方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1362681A1 (ru) * 1986-04-10 1987-12-30 Государственный научно-исследовательский институт гражданской авиации Устройство дл молниезащиты внешних топливных баков летательного аппарата
US6114050A (en) * 1996-01-11 2000-09-05 The Boeing Company Titanium-polymer hybrid laminates
US6327132B1 (en) * 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
RU2192991C2 (ru) * 2000-12-18 2002-11-20 Открытое Акционерное Общество "Московский Вертолетный Завод Им. М.Л. Миля" Способ защиты топливных баков вертолета от термического воздействия тока молнии
US20100264274A1 (en) * 2009-04-20 2010-10-21 Airbus Operations Limited Edge seal for fibre-reinforced composite structure
WO2012074639A1 (en) * 2010-12-03 2012-06-07 The Boeing Company Electric charge dissipation system for aircraft

Family Cites Families (18)

* 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
GB9807198D0 (en) * 1998-04-04 1998-06-03 British Aerospace Adhesively bonded joints in carbon fibre composite structures
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.
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
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
JP2010194749A (ja) * 2009-02-23 2010-09-09 Mitsubishi Heavy Ind Ltd 樹脂基複合材の製造方法
ES2376323B1 (es) * 2009-02-27 2013-01-24 Airbus Operations, S.L. Mejora de la protección contra impacto directo de rayos en zonas remachadas de paneles en cfrp.
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
JP5455541B2 (ja) * 2009-10-14 2014-03-26 三菱重工業株式会社 ストリンガーの製造方法
US8475102B2 (en) * 2009-10-22 2013-07-02 Alcoa Inc. Enhanced conductivity sleeved fastener and method for making same
JP5619446B2 (ja) * 2010-03-23 2014-11-05 三菱重工業株式会社 キャップ、これを用いた締結構造およびこの締結構造を有する航空機
CN104203752A (zh) * 2012-03-26 2014-12-10 三菱重工业株式会社 燃料箱、主翼、航空器主体、航空器及移动体
JP6071686B2 (ja) * 2013-03-26 2017-02-01 三菱重工業株式会社 燃料タンク、主翼、航空機胴体、航空機及び移動体

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1362681A1 (ru) * 1986-04-10 1987-12-30 Государственный научно-исследовательский институт гражданской авиации Устройство дл молниезащиты внешних топливных баков летательного аппарата
US6114050A (en) * 1996-01-11 2000-09-05 The Boeing Company Titanium-polymer hybrid laminates
US6327132B1 (en) * 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
RU2192991C2 (ru) * 2000-12-18 2002-11-20 Открытое Акционерное Общество "Московский Вертолетный Завод Им. М.Л. Миля" Способ защиты топливных баков вертолета от термического воздействия тока молнии
US20100264274A1 (en) * 2009-04-20 2010-10-21 Airbus Operations Limited Edge seal for fibre-reinforced composite structure
WO2012074639A1 (en) * 2010-12-03 2012-06-07 The Boeing Company Electric charge dissipation system for aircraft

Also Published As

Publication number Publication date
EP2979977B1 (en) 2018-08-15
EP2979977A1 (en) 2016-02-03
BR112015024865A8 (pt) 2019-12-17
CN105102319A (zh) 2015-11-25
CA2907845C (en) 2018-02-13
BR112015024865A2 (pt) 2017-07-18
JP2014189070A (ja) 2014-10-06
CN105102319B (zh) 2018-09-28
CA2907845A1 (en) 2014-10-02
JP6113544B2 (ja) 2017-04-12
US20160052638A1 (en) 2016-02-25
WO2014156274A1 (ja) 2014-10-02
RU2015140425A (ru) 2017-04-27
EP2979977A4 (en) 2016-12-14

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