BR112015024865A2 - tanque de combustível, asas principais, fuselagem da aeronave, aeronave e estrutura em movimento - Google Patents
tanque de combustível, asas principais, fuselagem da aeronave, aeronave e estrutura em movimentoInfo
- Publication number
- BR112015024865A2 BR112015024865A2 BR112015024865A BR112015024865A BR112015024865A2 BR 112015024865 A2 BR112015024865 A2 BR 112015024865A2 BR 112015024865 A BR112015024865 A BR 112015024865A BR 112015024865 A BR112015024865 A BR 112015024865A BR 112015024865 A2 BR112015024865 A2 BR 112015024865A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- fuel tank
- moving structure
- main wings
- carbon fiber
- Prior art date
Links
- 239000002828 fuel tank Substances 0.000 title abstract 4
- 239000004918 carbon fiber reinforced polymer Substances 0.000 abstract 2
- 229920000049 Carbon (fiber) Polymers 0.000 abstract 1
- 239000004917 carbon fiber Substances 0.000 abstract 1
- 238000010030 laminating Methods 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 abstract 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 abstract 1
- 239000004033 plastic Substances 0.000 abstract 1
- 229920003023 plastic Polymers 0.000 abstract 1
- 239000012779 reinforcing material Substances 0.000 abstract 1
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
- 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
- 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
- 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)
Abstract
resumo tanque de combustível, asas principais, fuselagem da aeronave, aeronave e estrutura em movimento o propósito da presente invenção é fornecer um tanque de combustível, asas principais, uma fuselagem de aeronave, uma aeronave e uma estrutura em movimento que permitam que as horas de trabalho e os custos envolvidos no ge-renciamento da qualidade sejam reduzidos, e aumentos de peso sejam evitados. o tanque de combustível compreende um membro estrutural que usa um plástico re-forçado de fibra de carbono (cfrp) (15), incluindo um material de reforço contendo fibra de carbono e uma matriz contendo plástico. o membro estrutural é formado pela laminação de folhas condutivas (17) entre prepregs do plástico reforçado com fibra de carbono (cfrp) (15), e é formado com um orifício de fixação (22) ao qual um parafuso passante é fixado.
Applications Claiming Priority (2)
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 |
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 |
---|---|
BR112015024865A2 true BR112015024865A2 (pt) | 2017-07-18 |
BR112015024865A8 BR112015024865A8 (pt) | 2019-12-17 |
Family
ID=51623276
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015024865A BR112015024865A8 (pt) | 2013-03-26 | 2014-01-28 | tanque de combustível, asas principais, fuselagem da aeronave, aeronave e estrutura móvel |
Country Status (8)
Country | Link |
---|---|
US (1) | US20160052638A1 (pt) |
EP (1) | EP2979977B1 (pt) |
JP (1) | JP6113544B2 (pt) |
CN (1) | CN105102319B (pt) |
BR (1) | BR112015024865A8 (pt) |
CA (1) | CA2907845C (pt) |
RU (1) | RU2641404C2 (pt) |
WO (1) | WO2014156274A1 (pt) |
Families Citing this family (17)
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 |
EP3252842A1 (en) * | 2016-06-01 | 2017-12-06 | 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 |
CN107264817A (zh) * | 2017-06-05 | 2017-10-20 | 芜湖中科飞机制造有限公司 | 机翼油箱 |
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 |
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 |
JP7114364B2 (ja) | 2018-06-22 | 2022-08-08 | キヤノン株式会社 | 電源装置及び画像形成装置 |
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 |
Family Cites Families (24)
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 |
SU1362681A1 (ru) * | 1986-04-10 | 1987-12-30 | Государственный научно-исследовательский институт гражданской авиации | Устройство дл молниезащиты внешних топливных баков летательного аппарата |
US4755904A (en) * | 1986-06-06 | 1988-07-05 | The Boeing Company | Lightning protection system for conductive composite material structure |
US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
GB9807198D0 (en) * | 1998-04-04 | 1998-06-03 | British Aerospace | Adhesively bonded joints in carbon fibre composite structures |
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 |
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 |
GB0906686D0 (en) * | 2009-04-20 | 2009-06-03 | Airbus Uk Ltd | Edge seal for fibre-reinforced composite structure |
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 |
WO2011050040A1 (en) * | 2009-10-22 | 2011-04-28 | 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 |
US9802714B2 (en) * | 2010-12-03 | 2017-10-31 | The Boeing Company | Electric charge dissipation system for aircraft |
WO2013146335A1 (ja) * | 2012-03-26 | 2013-10-03 | 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 |
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 |
-
2013
- 2013-03-26 JP JP2013064444A patent/JP6113544B2/ja active Active
-
2014
- 2014-01-28 CN CN201480018287.9A patent/CN105102319B/zh not_active Expired - Fee Related
- 2014-01-28 CA CA2907845A patent/CA2907845C/en active Active
- 2014-01-28 BR BR112015024865A patent/BR112015024865A8/pt not_active IP Right Cessation
- 2014-01-28 RU RU2015140425A patent/RU2641404C2/ru active
- 2014-01-28 WO PCT/JP2014/051831 patent/WO2014156274A1/ja active Application Filing
- 2014-01-28 EP EP14776202.5A patent/EP2979977B1/en active Active
- 2014-01-28 US US14/780,156 patent/US20160052638A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
RU2015140425A (ru) | 2017-04-27 |
CA2907845C (en) | 2018-02-13 |
JP2014189070A (ja) | 2014-10-06 |
EP2979977A4 (en) | 2016-12-14 |
CN105102319A (zh) | 2015-11-25 |
RU2641404C2 (ru) | 2018-01-17 |
CA2907845A1 (en) | 2014-10-02 |
EP2979977A1 (en) | 2016-02-03 |
CN105102319B (zh) | 2018-09-28 |
JP6113544B2 (ja) | 2017-04-12 |
WO2014156274A1 (ja) | 2014-10-02 |
US20160052638A1 (en) | 2016-02-25 |
BR112015024865A8 (pt) | 2019-12-17 |
EP2979977B1 (en) | 2018-08-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112015024865A2 (pt) | tanque de combustível, asas principais, fuselagem da aeronave, aeronave e estrutura em movimento | |
JP2014189070A5 (pt) | ||
Lee et al. | On the use of nanocellulose as reinforcement in polymer matrix composites | |
BR112014017646A8 (pt) | Pré-impregnado, métodos para produzir um pré-impregnado, e de fabricação de um membro estrutural de material compósito reforçado com fibra, e, uso de um pré-impregnado | |
CA2814894C (en) | Optimized cross-ply orientation in composite laminates | |
BR112015024429A2 (pt) | tanque de combustível, asas principais, fuselagem de aeronave, aeronave e corpo móvel | |
BR112014020090A8 (pt) | Aeronave para decolagem e aterrissagem vertical com duas disposições de asa | |
BR112014031120A2 (pt) | aperfeiçoamentos em materiais compósitos | |
BR112017005619A2 (pt) | material compósito curável, e, métodos para fabricar uma estrutura de compósito e para fabricar um material compósito. | |
BR112018069617A2 (pt) | material compósito reforçado por fibra, laminado, tubo, tubo de elevação e saída de lama | |
ATE542741T1 (de) | Befestigung für pylonkasten an flügeln, festklemmen einer seitenplatte des kastens | |
BR112014018371A8 (pt) | Método de fabricação de painel | |
BR112013024886A2 (pt) | pré-impregnado, material compósito reforçado com fibra e método para fabricação de um material compósito reforçado com fibra | |
BR112016030776A8 (pt) | pré-forma, e, métodos para fabricação de uma estrutura compósita e para fabricação de fitas fibrosas secas para deposição de fitas automatizada | |
BR112015010679A2 (pt) | sistema de resina epóxi curável, processo para formar um compósito de epóxi reforçado com fibra e compósito reforçado com fibra curada | |
CO2018001016A2 (es) | Método de preparación de tereftalato de polietileno reforzado con grafeno mediante moldeo por inyección | |
BR112014015544A2 (pt) | Pré-impregnado, método de processamento de pré-impregnado e material compósito reforçado por fibra | |
BR112014013091A2 (pt) | melhorias em ou relacionadas aos compósitos reforçados com fibra | |
BR112017002081A2 (pt) | elemento de superfície de controle para uma aeronave | |
BR112013017151A2 (pt) | película ou espuma reforçada, estrutura em multicamada e artigo | |
BR112014015515B8 (pt) | Núcleo estrutural e painel compósito | |
RU2015109128A (ru) | Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата | |
BR112017018404A2 (pt) | adesivo em duas partes incluindo curativos reforçados | |
BR112017006209A2 (pt) | lâmina de energia eólica, e, método para fabricação da lâmina de energia eólica | |
BR112017005088A2 (pt) | caixa de ventoinha para um mecanis¬mo de propulsão de aeronave |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 8A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2655 DE 23-11-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |