BRPI0806895A2 - Elemento de conexão e uso de tal elemento de conexão para fixação de componentes de aeronave no caso de uma construção híbrida de cfk-metal. - Google Patents

Elemento de conexão e uso de tal elemento de conexão para fixação de componentes de aeronave no caso de uma construção híbrida de cfk-metal.

Info

Publication number
BRPI0806895A2
BRPI0806895A2 BRPI0806895-0A2A BRPI0806895A BRPI0806895A2 BR PI0806895 A2 BRPI0806895 A2 BR PI0806895A2 BR PI0806895 A BRPI0806895 A BR PI0806895A BR PI0806895 A2 BRPI0806895 A2 BR PI0806895A2
Authority
BR
Brazil
Prior art keywords
connection element
cfk
hybrid
case
metal construction
Prior art date
Application number
BRPI0806895-0A2A
Other languages
English (en)
Inventor
Michael Kolax
Wolf-Dietrich Dolzinski
Original Assignee
Airbus Gmbh
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 Airbus Gmbh filed Critical Airbus Gmbh
Publication of BRPI0806895A2 publication Critical patent/BRPI0806895A2/pt

Links

Classifications

    • 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04—Rivets; Spigots or the like fastened by riveting
    • F16B19/06—Solid rivets made in one piece
    • 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
    • Y10T403/00—Joints and connections
    • Y10T403/75—Joints and connections having a joining piece extending through aligned openings in plural members

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Insertion Pins And Rivets (AREA)
  • Laminated Bodies (AREA)
BRPI0806895-0A2A 2007-01-23 2008-01-22 Elemento de conexão e uso de tal elemento de conexão para fixação de componentes de aeronave no caso de uma construção híbrida de cfk-metal. BRPI0806895A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US89736207P 2007-01-23 2007-01-23
DE102007003276A DE102007003276B4 (de) 2007-01-23 2007-01-23 Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind
PCT/EP2008/050692 WO2008090144A1 (en) 2007-01-23 2008-01-22 Connecting element and use of such a connecting element for fastening aircraft components in the case of a cfk-metal hybrid construction

Publications (1)

Publication Number Publication Date
BRPI0806895A2 true BRPI0806895A2 (pt) 2014-04-15

Family

ID=39563718

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0806895-0A2A BRPI0806895A2 (pt) 2007-01-23 2008-01-22 Elemento de conexão e uso de tal elemento de conexão para fixação de componentes de aeronave no caso de uma construção híbrida de cfk-metal.

Country Status (9)

Country Link
US (1) US8844868B2 (pt)
EP (1) EP2106365B1 (pt)
JP (1) JP2010516538A (pt)
CN (1) CN101631719B (pt)
BR (1) BRPI0806895A2 (pt)
CA (1) CA2671917A1 (pt)
DE (1) DE102007003276B4 (pt)
RU (1) RU2009124190A (pt)
WO (1) WO2008090144A1 (pt)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0819159D0 (en) * 2008-10-20 2008-11-26 Airbus Uk Ltd Joint between aircraft components
US8336820B2 (en) * 2008-10-27 2012-12-25 Embraer S.A. Aircraft cabin floor structures, systems and methods
JP5625260B2 (ja) * 2009-04-21 2014-11-19 株式会社豊田自動織機 繊維強化複合材及び繊維強化複合材の締結構造
DE102009048157B4 (de) 2009-10-02 2019-05-29 Audi Ag Vorrichtung zur Anbringung eines Anbauteils an einem aus einem Faserverbundwerkstoff bestehenden Bauteil
JP5473892B2 (ja) * 2010-12-28 2014-04-16 三菱航空機株式会社 耐雷ファスナ、航空機
EP2689149B1 (en) * 2011-03-24 2017-05-03 Arconic Inc. Hybrid collar for fastening systems
RU2475425C1 (ru) * 2011-10-06 2013-02-20 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" Устройство металлизации корпуса изделия
DE102011119596A1 (de) * 2011-11-29 2013-05-29 Tox Pressotechnik Gmbh & Co. Kg Stanzniet mit einem Nietelement aus einem Kopfabschnitt, einem Schaftabschnitt und einem Fußabschnitt
DE102012001859B4 (de) * 2012-02-01 2015-04-23 Daimler Ag Verbindungsanordnung und Verfahren zum Verbinden wenigstens eines ersten Bauteils aus einem kohlefaserverstärkten Verbundwerkstoff mit wenigstens einem zweiten Bauteil
FR2986580B1 (fr) * 2012-02-08 2014-02-28 Safran Piece de revolution de rotor de turbomachine aeronautique
JP2013249918A (ja) * 2012-06-01 2013-12-12 Sumitomo Electric Ind Ltd 締結構造体およびその製造方法
JP2013249917A (ja) * 2012-06-01 2013-12-12 Sumitomo Electric Ind Ltd 締結構造体
JP5730929B2 (ja) * 2012-06-11 2015-06-10 株式会社呉英製作所 カップ型回転砥石
US20140079523A1 (en) * 2012-09-14 2014-03-20 Caterpillar Inc. Joint interface for laminate structures
KR101457469B1 (ko) 2012-12-18 2014-11-04 주식회사 성우하이텍 복합 소재와 금속재의 접합 유닛
DE102012223863A1 (de) * 2012-12-19 2014-06-26 Bayerische Motoren Werke Aktiengesellschaft Befestigungsvorrichtung für ein aus einem kohlenstofffaserverstärkten Kunststoff bestehendes Bauteil an einer Komponente, insbes. einer Fahrwerkskomponente eines Fahrzeugs
US9303671B2 (en) 2013-01-15 2016-04-05 GM Global Technology Operations LLC Method of isolating metallic fasteners in composite panels
JP5729429B2 (ja) * 2013-07-29 2015-06-03 トヨタ自動車株式会社 接合構造、及び接合構造の製造方法
DE102013215502A1 (de) 2013-08-07 2015-02-12 Bayerische Motoren Werke Aktiengesellschaft Nicht-lösbare punktuelle Verbindung für CFK zur Maximierung der übertragbaren Last
DE102014113438A1 (de) 2013-11-06 2015-05-07 Profil Verbindungstechnik Gmbh & Co. Kg Verfahren zum Verbinden von Blechteilen und Zusammenbauteil sowie Setzkopf und Matrize
US10518819B2 (en) * 2014-06-30 2019-12-31 Basf Se Composite thermoplastic structure and composite compression limiter for same
DE102014216790A1 (de) 2014-08-22 2016-02-25 Richard Bergner Holding GmbH & Co. KG Verfahren zur Herstellung eines Verbindungselements sowie Verbindungselement und CFK-Bauteil mit einem derartigen Verbindungselement
DE102014220337A1 (de) 2014-10-08 2016-04-14 Richard Bergner Holding GmbH & Co. KG Verfahren zur Herstellung eines Verbindungselements sowie Verbindungselement und CFK-Bauteil mit einem derartigen Verbindungselement
US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler
JP6354662B2 (ja) * 2015-05-27 2018-07-11 トヨタ自動車株式会社 車両用部材の接合構造及び車両用部材の接合方法
CN105398557A (zh) * 2015-10-29 2016-03-16 苏州金业船用机械厂 一种耐腐蚀性螺旋桨桨叶
DE102016212437A1 (de) * 2016-07-07 2018-01-11 Audi Ag Bauteil
US10427776B2 (en) * 2016-07-27 2019-10-01 The Boeing Company Sliding joint kits, systems containing the same, and related methods
CN106314759A (zh) * 2016-09-06 2017-01-11 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种飞机机翼的翼梁连接结构
CN106741830A (zh) * 2016-11-24 2017-05-31 江西洪都航空工业集团有限责任公司 一种飞机蒙皮连接面的防电偶腐蚀方法
WO2019012717A1 (ja) * 2017-07-10 2019-01-17 第一電通株式会社 締結方法及び締結装置
CN108661994A (zh) * 2018-05-08 2018-10-16 中国人民解放军海军工程大学 一种防电化学腐蚀的胶螺混合连接结构及安装方法
CN108547836A (zh) * 2018-05-14 2018-09-18 浙江众泰汽车制造有限公司 一种碳纤维复合材料与异种材料的连接结构及连接方法
US11548609B2 (en) * 2019-02-14 2023-01-10 The Boeing Company Moisture control systems and methods for controlling moisture in an aircraft
DE102019108628B4 (de) * 2019-04-02 2024-06-27 Harting Electric Stiftung & Co. Kg Steckverbindergehäuse
WO2020208802A1 (ja) * 2019-04-12 2020-10-15 株式会社Ｉｈｉエアロスペース 継手構造体及びその組立方法
GB2587391A (en) * 2019-09-26 2021-03-31 Airbus Operations Ltd Aircraft assembly
US11685508B2 (en) * 2020-04-08 2023-06-27 The Boeing Company Systems and methods for constructing a bonded structure
JP7446915B2 (ja) * 2020-05-25 2024-03-11 三菱重工業株式会社 整流構造、飛翔体及び宇宙機
CN113357236A (zh) * 2021-06-15 2021-09-07 清华大学 三维打印碳纤维复合材料与金属材料的连接结构及连接方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4221041A (en) * 1978-10-02 1980-09-09 Boeing Commercial Airplane Company Semi-tubular rivets and method of using
US4344995A (en) * 1980-09-15 1982-08-17 The Boeing Company Hybrid composite structures
US4556591A (en) * 1981-09-25 1985-12-03 The Boeing Company Conductive bonded/bolted joint seals for composite aircraft
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
US4760493A (en) * 1985-09-30 1988-07-26 The Boeing Company Lightning protection system for composite material aircraft structures
US4630168A (en) * 1985-12-16 1986-12-16 The Boeing Company Lightning protection fastener
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
US4912594A (en) * 1986-11-03 1990-03-27 The Boeing Company Integral lightning protection repair system and method for its use
GB2284031B (en) * 1987-11-27 1995-11-08 Gen Electric Composite fastener
GB8924231D0 (en) 1989-10-27 1989-12-13 British Aerospace Carbon fibre composite structures
FR2668580B1 (fr) 1990-10-30 1993-01-22 Aerospatiale Structure anti-etincelage, notamment pour aeronef.
GB9215827D0 (en) * 1992-07-24 1992-09-09 British Aerospace A lightning shield
GB9411006D0 (en) * 1994-06-02 1994-07-20 British Aerospace Method of fastening composite aircraft skins
DE19712180C2 (de) * 1997-03-22 1999-01-21 Daimler Benz Aerospace Airbus Verbindungselement für Kunststoffbauteile
AT405813B (de) * 1997-11-10 1999-11-25 Fischer Adv Components Gmbh Druckspant, insbesondere für flugzeuge
US6582172B2 (en) * 2001-08-29 2003-06-24 The United States Of America As Represented By The Secretary Of The Navy Isolated mechanical fastening system
ES2264299B1 (es) * 2003-06-06 2007-11-16 Airbus España S.L. Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica.
US8011619B2 (en) * 2004-01-05 2011-09-06 Airbus Deutschland Gmbh Insulation package arrangement for insulating the interior of an aircraft fuselage
US7347641B2 (en) * 2004-03-31 2008-03-25 The Boeing Company Methods and systems for joining structures
JP4786426B2 (ja) * 2005-10-06 2011-10-05 三菱重工業株式会社 ファスナ
WO2007142354A1 (ja) * 2006-06-09 2007-12-13 Mitsubishi Heavy Industries, Ltd. ファスナ

Also Published As

Publication number Publication date
RU2009124190A (ru) 2010-12-27
CN101631719A (zh) 2010-01-20
US20090304438A1 (en) 2009-12-10
EP2106365B1 (en) 2015-03-04
DE102007003276A1 (de) 2008-07-31
WO2008090144A1 (en) 2008-07-31
US8844868B2 (en) 2014-09-30
EP2106365A1 (en) 2009-10-07
WO2008090144B1 (en) 2008-10-09
CN101631719B (zh) 2014-06-18
CA2671917A1 (en) 2008-07-31
JP2010516538A (ja) 2010-05-20
DE102007003276B4 (de) 2013-11-28

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 6A 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: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2277 DE 26/08/2014.