CN101273207B - 将轻质板体固定在支座上的固定装置 - Google Patents

将轻质板体固定在支座上的固定装置 Download PDF

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Publication number
CN101273207B
CN101273207B CN2006800357845A CN200680035784A CN101273207B CN 101273207 B CN101273207 B CN 101273207B CN 2006800357845 A CN2006800357845 A CN 2006800357845A CN 200680035784 A CN200680035784 A CN 200680035784A CN 101273207 B CN101273207 B CN 101273207B
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CN
China
Prior art keywords
fixing device
fixing
board
flange
support
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.)
Expired - Fee Related
Application number
CN2006800357845A
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English (en)
Chinese (zh)
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CN101273207A (zh
Inventor
D·奇普里安
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Airbus Operations SAS
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Airbus Operations SAS
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Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of CN101273207A publication Critical patent/CN101273207A/zh
Application granted granted Critical
Publication of CN101273207B publication Critical patent/CN101273207B/zh
Expired - Fee Related legal-status Critical Current
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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
    • B64C1/18—Floors
    • 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
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
    • 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
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
  • Electrochromic Elements, Electrophoresis, Or Variable Reflection Or Absorption Elements (AREA)
  • Fastening Of Light Sources Or Lamp Holders (AREA)
  • Led Device Packages (AREA)
  • Floor Finish (AREA)
CN2006800357845A 2005-09-28 2006-09-27 将轻质板体固定在支座上的固定装置 Expired - Fee Related CN101273207B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0552927A FR2891325B1 (fr) 2005-09-28 2005-09-28 Dispositif pour la fixation d'un panneau leger sur un support
FR0552927 2005-09-28
PCT/FR2006/050946 WO2007036673A1 (fr) 2005-09-28 2006-09-27 Dispositif pour la fixation d'un panneau leger sur un support

Publications (2)

Publication Number Publication Date
CN101273207A CN101273207A (zh) 2008-09-24
CN101273207B true CN101273207B (zh) 2010-09-29

Family

ID=36263746

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2006800357845A Expired - Fee Related CN101273207B (zh) 2005-09-28 2006-09-27 将轻质板体固定在支座上的固定装置

Country Status (11)

Country Link
US (1) US8220222B2 (https=)
EP (1) EP1929159B1 (https=)
JP (1) JP5067890B2 (https=)
CN (1) CN101273207B (https=)
AT (1) ATE441034T1 (https=)
BR (1) BRPI0616725A2 (https=)
CA (1) CA2623240C (https=)
DE (1) DE602006008809D1 (https=)
FR (1) FR2891325B1 (https=)
RU (1) RU2401949C2 (https=)
WO (1) WO2007036673A1 (https=)

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US9284036B2 (en) * 2007-12-27 2016-03-15 Airbus Operations Gmbh Floor plate for covering a floor framework in an aircraft
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US8950159B2 (en) 2008-12-23 2015-02-10 Woodwelding Ag Method of anchoring a connector, and connector
CA2747221C (en) * 2008-12-23 2017-08-22 Woodwelding Ag Method of anchoring a connector, and connector
US9175474B2 (en) 2010-02-05 2015-11-03 Textron Innovations Inc. Apparatus for attaching a member to a core-stiffened structure and a combination thereof
EP2550175A4 (en) * 2010-03-23 2015-04-01 Be Aerospace Inc PASSENGER SEAT ARRANGEMENT WITH CORRESPONDING FLOOR PANEL STRUCTURE
US8544796B2 (en) * 2010-03-23 2013-10-01 Be Aerospace, Inc. Passenger seat assembly with associated floor panel and aircraft sidewall attachment, and method
CN101906850A (zh) * 2010-07-20 2010-12-08 重庆大学 群锚专用抗剪锚栓副
AT510323B1 (de) * 2010-09-06 2012-09-15 Facc Ag Befestigungseinrichtung
DE102011018526A1 (de) * 2011-04-26 2012-10-31 Airbus Operations Gmbh Krafteinleitungsbeschlag für Leichtbaukomponenten
FR2983826B1 (fr) * 2011-12-12 2013-12-20 Airbus Operations Sas Structure avant d'avion perfectionnee a compartiment pour train d'atterrissage.
US8763753B2 (en) * 2012-02-10 2014-07-01 General Electric Company Acoustic panel and method of forming
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
FR3003233B1 (fr) * 2013-03-18 2016-05-06 Airbus Operations Sas Panneau de voilure pour aeronef
EP2818403B1 (en) * 2013-06-24 2016-02-10 Airbus Operations GmbH Locally reinforced aircraft structural component
EP2913539A1 (en) * 2014-02-28 2015-09-02 Redco NV A rivet
AT515304B1 (de) 2014-03-07 2015-08-15 Facc Ag Vorrichtung zur Verbindung eines Strukturelements sowie Strukturelement
DE102014206640A1 (de) 2014-04-07 2015-10-08 Bayerische Motoren Werke Aktiengesellschaft Kunststoffbauteil mit einem Verbindungselement
US9932831B2 (en) * 2014-05-09 2018-04-03 United Technologies Corporation High temperature compliant metallic elements for low contact stress ceramic support
US9611877B1 (en) * 2015-01-20 2017-04-04 Gerald E. Attanasio Honeycomb panel fastener
JP2016137733A (ja) * 2015-01-26 2016-08-04 三菱航空機株式会社 フロアパネル装置
US10247218B2 (en) * 2015-03-10 2019-04-02 Sikorsky Aircraft Corporation Brushing retention of threaded fastener
ES2835329T3 (es) * 2015-06-03 2021-06-22 Onguard Group Ltd Montaje de sujeción
FR3038942B1 (fr) 2015-07-17 2018-03-02 Safran Ceramics Assemblage par liaison mecanique comportant au moins une piece en materiau composite
US10309434B2 (en) * 2016-03-31 2019-06-04 The Boeing Company Thrust reverser honeycomb panel load distribution systems and methods
US9598183B1 (en) 2016-05-06 2017-03-21 Kellstrom Defense Aerospace, Inc. Aircraft wing repair systems and methods
CN106300878B (zh) * 2016-10-25 2018-11-30 株洲中车机电科技有限公司 一种直线电机感应板安装止动装置
US10836463B2 (en) * 2017-07-06 2020-11-17 The Boeing Company Aircraft floor panel floating connection system
US10919612B2 (en) 2018-03-08 2021-02-16 The Boeing Company Floor panels and flooring systems for a passenger vehicle, and methods for installation
EP3779928B1 (en) * 2019-08-13 2023-11-08 Humanetics Innovative Solutions, Inc. Coupling design for coupling simulated pelvic flesh to a pelvic support structure of a pelvis assembly of an anthropomorphic test device
FR3105778A1 (fr) 2019-12-27 2021-07-02 Airbus Structure de plancher pour aéronef à élément de recouvrement de rail soutenu par une structure alvéolaire
US20230373568A1 (en) * 2021-01-15 2023-11-23 Autoproducts Aps Flooring for a vehicle, as well as a method of mounting such flooring in a motor vehicle
US11945569B2 (en) * 2021-01-29 2024-04-02 Airbus Operations (S.A.S.) Hybrid anchor rail for aircraft floor
EP4321428B1 (de) * 2022-08-12 2026-04-29 Airbus Operations GmbH Schienensystem für eine kabine eines fahrzeugs
EP4520655A3 (en) * 2023-07-31 2025-04-02 AIRBUS Operations GmbH Aircraft floor arrangement with customizable load-bearing capabilities
US12286998B1 (en) * 2023-10-06 2025-04-29 The Boeing Company Serrated fitting
FR3159640A1 (fr) * 2024-02-28 2025-08-29 Airbus Operations Assemblage d’un panneau sandwich à une structure
CN118257766B (zh) * 2024-05-30 2024-08-30 洛阳船舶材料研究所(中国船舶集团有限公司第七二五研究所) 一种金属框架与大厚度夹心复合材料连接结构及成型方法
FR3165606A1 (fr) * 2024-08-16 2026-02-20 Segula Engineering Moyens d’assemblage structurel ou semi-structurel pour assembler structurellement ou semi-structurellement au moins deux éléments structurels et/ou semi-structurels en matériaux composites.

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US3110064A (en) * 1958-11-24 1963-11-12 Minnesota Mining & Mfg Wall securement
US4399642A (en) * 1980-07-24 1983-08-23 The Boeing Company Aircraft floor panel installation system
US5230485A (en) * 1991-01-26 1993-07-27 Deutsche Aerospace Airbus Gmbh Connector device for securing structural components to each other
CN2596090Y (zh) * 2001-09-17 2003-12-31 亚翔工程股份有限公司 蜂巢板接合结构改进
FR2864940A1 (fr) * 2004-01-09 2005-07-15 Airbus France Rail de fixation pour aeronef

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US3765465A (en) * 1972-01-05 1973-10-16 Deutsch Fastener Corp Retractable captive fastener
US4481702A (en) * 1982-09-30 1984-11-13 The Boeing Company Method of assembling threaded insert bushing within a working material
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US3110064A (en) * 1958-11-24 1963-11-12 Minnesota Mining & Mfg Wall securement
US4399642A (en) * 1980-07-24 1983-08-23 The Boeing Company Aircraft floor panel installation system
US5230485A (en) * 1991-01-26 1993-07-27 Deutsche Aerospace Airbus Gmbh Connector device for securing structural components to each other
CN2596090Y (zh) * 2001-09-17 2003-12-31 亚翔工程股份有限公司 蜂巢板接合结构改进
FR2864940A1 (fr) * 2004-01-09 2005-07-15 Airbus France Rail de fixation pour aeronef

Also Published As

Publication number Publication date
RU2401949C2 (ru) 2010-10-20
DE602006008809D1 (de) 2009-10-08
FR2891325A1 (fr) 2007-03-30
RU2008116617A (ru) 2009-11-10
CA2623240C (fr) 2013-11-26
CA2623240A1 (fr) 2007-04-05
JP2009509854A (ja) 2009-03-12
FR2891325B1 (fr) 2007-10-26
EP1929159A1 (fr) 2008-06-11
WO2007036673A1 (fr) 2007-04-05
US20080302060A1 (en) 2008-12-11
BRPI0616725A2 (pt) 2012-12-25
JP5067890B2 (ja) 2012-11-07
EP1929159B1 (fr) 2009-08-26
ATE441034T1 (de) 2009-09-15
CN101273207A (zh) 2008-09-24
US8220222B2 (en) 2012-07-17

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C06 Publication
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C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee

Owner name: AIRBUS OPERATIONS S.A.S.

Free format text: FORMER NAME: AIRBUS FRANCE

CP01 Change in the name or title of a patent holder

Address after: France Toulouse

Patentee after: Airbus Operations S.A.S.

Address before: France Toulouse

Patentee before: Airbus France

Address after: France Toulouse

Patentee after: Airbus France

Address before: France Toulouse

Patentee before: Airbus France

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100929

Termination date: 20200927