JP5067890B2 - 軽量パネルの支持体取付方法 - Google Patents

軽量パネルの支持体取付方法 Download PDF

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Publication number
JP5067890B2
JP5067890B2 JP2008532840A JP2008532840A JP5067890B2 JP 5067890 B2 JP5067890 B2 JP 5067890B2 JP 2008532840 A JP2008532840 A JP 2008532840A JP 2008532840 A JP2008532840 A JP 2008532840A JP 5067890 B2 JP5067890 B2 JP 5067890B2
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JP
Japan
Prior art keywords
support
panel
fixing device
insert
flange
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
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JP2008532840A
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English (en)
Japanese (ja)
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JP2009509854A (ja
JP2009509854A5 (https=
Inventor
チプリアン．ダニーロ
Original Assignee
エアバス オペラシオン（エス．ア．エス）
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Publication of JP2009509854A publication Critical patent/JP2009509854A/ja
Publication of JP2009509854A5 publication Critical patent/JP2009509854A5/ja
Application granted granted Critical
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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)
JP2008532840A 2005-09-28 2006-09-27 軽量パネルの支持体取付方法 Expired - Fee Related JP5067890B2 (ja)

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 (3)

Publication Number Publication Date
JP2009509854A JP2009509854A (ja) 2009-03-12
JP2009509854A5 JP2009509854A5 (https=) 2012-03-22
JP5067890B2 true JP5067890B2 (ja) 2012-11-07

Family

ID=36263746

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008532840A Expired - Fee Related JP5067890B2 (ja) 2005-09-28 2006-09-27 軽量パネルの支持体取付方法

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
FR2939404B1 (fr) * 2008-12-09 2010-11-26 Airbus France Plancher modulaire pour aeronef
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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US3526072A (en) * 1968-03-29 1970-09-01 James R Campbell Load distributing system for panels incorporating honeycomb core
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FR2864940B1 (fr) * 2004-01-09 2007-03-30 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
CN101273207B (zh) 2010-09-29
EP1929159A1 (fr) 2008-06-11
WO2007036673A1 (fr) 2007-04-05
US20080302060A1 (en) 2008-12-11
BRPI0616725A2 (pt) 2012-12-25
EP1929159B1 (fr) 2009-08-26
ATE441034T1 (de) 2009-09-15
CN101273207A (zh) 2008-09-24
US8220222B2 (en) 2012-07-17

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