ATE441034T1 - Vorrichtung zur befestigung einer leichten platte an einem träger - Google Patents

Vorrichtung zur befestigung einer leichten platte an einem träger

Info

Publication number
ATE441034T1
ATE441034T1 AT06831233T AT06831233T ATE441034T1 AT E441034 T1 ATE441034 T1 AT E441034T1 AT 06831233 T AT06831233 T AT 06831233T AT 06831233 T AT06831233 T AT 06831233T AT E441034 T1 ATE441034 T1 AT E441034T1
Authority
AT
Austria
Prior art keywords
support
panel
washer
fastening
light plate
Prior art date
Application number
AT06831233T
Other languages
English (en)
Inventor
Danilo Ciprian
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE441034T1 publication Critical patent/ATE441034T1/de

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
    • B64C1/18—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)
AT06831233T 2005-09-28 2006-09-27 Vorrichtung zur befestigung einer leichten platte an einem träger ATE441034T1 (de)

Applications Claiming Priority (2)

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
PCT/FR2006/050946 WO2007036673A1 (fr) 2005-09-28 2006-09-27 Dispositif pour la fixation d'un panneau leger sur un support

Publications (1)

Publication Number Publication Date
ATE441034T1 true ATE441034T1 (de) 2009-09-15

Family

ID=36263746

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06831233T ATE441034T1 (de) 2005-09-28 2006-09-27 Vorrichtung zur befestigung einer leichten platte an einem träger

Country Status (11)

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

Families Citing this family (34)

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US20070294954A1 (en) * 2006-06-22 2007-12-27 Barrett Jeffrey L Prefabricated bathroom assembly and methods of its manufacture and installation
DE102007018753B4 (de) 2007-04-20 2012-11-08 Airbus Operations Gmbh Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten
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
WO2010072009A1 (en) * 2008-12-23 2010-07-01 Woodwelding Ag Method of anchoring a connector, and connector
EP2531665B1 (de) 2010-02-05 2015-08-26 Bell Helicopter Textron Inc. Vorrichtung zur befestigung eines elements an eine kernversteifte wabenförmige struktur
JP2013522123A (ja) 2010-03-23 2013-06-13 ビー イー エアロスペイス，インク． 乗客座席組立体および関連付けられた床板構造体
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 (de) * 2013-06-24 2016-02-10 Airbus Operations GmbH Lokal verstärktes Flugzeugstrukturbauteil
EP2913539A1 (de) * 2014-02-28 2015-09-02 Redco NV Niete
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
US10370844B2 (en) * 2015-06-03 2019-08-06 Onguard Group Limited Securing assembly
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
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
WO2022152613A1 (en) * 2021-01-15 2022-07-21 Vbi Minibus & Components Aps Flooring for a vehicle, as well as a method of mounting such flooring in a motor vehicle
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

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US3110064A (en) * 1958-11-24 1963-11-12 Minnesota Mining & Mfg Wall securement
US3137887A (en) * 1962-06-15 1964-06-23 Republic Aviat Corp Bushing
US3296765A (en) * 1964-06-29 1967-01-10 Rohe Mechanical sandwich panel spacer with improved torque resistant anchorage
US3526072A (en) * 1968-03-29 1970-09-01 James R Campbell Load distributing system for panels incorporating honeycomb core
US3765465A (en) * 1972-01-05 1973-10-16 Deutsch Fastener Corp Retractable captive fastener
US4399642A (en) * 1980-07-24 1983-08-23 The Boeing Company Aircraft floor panel installation system
US4481702A (en) * 1982-09-30 1984-11-13 The Boeing Company Method of assembling threaded insert bushing within a working material
WO1984003130A1 (en) * 1983-02-07 1984-08-16 Boeing Co Unitary fastener insert for structural sandwich panels
JPS60180811U (ja) * 1984-05-11 1985-11-30 タキゲン製造株式会社 皿ビスによる固着構造
DE3433375A1 (de) * 1984-09-12 1986-03-20 KSA Dichtsysteme GmbH & Co KG, 7143 Vaihingen Dicht- und sicherungseinrichtung
JPS6255710U (de) * 1985-09-27 1987-04-07
GB2212237B (en) * 1987-11-11 1991-08-21 Avdel Ltd Bush
DE3831523A1 (de) * 1988-09-16 1990-03-22 Koenig Verbindungstech Ag Verfahren zum dichten verschliessen einer bohrung
DE4102273C2 (de) * 1991-01-26 1993-12-09 Deutsche Aerospace Airbus Anschlußelement
JPH09166123A (ja) * 1995-12-12 1997-06-24 Japan Drive-It Co Ltd 固着具
US6055790A (en) * 1998-05-18 2000-05-02 The United States Of America As Represented By The Secretary Of The Air Force Thermal conductive insert for sandwich structures
JP4390322B2 (ja) * 1999-08-17 2009-12-24 株式会社Ｉｈｉエアロスペース ハニカムパネル構造体
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
DE10360809A1 (de) * 2003-12-19 2005-07-28 Airbus Deutschland Gmbh Sitzschiene
FR2864940B1 (fr) * 2004-01-09 2007-03-30 Airbus France Rail de fixation pour aeronef

Also Published As

Publication number Publication date
CN101273207B (zh) 2010-09-29
JP5067890B2 (ja) 2012-11-07
JP2009509854A (ja) 2009-03-12
EP1929159A1 (de) 2008-06-11
RU2008116617A (ru) 2009-11-10
US20080302060A1 (en) 2008-12-11
WO2007036673A1 (fr) 2007-04-05
FR2891325A1 (fr) 2007-03-30
CA2623240A1 (fr) 2007-04-05
US8220222B2 (en) 2012-07-17
EP1929159B1 (de) 2009-08-26
FR2891325B1 (fr) 2007-10-26
CN101273207A (zh) 2008-09-24
CA2623240C (fr) 2013-11-26
RU2401949C2 (ru) 2010-10-20
BRPI0616725A2 (pt) 2012-12-25
DE602006008809D1 (de) 2009-10-08

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties