BRPI0616725A2 - dispositivo para a fixaÇço de um painel leve, e, veÍculo de transporte de passageiros - Google Patents

dispositivo para a fixaÇço de um painel leve, e, veÍculo de transporte de passageiros Download PDF

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Publication number
BRPI0616725A2
BRPI0616725A2 BRPI0616725-0A BRPI0616725A BRPI0616725A2 BR PI0616725 A2 BRPI0616725 A2 BR PI0616725A2 BR PI0616725 A BRPI0616725 A BR PI0616725A BR PI0616725 A2 BRPI0616725 A2 BR PI0616725A2
Authority
BR
Brazil
Prior art keywords
panel
piece
flange
insert
support
Prior art date
Application number
BRPI0616725-0A
Other languages
English (en)
Portuguese (pt)
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
Publication of BRPI0616725A2 publication Critical patent/BRPI0616725A2/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
    • B64C1/18—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)
BRPI0616725-0A 2005-09-28 2006-09-27 dispositivo para a fixaÇço de um painel leve, e, veÍculo de transporte de passageiros BRPI0616725A2 (pt)

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 (1)

Publication Number Publication Date
BRPI0616725A2 true BRPI0616725A2 (pt) 2012-12-25

Family

ID=36263746

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0616725-0A BRPI0616725A2 (pt) 2005-09-28 2006-09-27 dispositivo para a fixaÇço de um painel leve, e, veÍculo de transporte de passageiros

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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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
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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
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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Legal Events

Date Code Title Description
B06G Technical and formal requirements: other requirements [chapter 6.7 patent gazette]

Free format text: SOLICITA-SE A REGULARIZACAO DA PROCURACAO, UMA VEZ QUE BASEADO NO ARTIGO 216 1O DA LPI, O DOCUMENTO DE PROCURACAO DEVE SER APRESENTADO NO ORIGINAL, TRASLADO OU FOTOCOPIA AUTENTICADA.

B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

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

Free format text: REFERENTE A 12A 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 2481 DE 24-07-2018 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.