WO2009124832A3 - Flugzeug mit kraftübertragungselement zwischen einem kabinenstrukturelement und einer primärstruktur - Google Patents

Flugzeug mit kraftübertragungselement zwischen einem kabinenstrukturelement und einer primärstruktur Download PDF

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Publication number
WO2009124832A3
WO2009124832A3 PCT/EP2009/053301 EP2009053301W WO2009124832A3 WO 2009124832 A3 WO2009124832 A3 WO 2009124832A3 EP 2009053301 W EP2009053301 W EP 2009053301W WO 2009124832 A3 WO2009124832 A3 WO 2009124832A3
Authority
WO
WIPO (PCT)
Prior art keywords
force transmission
aircraft
primary structure
cabin
cabin structural
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.)
Ceased
Application number
PCT/EP2009/053301
Other languages
English (en)
French (fr)
Other versions
WO2009124832A4 (de
WO2009124832A2 (de
Inventor
Ulrike Graeber
Peter Grosse-Plankermann
Martin PÄTZ
Holger Becker
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Original Assignee
Airbus Operations 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
Priority claimed from DE102008018249A external-priority patent/DE102008018249A1/de
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to EP09729619.8A priority Critical patent/EP2265490B1/de
Priority to US12/936,714 priority patent/US8430362B2/en
Publication of WO2009124832A2 publication Critical patent/WO2009124832A2/de
Publication of WO2009124832A3 publication Critical patent/WO2009124832A3/de
Publication of WO2009124832A4 publication Critical patent/WO2009124832A4/de
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • B64C1/066—Interior liners
    • 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
    • B64C1/068—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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1484—Windows
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • General Details Of Gearings (AREA)
  • Tires In General (AREA)

Abstract

Die Erfindung geht aus von einem Flugzeug mit einem Kraftübertragungselement, das ein Kabinenstruktursegment (16) mit einer Flugzeugprimärstruktur (5) lösbar verbindet und ein Kabinenlagerelement (110) sowie ein Strukturlagerelement (114) aufweist, wobei das Kabinenlagerelement (110) mit dem Kabinenstruktursegment (16) und das Strukturlagerelement (114) mit der Flugzeugprimärstruktur (5) verbunden ist. Erfindungsgemäß ist das Kraftübertragungselement (106) derart gestaltet, dass eine Kraftübertragung zwischen dem Kabinenstruktursegment (16) und der Flugzeugprimärstruktur (5) mit mindestens einem Bewegungsfreiheitsgrad erfolgen kann.
PCT/EP2009/053301 2008-04-10 2009-03-20 Flugzeug mit kraftübertragungselement zwischen einem kabinenstrukturelement und einer primärstruktur Ceased WO2009124832A2 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP09729619.8A EP2265490B1 (de) 2008-04-10 2009-03-20 Flugzeug mit kraftübertragungselement zwischen einem kabinenstrukturelement und einer primärstruktur
US12/936,714 US8430362B2 (en) 2008-04-10 2009-03-20 Aircraft having a force transmission element between a cabin structural element and a primary structure

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US12386608P 2008-04-10 2008-04-10
DE102008018249A DE102008018249A1 (de) 2006-10-12 2008-04-10 Flugzeug mit Kraftübertragungselement zwischen einem Kabinenstrukturelement und einer Primärstruktur
DE102008018249.4 2008-04-10
US61/123,866 2008-04-10

Publications (3)

Publication Number Publication Date
WO2009124832A2 WO2009124832A2 (de) 2009-10-15
WO2009124832A3 true WO2009124832A3 (de) 2010-01-21
WO2009124832A4 WO2009124832A4 (de) 2010-03-25

Family

ID=41059491

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/053301 Ceased WO2009124832A2 (de) 2008-04-10 2009-03-20 Flugzeug mit kraftübertragungselement zwischen einem kabinenstrukturelement und einer primärstruktur

Country Status (2)

Country Link
US (1) US8430362B2 (de)
WO (1) WO2009124832A2 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006048376B4 (de) * 2006-10-12 2010-04-15 Airbus Deutschland Gmbh Freitragende Kabinenstruktur
DE102008038806A1 (de) 2008-08-13 2010-02-25 Airbus Deutschland Gmbh Vormontage und Integration von Flugzeugkabinen
DE102009024157A1 (de) * 2009-06-08 2011-03-03 Airbus Operations Gmbh System und Verfahren zum Herstellen einer Fahrzeugkabine
GB201001834D0 (en) 2010-02-04 2010-03-24 Airbus Operations Ltd Bridging seal
FR2961485B1 (fr) 2010-06-22 2013-03-29 Airbus Operations Sas Dispositif de fixation de systemes pour aeronef, destine a etre notamment utilise au niveau d'un hublot
DE102011102364A1 (de) * 2011-05-24 2012-11-29 Airbus Operations Gmbh Freitragendes Kabinenstruktursegment
US8914979B2 (en) * 2011-07-21 2014-12-23 Spirit AcroSystems, Inc. System and method for assembling aircraft components
US9199715B2 (en) * 2013-10-10 2015-12-01 The Boeing Company Self-aligning fitting assemblies and systems and methods including the same
WO2015162542A2 (en) * 2014-04-25 2015-10-29 Bombardier Inc. Buffer zone for interior aircraft features
DE102014215661A1 (de) * 2014-08-07 2016-02-11 Airbus Operations Gmbh Flugzeuginnenverkleidungsbauteil, Verfahren zur Herstellung eines Flugzeuginnenverkleidungsbauteils und Flugzeugbaugruppe
US10053204B2 (en) 2015-08-31 2018-08-21 The Boeing Company Adjustable support structure for aircraft cabin ceiling
US10179638B2 (en) 2015-08-31 2019-01-15 The Boeing Company Crown raceway support (CRS) for crown integration panel (CIP)
US10011343B2 (en) 2015-08-31 2018-07-03 The Boeing Company Self-aligning structural attachment for crown integration panel (CIP)
US9758233B2 (en) 2015-08-31 2017-09-12 The Boeing Company Support system having a crown integration panel (CIP)
US10259559B2 (en) 2015-08-31 2019-04-16 The Boeing Company Remotely-activated self-centering cable latch
EP4378837B1 (de) * 2022-11-30 2025-06-11 Airbus Operations GmbH Installationssystem und verfahren zur installation einer selbsttragenden fachwerkstruktur
US12129012B2 (en) * 2023-01-25 2024-10-29 The Boeing Company Aircraft cabin seal

Citations (9)

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US2095626A (en) * 1933-04-20 1937-10-12 Sperry Gyroscope Co Inc Soundproof cabin for aircraft
US3416274A (en) * 1965-10-08 1968-12-17 Nasa Flexibly connected support and skin
US4050208A (en) * 1976-10-04 1977-09-27 The Boeing Company Aircraft interior ceiling panel assembly and attachment apparatus
EP0437870A1 (de) * 1989-12-27 1991-07-24 The Boeing Company Universale Kabinenseitenwandabdeckung eines Flugzeuges
US5201831A (en) * 1991-11-15 1993-04-13 Atr International, Inc. Aircraft interior shell
GB2287517A (en) * 1994-03-14 1995-09-20 Kenneth Barry Wilson Panel assembly system
DE19639915A1 (de) * 1996-09-27 1998-06-10 Gruenzweig & Hartmann Montage Hochtemperaturdämmsystem
US20030042363A1 (en) * 2001-09-06 2003-03-06 Marc Dussac Structural assembly of part of an aircraft and aircraft, particularly rotary-wing aircraft, comprising such a structural assembly
US20060102786A1 (en) * 2004-10-13 2006-05-18 Airbus Deutschland Gmbh Joint cover in aircraft

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JPS5647400A (en) 1979-09-26 1981-04-30 Kawasaki Heavy Ind Ltd Boxxshaped cabin structure which can be mounted and demounted to and from aircraft for freight
JPS574455A (en) 1980-06-06 1982-01-11 Tenryu Industries Box body with holding rail
US4799631A (en) * 1987-02-18 1989-01-24 Atr International, Inc. Aircraft shell module
US5687929A (en) * 1995-06-29 1997-11-18 Hexcel Corporation Extensions for storage bins
US6158690A (en) * 1998-10-30 2000-12-12 Sikorsky Aircraft Corporation Cabin interior panel system for reducing noise transmission in an aircraft
RU2191716C2 (ru) 1999-04-27 2002-10-27 Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М.Бериева Салон летательного аппарата
JP4444422B2 (ja) 1999-12-15 2010-03-31 近畿車輌株式会社 鉄道車両の内妻仕切等の取付構造
US6536710B1 (en) * 2002-02-06 2003-03-25 The Boeing Company Overhead lattice support structure
DE10339507B4 (de) 2003-07-18 2007-04-26 Telair International Gmbh Frachtmodul
US20050044712A1 (en) 2003-08-28 2005-03-03 Gideon David E. Sidewall panel integrated with insulation and air ducts
US7380752B2 (en) 2003-10-17 2008-06-03 The Boeing Company Aircraft interior architecture
US7252267B2 (en) * 2003-10-17 2007-08-07 The Boeing Company Aircraft archway architecture
JP4324446B2 (ja) 2003-10-27 2009-09-02 東急車輛製造株式会社 車両用艤装構造
US6848654B1 (en) * 2004-01-09 2005-02-01 The Boeing Company Modular offset aisle overhead crew rest
FR2869289B1 (fr) 2004-04-27 2007-07-13 Eads Sogerma Services Sa Amenagement interieur des parois du fuselage d'un aeronef.
US7629026B2 (en) 2004-09-03 2009-12-08 Eastman Kodak Company Thermally controlled fluidic self-assembly
JP3734490B2 (ja) 2004-12-06 2006-01-11 株式会社日立製作所 鉄道車両用肩部内装パネル
DE102005023886A1 (de) 2005-05-24 2006-12-07 Airbus Deutschland Gmbh Flugzeugrumpf-Montagekonzept
GB0512541D0 (en) 2005-06-20 2005-07-27 James Park Associates Ltd Aircraft interior module
DE102006048376B4 (de) * 2006-10-12 2010-04-15 Airbus Deutschland Gmbh Freitragende Kabinenstruktur
DE102009024157A1 (de) * 2009-06-08 2011-03-03 Airbus Operations Gmbh System und Verfahren zum Herstellen einer Fahrzeugkabine

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2095626A (en) * 1933-04-20 1937-10-12 Sperry Gyroscope Co Inc Soundproof cabin for aircraft
US3416274A (en) * 1965-10-08 1968-12-17 Nasa Flexibly connected support and skin
US4050208A (en) * 1976-10-04 1977-09-27 The Boeing Company Aircraft interior ceiling panel assembly and attachment apparatus
EP0437870A1 (de) * 1989-12-27 1991-07-24 The Boeing Company Universale Kabinenseitenwandabdeckung eines Flugzeuges
US5201831A (en) * 1991-11-15 1993-04-13 Atr International, Inc. Aircraft interior shell
GB2287517A (en) * 1994-03-14 1995-09-20 Kenneth Barry Wilson Panel assembly system
DE19639915A1 (de) * 1996-09-27 1998-06-10 Gruenzweig & Hartmann Montage Hochtemperaturdämmsystem
US20030042363A1 (en) * 2001-09-06 2003-03-06 Marc Dussac Structural assembly of part of an aircraft and aircraft, particularly rotary-wing aircraft, comprising such a structural assembly
US20060102786A1 (en) * 2004-10-13 2006-05-18 Airbus Deutschland Gmbh Joint cover in aircraft

Also Published As

Publication number Publication date
WO2009124832A4 (de) 2010-03-25
US20110133027A1 (en) 2011-06-09
US8430362B2 (en) 2013-04-30
WO2009124832A2 (de) 2009-10-15

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