ATE510765T1 - Leitungssystemanordnung in einem einen rumpf aufweisenden luft- oder raumfahrzeug - Google Patents

Leitungssystemanordnung in einem einen rumpf aufweisenden luft- oder raumfahrzeug

Info

Publication number
ATE510765T1
ATE510765T1 AT07729680T AT07729680T ATE510765T1 AT E510765 T1 ATE510765 T1 AT E510765T1 AT 07729680 T AT07729680 T AT 07729680T AT 07729680 T AT07729680 T AT 07729680T AT E510765 T1 ATE510765 T1 AT E510765T1
Authority
AT
Austria
Prior art keywords
fuselage
region
fuse
aircraft
pipe system
Prior art date
Application number
AT07729680T
Other languages
English (en)
Inventor
Hans-Georg Laue
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
Application filed by Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Application granted granted Critical
Publication of ATE510765T1 publication Critical patent/ATE510765T1/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
    • B64C1/06—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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin 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
    • 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
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1446—Inspection hatches
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
    • H02G3/02—Details
    • H02G3/04—Protective tubing or conduits, e.g. cable ladders or cable troughs
    • H02G3/0406—Details thereof
    • H02G3/0418—Covers or lids; Their fastenings
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
    • H02G3/02—Details
    • H02G3/04—Protective tubing or conduits, e.g. cable ladders or cable troughs
    • H02G3/0437—Channels

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structural Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Remote Sensing (AREA)
  • Casings For Electric Apparatus (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Protection Of Pipes Against Damage, Friction, And Corrosion (AREA)
  • Cable Accessories (AREA)
  • Connection Of Plates (AREA)
  • Pipeline Systems (AREA)
AT07729680T 2006-05-31 2007-05-30 Leitungssystemanordnung in einem einen rumpf aufweisenden luft- oder raumfahrzeug ATE510765T1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US80956206P 2006-05-31 2006-05-31
DE102006025388A DE102006025388B4 (de) 2006-05-31 2006-05-31 Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug
PCT/EP2007/055267 WO2007138082A1 (en) 2006-05-31 2007-05-30 Line system arrangement in an aircraft or spacecraft having a fuselage

Publications (1)

Publication Number Publication Date
ATE510765T1 true ATE510765T1 (de) 2011-06-15

Family

ID=38650369

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07729680T ATE510765T1 (de) 2006-05-31 2007-05-30 Leitungssystemanordnung in einem einen rumpf aufweisenden luft- oder raumfahrzeug

Country Status (10)

Country Link
US (1) US8490921B2 (de)
EP (1) EP2021235B1 (de)
JP (1) JP2009538776A (de)
CN (1) CN101454199A (de)
AT (1) ATE510765T1 (de)
BR (1) BRPI0711877A2 (de)
CA (1) CA2650445A1 (de)
DE (1) DE102006025388B4 (de)
RU (1) RU2446985C2 (de)
WO (1) WO2007138082A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006025388B4 (de) * 2006-05-31 2009-10-29 Airbus Deutschland Gmbh Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug
FR2944262B1 (fr) * 2009-04-14 2013-02-01 Eads Europ Aeronautic Defence Procede et dispositif de pre-assemblage d'equipements pour fuselage d'aeronef
DE102009020891B4 (de) * 2009-05-08 2015-02-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper
FI122231B (fi) * 2010-01-19 2011-10-31 U Cont Ltd Oy Eristerakennemoduuli ja eristerakenne
DE102010045588B4 (de) * 2010-09-16 2017-04-06 Airbus Operations Gmbh Rumpfsegment für ein Luftfahrzeug
CA2862409C (en) 2012-02-02 2019-04-09 Bombardier Inc. Cable retainer device and method for retaining cable in an aircraft
WO2015038042A1 (en) * 2013-09-11 2015-03-19 Saab Ab Aircraft section shafts forming a common shaft and method for assembly
EP2889212B1 (de) * 2013-12-30 2016-01-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Unterbodenstruktur mit integrierter Schale für ein Drehflügelflugzeug
FR3035072B1 (fr) * 2015-04-20 2020-09-18 Airbus Operations Sas Aeronef a architecture d'espace sous-cabine amelioree
US10926857B2 (en) * 2016-06-17 2021-02-23 The Boeing Company Pressurized bulkhead
US10992120B2 (en) * 2019-07-01 2021-04-27 The Boeing Company Sidewall closeout area assembly, system, and method for routing conductive elements in an aircraft
FR3105166A1 (fr) * 2019-12-18 2021-06-25 Airbus Operations Ensemble de conduits pour aéronef à montage en glissière
EP3865406B1 (de) 2020-02-12 2024-08-07 Airbus Operations S.L.U. Verfahren zum umbau der anordnung eines motorsteuergeräts in einem luftfahrzeug
EP4393822A1 (de) * 2022-12-30 2024-07-03 Airbus Operations GmbH Verfahren zur nutzung eines luftverteilungssystems in einem flugzeugrumpf

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE409896A (de) * 1934-06-11
GB641633A (en) 1948-03-05 1950-08-16 Fairey Aviat Co Ltd Improvements in or relating to aircraft fuselages
US2549110A (en) * 1949-05-31 1951-04-17 Northrop Aircraft Inc Panel hinge
US2965336A (en) * 1956-03-30 1960-12-20 Lissarrague Pierre Jules Device for forming an opening in a metallic panel
US2976806A (en) * 1958-03-05 1961-03-28 Gen Dynamics Corp Missile structure
FR1460060A (fr) * 1965-10-15 1966-06-17 Nord Aviation Fuselage de grande capacité et aérodyne correspondant
US4674712A (en) * 1985-01-22 1987-06-23 The Boeing Company Double-lobe fuselage composite airplane
EP0389469B1 (de) * 1987-11-17 1993-01-07 Darchem Limited Flugzeugfeuerschutzeinrichtung
US4925132A (en) * 1988-11-30 1990-05-15 The Beta Group Wide-body aircraft having efficient utilization of interior space and method therefor
FR2649665B1 (fr) * 1989-07-12 1991-11-08 Airbus Ind Fuselage de grande capacite pour avion
DE4313592C2 (de) * 1993-04-26 2000-02-17 Daimler Chrysler Aerospace Großraumflugzeug
US5816539A (en) * 1994-02-18 1998-10-06 Lockheed Martin Corporation Orbital assist module and interstage
RU2093729C1 (ru) 1994-11-29 1997-10-20 Ракетно-космическая корпорация "Энергия" им.С.П.Королева Бортовая кабельная сеть летательного аппарата
FR2782495B1 (fr) * 1998-08-19 2000-11-10 Aerospatiale Structure avant d'avion
CA2256887C (en) * 1998-12-21 2008-07-08 Indoor Air Technologies Inc. Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions
FR2807737B1 (fr) * 2000-04-14 2002-07-12 Aerospatiale Matra Airbus Dispositif de prise de pression et son procede d'implantation sur un panneau de fuselage d'aeronef
US6536710B1 (en) * 2002-02-06 2003-03-25 The Boeing Company Overhead lattice support structure
JP4490963B2 (ja) * 2003-02-15 2010-06-30 ガルフストリーム・エアロスペース・コーポレイション 航空機キャビン大気組成制御方法
WO2005012085A1 (de) * 2003-07-18 2005-02-10 Telair International Gmbh Frachtraumboden für ein flugzeug und verfahren zu dessen montage
DE10343627B4 (de) 2003-09-20 2014-03-06 Eads Deutschland Gmbh Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs
US7252267B2 (en) * 2003-10-17 2007-08-07 The Boeing Company Aircraft archway architecture
US20050166983A1 (en) * 2004-02-03 2005-08-04 Shaw James R. Flush mounted waste disposal service panel assembly
DE102006025388B4 (de) * 2006-05-31 2009-10-29 Airbus Deutschland Gmbh Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug

Also Published As

Publication number Publication date
RU2446985C2 (ru) 2012-04-10
US20090152399A1 (en) 2009-06-18
WO2007138082B1 (en) 2008-01-31
BRPI0711877A2 (pt) 2012-01-10
CN101454199A (zh) 2009-06-10
RU2008145657A (ru) 2010-07-10
US8490921B2 (en) 2013-07-23
JP2009538776A (ja) 2009-11-12
DE102006025388B4 (de) 2009-10-29
CA2650445A1 (en) 2007-12-06
DE102006025388A1 (de) 2007-12-06
EP2021235B1 (de) 2011-05-25
WO2007138082A1 (en) 2007-12-06
EP2021235A1 (de) 2009-02-11

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