ATE531618T1 - Rumpfstruktur - Google Patents

Rumpfstruktur

Info

Publication number
ATE531618T1
ATE531618T1 AT07729698T AT07729698T ATE531618T1 AT E531618 T1 ATE531618 T1 AT E531618T1 AT 07729698 T AT07729698 T AT 07729698T AT 07729698 T AT07729698 T AT 07729698T AT E531618 T1 ATE531618 T1 AT E531618T1
Authority
AT
Austria
Prior art keywords
inner shell
fuselage
window
fits
hull structure
Prior art date
Application number
AT07729698T
Other languages
English (en)
Inventor
Guenter Pahl
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 ATE531618T1 publication Critical patent/ATE531618T1/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
    • B64C1/068—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
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Body Structure For Vehicles (AREA)
AT07729698T 2006-06-02 2007-05-31 Rumpfstruktur ATE531618T1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US81024706P 2006-06-02 2006-06-02
DE102006025930A DE102006025930B4 (de) 2006-06-02 2006-06-02 Rumpfstruktur und Verfahren zur Herstellung einer Rumpfstruktur
PCT/EP2007/055286 WO2007141176A1 (en) 2006-06-02 2007-05-31 Fuselage structure and method for the production of a fuselage structure

Publications (1)

Publication Number Publication Date
ATE531618T1 true ATE531618T1 (de) 2011-11-15

Family

ID=38663623

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07729698T ATE531618T1 (de) 2006-06-02 2007-05-31 Rumpfstruktur

Country Status (10)

Country Link
US (1) US8444088B2 (de)
EP (1) EP2024228B1 (de)
JP (1) JP2009538778A (de)
CN (1) CN101460358B (de)
AT (1) ATE531618T1 (de)
BR (1) BRPI0712309A2 (de)
CA (1) CA2649339A1 (de)
DE (1) DE102006025930B4 (de)
RU (1) RU2434782C2 (de)
WO (1) WO2007141176A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006025930B4 (de) * 2006-06-02 2008-09-11 Airbus Deutschland Gmbh Rumpfstruktur und Verfahren zur Herstellung einer Rumpfstruktur
FR2911112B1 (fr) * 2007-01-05 2009-02-13 Airbus France Sas Section de fuselage pour aeronef et aeronef comprenant une telle section
DE102008007545A1 (de) * 2008-02-05 2009-08-27 Airbus Deutschland Gmbh Lasttragendes und schadenstolerantes Laminatflugzeugfenster
DE102008056702B4 (de) * 2008-11-11 2014-04-03 Airbus Operations Gmbh Flugzeugfenster
CN102481971B (zh) * 2009-10-08 2014-12-31 三菱重工业株式会社 复合材料构造体、具备该构造体的航空器主翼及航空器机身
DE102009060876A1 (de) * 2009-12-30 2011-07-14 IMA Materialforschung und Anwendungstechnik GmbH, 01109 Luft- oder Raumfahrzeughülle
US8616500B2 (en) 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
RU2475412C1 (ru) * 2011-08-29 2013-02-20 Общество С Ограниченной Ответственностью "Научно-Инженерная Компания" (Ооо "Ник") Оболочка отсека герметичного фюзеляжа магистрального самолета из полимерного композиционного материала и способ ее изготовления
US8939406B2 (en) * 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
RU190988U1 (ru) * 2019-04-09 2019-07-18 Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Узел крепления элементов конструкции космического аппарата

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2327636A (en) * 1943-08-24 Aircraft fuselage construction
US1441984A (en) * 1918-09-20 1923-01-09 Dayton Wright Company Fuselage
US2203174A (en) * 1936-12-28 1940-06-04 Messerschmitt Boelkow Blohm Vehicle window
GB620863A (en) * 1947-01-27 1949-03-31 Henrique Emil Mendelssohn Improvements in or relating to aircraft
US2613402A (en) * 1949-10-13 1952-10-14 Saunders Roe Ltd Window for pressurized chambers
US2659686A (en) * 1950-02-13 1953-11-17 Libbey Owens Ford Glass Co Laminated glass structure
DE1252533B (de) * 1965-11-10
FR1497214A (fr) * 1966-10-21 1967-10-06 Bande à fenêtres continue pour fuselages d'avions
US4035536A (en) * 1975-03-03 1977-07-12 Mcdonnell Douglas Corporation Sandwich panel core
US4450661A (en) * 1981-09-30 1984-05-29 The Boeing Company Composite structures window belt and method of making
SU1663894A1 (ru) 1989-08-29 1995-09-27 Московский авиационный технологический институт им.К.Э.Циолковского Многоразовый двухмодульный космический корабль
AU6250999A (en) * 1998-10-06 2000-04-26 Williams International Company, L.L.C. Aircraft window
DE19929471C1 (de) * 1999-06-26 2001-01-18 Eads Airbus Gmbh Verfahren und Vorrichtung zur Herstellung eines dreidimensionalen Großbauteiles
ES2249223T3 (es) * 1999-12-16 2006-04-01 Airbus Deutschland Gmbh Componente estructural.
RU2197410C2 (ru) 2000-11-10 2003-01-27 Закрытое акционерное общество "Кристалл" Фюзеляж
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
US6736352B2 (en) * 2002-06-25 2004-05-18 The Boeing Company Aircraft windows and associated methods for installation
US7300693B2 (en) * 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7802413B2 (en) * 2004-10-04 2010-09-28 The Boeing Company Apparatus and methods for reinforcing a structural panel
US7530531B2 (en) * 2004-10-04 2009-05-12 The Boeing Company Apparatus and methods for installing an aircraft window panel
US7823832B2 (en) * 2004-10-04 2010-11-02 The Boeing Company Injection-molded window panel and related methods
US7438263B2 (en) * 2005-09-09 2008-10-21 The Boeing Company Optimal aircraft window shape for noise control
US8292226B2 (en) * 2005-11-15 2012-10-23 The Boeing Company Weight-optimizing internally pressurized composite-body aircraft fuselages having near-elliptical cross sections
DE102006025930B4 (de) * 2006-06-02 2008-09-11 Airbus Deutschland Gmbh Rumpfstruktur und Verfahren zur Herstellung einer Rumpfstruktur
US9611029B2 (en) * 2006-10-11 2017-04-04 The Boeing Company Floor beam support assembly, system, and associated method
FR2911112B1 (fr) * 2007-01-05 2009-02-13 Airbus France Sas Section de fuselage pour aeronef et aeronef comprenant une telle section
DE102007032233B4 (de) * 2007-07-11 2014-07-10 Airbus Operations Gmbh Installationssystem für ein Flugzeug
DE102008012282A1 (de) * 2008-03-03 2009-09-17 Airbus Deutschland Gmbh Rumpfstruktur für Flugzeug

Also Published As

Publication number Publication date
RU2008146845A (ru) 2010-07-20
RU2434782C2 (ru) 2011-11-27
CA2649339A1 (en) 2007-12-13
CN101460358B (zh) 2012-06-06
US20090166471A1 (en) 2009-07-02
US8444088B2 (en) 2013-05-21
CN101460358A (zh) 2009-06-17
DE102006025930B4 (de) 2008-09-11
JP2009538778A (ja) 2009-11-12
EP2024228A1 (de) 2009-02-18
EP2024228B1 (de) 2011-11-02
BRPI0712309A2 (pt) 2012-01-17
WO2007141176A1 (en) 2007-12-13
DE102006025930A1 (de) 2007-12-13

Similar Documents

Publication Publication Date Title
ATE531618T1 (de) Rumpfstruktur
DE602007011896D1 (de) Ausfallsichere steuerflächentropfenverbindung
BRPI0717778A2 (pt) Estrutura interior de cabina autossustentada com elementos de instalação integrados
BRPI0719612A2 (pt) "parte dianteira de fuselagem de aeronave e aeronave"
DE602005001782D1 (de) Flugzeugsitzschiene und deren Fertigungsverfahren
BRPI0715713A2 (pt) elemento de armaÇço, compartimento de bagagem de mço, e, mÉtodo para a instalaÇço de um compartimento de bagagem de mço em uma aeronave
WO2008007135A3 (en) A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof
BRPI0818132A8 (pt) Sistema de atuação para dispositivo de alta sustentação de bordo de ataque
EP1995171A3 (de) Vorrichtung und Verfahren zur Steuerung der Strömung mittels Plasma an der Hinterkante einer Tragfläche
WO2008144228A3 (en) Engine anticipation for rotary wing aircraft
EP1836089A4 (de) Schallabsorptionssystem für ein flugzeug-flugwerk
WO2006025963A3 (en) Method, system and storage medium which includes instruction for analyzing anatomical structures
FR2885596B1 (fr) Procede et systeme anti-crash, atterrisseur et aeronef
WO2009026270A3 (en) Hmm-based bilingual (mandarin-english) tts techniques
NO20064266L (no) System for fremgangsmate vedrorende komponentassosiasjonssporer
EP1904564A4 (de) System und verfahren für verbesserte drehflüglerleistung mit innen-/aussenlasten
BRPI0810866A2 (pt) Estrutura de compósito que compreende uma longarina com uma placa de apoio embutida dentro do rebaixo de um painel e método para transmitir forças.
DE602007009720D1 (de) Flugzeugflügel
GB2444694A (en) Window assembly retaining system
WO2007079273A3 (en) Method and device for resilient seal system
BRPI0913289A2 (pt) método para refrigerar um dispositivo eletrônico em uma aeronave, dispositivo de refrigeração de aeronave, e, sistema de refrigeração de componente eletrônico de aeronave redundante.
FR2976913B1 (fr) Dispositif combine de balise de secours et enregistreur de vol pour aeronef et aeronef equipe d'un tel dispositif
WO2009025193A1 (ja) 情報共有システム、情報共有方法、および情報共有プログラム
EP1904367A4 (de) Abstimmbares schalldämpfungssystem für eine flugzeugkabine
WO2008096088A3 (fr) Procede d'assemblage d'un hublot pour aeronef