ATE352486T1 - Flugzeugdeck - Google Patents

Flugzeugdeck

Info

Publication number
ATE352486T1
ATE352486T1 AT05106146T AT05106146T ATE352486T1 AT E352486 T1 ATE352486 T1 AT E352486T1 AT 05106146 T AT05106146 T AT 05106146T AT 05106146 T AT05106146 T AT 05106146T AT E352486 T1 ATE352486 T1 AT E352486T1
Authority
AT
Austria
Prior art keywords
fuselage
members
series
cross
stop collar
Prior art date
Application number
AT05106146T
Other languages
English (en)
Inventor
Alban Vetillard
Emmanuel Parro
Frederic Leclerc
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 ATE352486T1 publication Critical patent/ATE352486T1/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Radio Relay Systems (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
  • Pallets (AREA)
  • Table Devices Or Equipment (AREA)
  • Golf Clubs (AREA)
  • Vehicle Body Suspensions (AREA)
AT05106146T 2004-07-08 2005-07-06 Flugzeugdeck ATE352486T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0407628A FR2872781B1 (fr) 2004-07-08 2004-07-08 Plancher pour aeronef

Publications (1)

Publication Number Publication Date
ATE352486T1 true ATE352486T1 (de) 2007-02-15

Family

ID=34946733

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05106146T ATE352486T1 (de) 2004-07-08 2005-07-06 Flugzeugdeck

Country Status (7)

Country Link
US (1) US7191982B2 (de)
EP (1) EP1614624B1 (de)
AT (1) ATE352486T1 (de)
CA (1) CA2511864C (de)
DE (1) DE602005000493T2 (de)
ES (1) ES2281057T3 (de)
FR (1) FR2872781B1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US8691137B2 (en) * 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US9102103B2 (en) * 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
US8491745B2 (en) * 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US7807005B2 (en) 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US7775478B2 (en) * 2006-09-29 2010-08-17 The Boeing Company Floor beam assembly, system, and associated method
US9611029B2 (en) * 2006-10-11 2017-04-04 The Boeing Company Floor beam support assembly, system, and associated method
FR2913400B1 (fr) * 2007-03-07 2009-11-20 Airbus France Plancher d'aeronef et fuselage muni d'un tel plancher.
DE102008007838B4 (de) * 2008-02-07 2013-07-18 Airbus Operations Gmbh Fußbodensystem für eine Rumpfzelle eines Flugzeugs
US8047469B2 (en) * 2008-03-01 2011-11-01 The Boeing Company Airframe attachment fitting
FR2930521B1 (fr) * 2008-04-29 2010-09-03 Airbus France Module de plancher d'aeronef, structure et procede de fixation d'un tel module, aeronef comprenant ceux-ci
FR2933065B1 (fr) * 2008-06-30 2011-08-26 Airbus France Procede d'assemblage d'un plancher dans une structure de coque prealablement constituee d'un troncon de fuselage d'aeronef
US8181422B2 (en) * 2008-12-23 2012-05-22 Spirit Aerosystems, Inc. Energy-absorbing structural composite element
DE102009015858B4 (de) * 2009-04-01 2015-01-08 Airbus Operations Gmbh Verbindung eines Querträgers mit einem Strukturbauteil
FR2946008B1 (fr) * 2009-05-28 2012-12-28 Airbus France Aeronef comprenant des traverses de support de plancher
FR2947525B1 (fr) * 2009-07-02 2011-09-02 Airbus Operations Sas Plancher d'aeronef a encombrement optimise
US10821653B2 (en) * 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
DE102010038695B4 (de) * 2010-07-30 2012-05-03 Airbus Operations Gmbh Vorrichtung zur Halterung von Steckverbindern
US9016625B2 (en) 2011-05-11 2015-04-28 The Boeing Company Reconfigurable floorboard system
US9926066B2 (en) * 2015-10-14 2018-03-27 The Boeing Company Corner tension fitting
FR3082823A1 (fr) * 2018-06-25 2019-12-27 Airbus Operations Module pour aeronef presentant une conception facilitant son assemblage dans un espace interieur defini par le fuselage de l'aeronef
US11511863B2 (en) * 2020-05-10 2022-11-29 The Boeing Company Sliding joint for load alleviation
US11702205B2 (en) 2020-06-12 2023-07-18 The Boeing Company Monument having attachment system with corner bracket fitting
USD944079S1 (en) * 2020-06-12 2022-02-22 The Boeing Company Corner bracket fitting for use in an attachment system
EP4180322B1 (de) * 2021-11-15 2025-04-30 Airbus Operations (S.A.S.) Flugzeug mit boden umfassend mindestens einem gelenkigen beweglichen bodenteil
EP4197918B1 (de) * 2021-12-16 2024-08-21 Airbus Operations (S.A.S.) Flexibles eckstück zur unterstützung einer verbindung zwischen mindestens drei wänden mindestens eines flugzeuggehäuses

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB531357A (en) * 1938-08-26 1941-01-02 Dornier Werke Gmbh Improvements in or relating to aircraft fusilages
FR1313327A (fr) * 1961-11-17 1962-12-28 Nord Aviation Instrument de bord pour le contrôle d'une entrée d'air de forme variable pour un moteur supersonique
US3155348A (en) * 1962-06-14 1964-11-03 Aviation Louis Breguet Sa Aircraft fuselage
FR1460060A (fr) * 1965-10-15 1966-06-17 Nord Aviation Fuselage de grande capacité et aérodyne correspondant
US3347496A (en) * 1966-05-03 1967-10-17 Ryan Aeronautical Co Engine air inlet system for supersonic v/stol aircraft
GB1458033A (en) * 1973-05-31 1976-12-08 British Aircraft Corp Ltd Air intakes for jet propulsion engines
US4674712A (en) * 1985-01-22 1987-06-23 The Boeing Company Double-lobe fuselage composite airplane
FR2635075B1 (fr) * 1988-08-04 1994-09-23 Onera (Off Nat Aerospatiale) Entree d'air supersonique bidimensionnelle et asymetrique pour l'air de combustion d'un moteur d'aeronef
FR2649665B1 (fr) * 1989-07-12 1991-11-08 Airbus Ind Fuselage de grande capacite pour avion
US5222694A (en) * 1992-08-03 1993-06-29 Atr International, Inc. Aircraft interior panel noise dampening support brackets
US5560102A (en) * 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly
US6793175B1 (en) * 1999-08-25 2004-09-21 The Boeing Company Supersonic external-compression diffuser and method for designing same

Also Published As

Publication number Publication date
US7191982B2 (en) 2007-03-20
ES2281057T3 (es) 2007-09-16
CA2511864C (en) 2013-12-17
EP1614624B1 (de) 2007-01-24
DE602005000493T2 (de) 2007-10-31
DE602005000493D1 (de) 2007-03-15
EP1614624A1 (de) 2006-01-11
CA2511864A1 (en) 2006-01-08
FR2872781A1 (fr) 2006-01-13
US20060226288A1 (en) 2006-10-12
FR2872781B1 (fr) 2007-10-05

Similar Documents

Publication Publication Date Title
ATE352486T1 (de) Flugzeugdeck
ATE409158T1 (de) Flugzeugdeck
DE602004001319D1 (de) Aufhängung eines Triebwerks unter einer Flugzeugflügel
FR2874370B1 (fr) Aile d'avion
FR2873347B1 (fr) Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
DE602007007771D1 (de) Flügelelement-verbundgelenk
BR0203556B1 (pt) aeronave com carenagem ventral e junta para esta.
FR2878229B1 (fr) Systeme de fixation d'un mat de moteur a l'aile d'un aeronef
FR2848661B1 (fr) Equipement anticollision terrain embarque a bord d'aeronef avec aide au retour en vol normal
WO2007096624A3 (en) Control surface failsafe drop link
FR2883256B1 (fr) Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
BR0102605A (pt) Componentes estrutural para um avião
FR2864030B1 (fr) Aeronef convertible pourvu de deux "tilt fan" de part et d'autre du fuselage et d'un troisieme "tilt fan" agence sur la queue de l'aeronef
RU2009142460A (ru) Секция крыло-фюзеляж летательного аппарата
ATE527170T1 (de) Start- und landesystem für unbemanntes fluggerät
RU2004116113A (ru) Переднее крепежное устройство для авиационного двигателя
ATE398071T1 (de) Flugzeuginneneinrichtung
DE602005013598D1 (de) Aufbau von Flugzeugrumpfpaneelen
ATE393730T1 (de) Flugzeug mit flügel-rumpf-verkleidung
WO2011071939A3 (en) Wing spar splice joint
FR2880868B1 (fr) Procede de locomotion aerienne et aeronef polyvalent a aile(s) gonflable(s) utilisant ce procede
ATE416969T1 (de) Seitenleitwerksanschluss
RU2007107932A (ru) Усиленная дверь
ATE338680T1 (de) Flugzeugtür und ein flugzeug mit einer solchen tür
DE602004005602D1 (de) Starrer flügel mit variablem auftrieb aufgrund des ausklappens eines flexiblen flügels

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties