DE10343627A1 - Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs - Google Patents

Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs Download PDF

Info

Publication number
DE10343627A1
DE10343627A1 DE2003143627 DE10343627A DE10343627A1 DE 10343627 A1 DE10343627 A1 DE 10343627A1 DE 2003143627 DE2003143627 DE 2003143627 DE 10343627 A DE10343627 A DE 10343627A DE 10343627 A1 DE10343627 A1 DE 10343627A1
Authority
DE
Germany
Prior art keywords
aircraft
closure element
hinge
area
outer contour
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.)
Granted
Application number
DE2003143627
Other languages
English (en)
Other versions
DE10343627B4 (de
Inventor
Juan Perez-Sanchez
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 Defence and Space GmbH
Original Assignee
EADS Deutschland 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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Priority to DE2003143627 priority Critical patent/DE10343627B4/de
Priority to FR0409718A priority patent/FR2859975B1/fr
Priority to US10/943,251 priority patent/US7503523B2/en
Priority to GB0420858A priority patent/GB2406320B/en
Publication of DE10343627A1 publication Critical patent/DE10343627A1/de
Priority to US12/340,141 priority patent/US7909289B2/en
Application granted granted Critical
Publication of DE10343627B4 publication Critical patent/DE10343627B4/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C1/14—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
    • 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
    • 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
    • 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
    • B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
    • 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
    • Y10T292/00—Closure fasteners
    • Y10T292/20—Clamps
    • Y10T292/202—Hatch fastener
    • 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
    • Y10T292/00—Closure fasteners
    • Y10T292/20—Clamps
    • Y10T292/205—Ring
    • Y10T292/212—With expanding or contracting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Clamps And Clips (AREA)
  • Details Of Aerials (AREA)

Abstract

Ein Verschlusselement für einen Bereich der Außenkontur eines Luftfahrzeugs, der zum Zwecke des Zugangs geöffnet und geschlossen werden kann, mit einem Scharnier (11, 12), durch welches das Verschlusselement (10) mit der Struktur (19) des Luftfahrzeugs (1) verbunden ist und um welches das Verschlusselement (10) zwischen einer geöffneten Position und einer geschlossenen Position geschwenkt werden kann, und mit einer Verriegelungsvorrichtung (15, 16, 17), mit welcher das Verschlusselement (10) in der geschlossenen Position gegen die Struktur des Luftfahrzeugs (1) verriegelbar ist. Erfindungsgemäß ist es vorgesehen, dass das Scharnier (11, 12) innerhalb der Außenkontur des Luftfahrzeugs (1) angeordnet ist und eine außerhalb der Außenkontur des Luftfahrzeugs (1) befindliche virtuelle Drehachse (X) aufweist, um welche das Verschlusselement (10) beim Öffnen und Schließen geschwenkt wird, und dass die Verriegelungsvorrichtung (15, 16, 17) so ausgebildet iat, dass sie das Verschlusselement (10) im geschlossenen Zustand unter im Wesentlichen vollständiger Entlastung des Scharniers (11, 12) formschlüssig mit der Struktur des Luftfahrzeugs verbindet. Das Verschlusselement kann beispielsweise, wie dargestellt, ein Radome (10), eine Inspektions- oder Wartungsluke oder eine Passagier- oder Frachtraumtür sein.
DE2003143627 2003-09-20 2003-09-20 Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs Expired - Fee Related DE10343627B4 (de)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE2003143627 DE10343627B4 (de) 2003-09-20 2003-09-20 Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs
FR0409718A FR2859975B1 (fr) 2003-09-20 2004-09-14 Dispositif de fermeture pour une structure porteuse
US10/943,251 US7503523B2 (en) 2003-09-20 2004-09-17 Closure system for a support structure
GB0420858A GB2406320B (en) 2003-09-20 2004-09-20 Closure device for a support structure
US12/340,141 US7909289B2 (en) 2003-09-20 2008-12-19 Closure system for a support structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2003143627 DE10343627B4 (de) 2003-09-20 2003-09-20 Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs

Publications (2)

Publication Number Publication Date
DE10343627A1 true DE10343627A1 (de) 2005-04-21
DE10343627B4 DE10343627B4 (de) 2014-03-06

Family

ID=33305261

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2003143627 Expired - Fee Related DE10343627B4 (de) 2003-09-20 2003-09-20 Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs

Country Status (4)

Country Link
US (2) US7503523B2 (de)
DE (1) DE10343627B4 (de)
FR (1) FR2859975B1 (de)
GB (1) GB2406320B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3620369A1 (de) * 2018-09-06 2020-03-11 Airbus Operations SAS Verbessertes türsystem für rumpf eines luftfahrzeugs

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10343627B4 (de) * 2003-09-20 2014-03-06 Eads Deutschland Gmbh Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs
FR2872778B1 (fr) * 2004-07-09 2007-10-12 Airbus France Sas Porte pour aeronef, et aeronef muni d'au moins une telle porte
US20060145016A1 (en) * 2004-12-30 2006-07-06 The Boeing Company Mating of spacecraft components using shape memory materials
US7748663B1 (en) * 2005-05-24 2010-07-06 Lockheed Martin Corporation Launch vehicle stage integration device
DE102006025388B4 (de) * 2006-05-31 2009-10-29 Airbus Deutschland Gmbh Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug
US7681837B2 (en) * 2007-08-17 2010-03-23 The Boeing Company Method and apparatus for closing a swing tail on an aircraft
US7970499B2 (en) * 2007-12-14 2011-06-28 The Boeing Company Method and apparatus for moving a swing tail cargo door on an aircraft
US7850122B2 (en) * 2007-12-14 2010-12-14 The Boeing Company Compliance mechanism
FR2940959B1 (fr) * 2009-01-15 2011-03-11 Airbus France Partie avant d'aeronef comportant une cloison concave separant une zone de radome non pressurisee et une zone pressurisee
FR2976909B1 (fr) * 2011-06-27 2013-07-12 Airbus Operations Sas Procede d'ouverture d'un dome de protection, en particulier d'un radome, et radome equipe d'un pantographe de mise en oeuvre
US8931738B2 (en) * 2012-02-21 2015-01-13 Raytheon Company Releasable radome cover
US9016631B2 (en) * 2012-04-09 2015-04-28 R4 Integration, Inc. Multi-purpose hatch system
US9279342B2 (en) 2012-11-21 2016-03-08 General Electric Company Turbine casing with service wedge
US9260281B2 (en) 2013-03-13 2016-02-16 General Electric Company Lift efficiency improvement mechanism for turbine casing service wedge
US10189578B2 (en) * 2013-06-12 2019-01-29 The Boeing Company Self-balancing pressure bulkhead
DE102013110480A1 (de) * 2013-09-23 2015-03-26 Airbus Operations Gmbh Blende und Türanordnung für ein Transportmittel
DE102013114391A1 (de) 2013-12-18 2015-06-18 Airbus Operations Gmbh Druckrumpf eines Flugzeuges, umfassend ein bewegbar relativ zur Rumpfstruktur befestigtes Druckschott
FR3032424B1 (fr) * 2015-02-06 2018-05-04 Airbus Operations Dispositif de manoeuvre d'au moins une trappe d'un aeronef comprenant une poignee de commande
RU2614871C2 (ru) * 2015-06-24 2017-03-30 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Грузовой отсек самолета
CN105547061B (zh) * 2015-12-18 2017-08-29 中国电子科技集团公司第四十一研究所 基于转台同步的天线罩大角度测量装置
US10145434B2 (en) * 2016-05-19 2018-12-04 The Boeing Company Translational inerter assembly and method for damping movement of a flight control surface
US10107347B2 (en) * 2016-05-19 2018-10-23 The Boeing Company Dual rack and pinion rotational inerter system and method for damping movement of a flight control surface of an aircraft
US10088006B2 (en) * 2016-05-19 2018-10-02 The Boeing Company Rotational inerter and method for damping an actuator
US10727574B2 (en) 2017-06-05 2020-07-28 The Nordam Group Llc Accessible radome assembly
DE102017120270B4 (de) 2017-09-04 2024-03-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Fahrzeug und Verfahren zur Herstellung einer Revisionsklappe
CN114616172A (zh) 2019-09-05 2022-06-10 Zsm控股有限责任公司 免于擦尾的允许长有效载荷的飞机机身构型
WO2021102441A1 (en) * 2019-11-22 2021-05-27 Zsm Holdings Llc Systems and methods for optimization of packaging large irregular payloads for shipment by air vehicles
WO2022093452A2 (en) 2020-09-23 2022-05-05 Zsm Holdings Llc Ram air turbine installations for low speed flight
CN117255757A (zh) 2021-02-03 2023-12-19 Zsm控股有限责任公司 用可更换尾锥加长飞机货舱的装置和方法
CA3213162A1 (en) 2021-03-10 2022-09-15 Zsm Holdings Llc Systems and methods for loading and unloading a cargo aircraft utilizing a curved path
EP4304936A1 (de) 2021-03-10 2024-01-17 ZSM Holdings LLC Abnehmbare frachtbodensysteme und verfahren für frachtflugzeug
CN117279831A (zh) 2021-03-10 2023-12-22 Zsm控股有限责任公司 后机身向上偏折的飞机机身构型
CN117295657A (zh) 2021-03-10 2023-12-26 Zsm控股有限责任公司 用于组装大型货物并将其装载至货运飞机的装置和方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4497462A (en) * 1983-03-28 1985-02-05 The Boeing Company Outward opening electrically powered plug-type cargo door
US4510714A (en) * 1982-09-30 1985-04-16 The Boeing Company Powered outward-opening cargo door
DE9207122U1 (de) * 1992-05-26 1992-08-13 Schemm Gmbh, 5952 Attendorn, De
DE29615287U1 (de) * 1996-09-04 1996-12-19 Berthold Horstmann Gmbh System zum Verbinden zweier Leitungen

Family Cites Families (87)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US503A (en) * 1837-12-07 Improvement in the manufacture of india-rubber boots and shoes
US1814933A (en) * 1930-09-02 1931-07-14 George J Keen Wire rope clamp
US2008741A (en) * 1932-02-03 1935-07-23 James R Allan Seal for closures
US2088909A (en) * 1933-12-19 1937-08-03 Jaubert George Francois Gastight closure
US2130297A (en) * 1936-06-02 1938-09-13 Om Edwards Co Inc Window and sash construction
US2301963A (en) * 1938-01-17 1942-11-17 Hancock Mfg Company Method of and apparatus for sealing and supporting closures
US2354789A (en) * 1940-08-26 1944-08-01 Atwood Vacuum Machine Co Automobile door hinge
US2473616A (en) * 1946-01-19 1949-06-21 Vickers Armstrongs Ltd Elliptical boundary frame for openings in pressure cabins for aircraft
US2530160A (en) * 1947-02-17 1950-11-14 Virgil A Finley Door seal
US2469131A (en) * 1947-05-28 1949-05-03 Chrysler Corp Inflatable door sealing system
US2549110A (en) * 1949-05-31 1951-04-17 Northrop Aircraft Inc Panel hinge
US2869485A (en) * 1954-08-03 1959-01-20 Diebold Inc Vault door construction
US2943756A (en) * 1956-05-24 1960-07-05 Gen Dynamics Corp Hinge structure
US3009672A (en) * 1961-03-10 1961-11-21 Douglas Aircraft Co Inc Jointure for end-loading aircraft
GB978841A (en) * 1962-02-22 1964-12-23 Short Brothers & Harland Ltd Improvements in nose-wheel undercarriage apparatus for aircraft
GB964617A (en) * 1962-07-24 1964-07-22 English Electric Co Ltd Improvements in and relating to aircraft fuselages
US3129040A (en) * 1962-10-19 1964-04-14 Rose James De Cabinet having an electrically operated closure
FR1533157A (fr) * 1963-08-05 1968-07-19 Maille & Vagneux Ets Système conditionnant le fonctionnement des portes à joint d'étanchéité gonflable
US3374972A (en) * 1965-09-27 1968-03-26 Lockheed Aircraft Corp Hinged end section for cargo aircraft
US3653615A (en) * 1969-06-03 1972-04-04 Spence William Aircraft nose opening mechanism
US3987876A (en) * 1975-12-17 1976-10-26 Scovill Manufacturing Company Luggage closure
US4106661A (en) * 1976-01-07 1978-08-15 The United States Of America As Represented By The Secretary Of The Army Inflatably sealed sterilizer door
US4011819A (en) * 1976-03-03 1977-03-15 The United States Of America As Represented By The Secretary Of The Navy Stress relieved molded cover assembly and method of making the same
US4030850A (en) * 1976-08-02 1977-06-21 The United States Of America As Represented By The Secretary Of The Army Interlocked joint
US4324373A (en) * 1979-11-19 1982-04-13 Ppg Industries, Inc. Method and apparatus for add-on reinforcement for transparency system for crew module for aircraft
US4312153A (en) * 1979-12-14 1982-01-26 Lockheed Corporation Door seal
US4441278A (en) * 1981-11-12 1984-04-10 The Presray Corporation Mounting for endless sealing strips
US4581615A (en) * 1983-02-08 1986-04-08 Levy Stanley P Double reflector antenna with integral radome reflector support
US4627355A (en) * 1984-06-19 1986-12-09 Westinghouse Electric Corp. Joint release mechanism
US4679750A (en) * 1984-06-20 1987-07-14 The Boeing Company Latch system
US4720065A (en) * 1985-01-24 1988-01-19 The Boeing Company Translatable outward opening plug-type aircraft door and actuating mechanisms therefor
USH451H (en) * 1985-12-04 1988-04-05 The United States Of America As Represented By The Secretary Of The Air Force Frameless transparencies for aircraft cockpit enclosure
IT1191735B (it) * 1986-04-15 1988-03-23 Riva Calzoni Spa Gruppo connettore ad innesto rapido per tubi,pali o simili
US4749997A (en) * 1986-07-25 1988-06-07 Grumman Aerospace Corporation Modular antenna array
US4739955A (en) * 1986-09-30 1988-04-26 The Boeing Company Aircraft cabin panel and insulation retainer with integrated use as a spacer-isolator
US4706413A (en) * 1986-10-16 1987-11-17 James Kenneth S Smoke detector-activated door seal
CA1272417A (en) * 1986-11-27 1990-08-07 Leonard William Westwell Airtight door assembly
EP0308971B1 (de) * 1987-09-24 1993-11-24 Kabushiki Kaisha Toshiba Lötstelle und Verfahren zu ihrer Bewerkstelligung
KR920010807B1 (en) * 1988-09-01 1992-12-17 Yoshida Kogyo Kk Sliding door opening and closing apparatus
US5176493A (en) * 1989-02-24 1993-01-05 North American Philips Corporation High speed wafer handling method
US5031863A (en) * 1989-12-21 1991-07-16 The Boeing Company Upward/outward opening, plug-type overwing emergency exit hatch
US5312153A (en) * 1990-07-23 1994-05-17 Ortho-Kinetics, Inc. Recline lift wall hugger chair
SE466562B (sv) * 1991-03-04 1992-03-02 Saab Space Ab Laasmekanism vid bandorgan foer fasthaallande av satellit vid adapter paa baerraket
US5102070A (en) * 1991-06-13 1992-04-07 Air Cruisers Company Inflatable aircraft evacuation slide arrangement
DE4221525C2 (de) * 1992-07-01 1996-08-08 Daimler Benz Aerospace Ag Vorrichtung zum Verbinden zylindrischer Bauteile
US5352061A (en) * 1993-01-05 1994-10-04 Honeywell Inc. Anti-rotation ring joint
US5350136A (en) * 1993-05-14 1994-09-27 United Technologies Corporation Nacelle arrangement
US5346272A (en) * 1993-06-07 1994-09-13 General Motors Corporation Door hinge with infinitely adjustable detent
US5520476A (en) * 1993-06-18 1996-05-28 Astro Aerospace Corporation Tie-down and release mechanism for spacecraft
US5743492A (en) * 1994-02-18 1998-04-28 Lockheed Martin Corporation Payload housing and assembly joint for a launch vehicle
SE509256C2 (sv) * 1994-06-14 1998-12-21 Saab Ericsson Space Ab Förband för lösbar förbindning av adapter på bärraket med satellit
ES2121416T3 (es) * 1994-10-08 1998-11-16 Whitley Don Scient Ltd Armarios y sistemas anaerobicos.
US6029928A (en) * 1994-11-21 2000-02-29 Kelly Space & Technology Inc. Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft
US5691736A (en) * 1995-03-28 1997-11-25 Loral Vought Systems Corporation Radome with secondary heat shield
DE19529706C2 (de) * 1995-08-11 2001-08-02 Deutsch Zentr Luft & Raumfahrt Flächentragwerk, insbesondere für ein Luftfahrzeug
US5820077A (en) * 1995-09-26 1998-10-13 Mcdonnell Douglas Technologies, Inc. Aircraft radome and integral attaching structure
US5975463A (en) * 1995-12-21 1999-11-02 Mcdonnell Douglas Expandable aircraft bay and method
US5803406A (en) * 1996-04-22 1998-09-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated thermal insulation system for spacecraft
DE19650416B4 (de) * 1996-12-05 2004-10-07 Airbus Deutschland Gmbh Fenster für ein Flugzeug mit einer Druckkabine
DE19702084C1 (de) 1997-01-22 1998-02-19 Eurocopter Deutschland Türsystem für ein Passagierflugzeug
US5896112A (en) * 1997-01-22 1999-04-20 The Whitaker Corporation Antenna compensation for differential thermal expansion rates
US5931415A (en) * 1997-05-09 1999-08-03 The Boeing Company Plug-type overwing emergency exit door assembly
ES2131476B1 (es) * 1997-09-26 2000-03-01 Const Aeronauticas Sa Sistema de fijacion y separacion de satelites.
US6196617B1 (en) * 1997-09-30 2001-03-06 Krystal Koach, Inc. Rear door structure for a vehicle
US6059234A (en) * 1998-02-25 2000-05-09 Kistler Aerospace Corporation Payload module
NO306917B1 (no) * 1998-07-13 2000-01-10 Abb Offshore Technology As Leddet klammerkopling
FR2782495B1 (fr) * 1998-08-19 2000-11-10 Aerospatiale Structure avant d'avion
US6193436B1 (en) * 1998-12-03 2001-02-27 Rand Display, Inc. Locking system for supporting element
SE511762C2 (sv) * 1999-02-03 1999-11-22 Saab Ericsson Space Ab Förband vid rymdfarkost
US6213426B1 (en) * 1999-07-09 2001-04-10 The Boeing Company Monolithic structure with redundant load paths
US6394392B1 (en) * 1999-10-19 2002-05-28 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
FR2807388B1 (fr) * 2000-04-07 2002-06-28 Aerospatiale Matra Airbus Porte d'aeronef et aeronef equipe d'une telle porte
EP1215137A1 (de) * 2000-12-13 2002-06-19 Alcan Technology & Management AG Frachtcontainer für Lufttransporte
SE516568C2 (sv) * 2000-12-14 2002-01-29 Saab Ericsson Space Ab Förband vid en rymdfarkost
FR2819782B1 (fr) * 2001-01-25 2003-04-11 Eads Airbus Sa Dispositif d'articulation d'un battant de porte d'aeronef et porte d'aeronef integrant un tel dispositif
US6648543B2 (en) * 2001-04-19 2003-11-18 Saab Ericsson Space Ab Device for a space vessel
US7337019B2 (en) * 2001-07-16 2008-02-26 Applied Materials, Inc. Integration of fault detection with run-to-run control
US6622967B2 (en) * 2002-01-09 2003-09-23 Lockheed Martin Corporation Aerodynamic control for separation of unstable bodies
US6702300B1 (en) * 2002-01-11 2004-03-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration High temperature seal for large structural movements
FR2835235B1 (fr) * 2002-01-31 2004-04-09 Airbus France Porte ejectable, pour aeronef
USD512365S1 (en) * 2002-06-25 2005-12-06 The Boeing Company Aircraft window
US6951319B2 (en) * 2002-11-22 2005-10-04 Theboeing Company Flexible hydraulic latch
DE10301783B4 (de) * 2003-01-18 2005-04-28 Eads Space Transp Gmbh Vorrichtung zum lösbaren Verbinden rotationssymmetrischer Bauteile
DE10343627B4 (de) * 2003-09-20 2014-03-06 Eads Deutschland Gmbh Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs
FR2864020B1 (fr) * 2003-12-19 2006-02-10 Airbus France Nez d'avion avec bouclier
US20050247823A1 (en) * 2004-05-04 2005-11-10 Wood Jeffrey H Injection-molded polycarbonate door
US7883058B2 (en) * 2005-08-23 2011-02-08 Airbus Deutschland Gmbh Combined displacement and swivel mechanism

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4510714A (en) * 1982-09-30 1985-04-16 The Boeing Company Powered outward-opening cargo door
US4497462A (en) * 1983-03-28 1985-02-05 The Boeing Company Outward opening electrically powered plug-type cargo door
DE9207122U1 (de) * 1992-05-26 1992-08-13 Schemm Gmbh, 5952 Attendorn, De
DE29615287U1 (de) * 1996-09-04 1996-12-19 Berthold Horstmann Gmbh System zum Verbinden zweier Leitungen

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3620369A1 (de) * 2018-09-06 2020-03-11 Airbus Operations SAS Verbessertes türsystem für rumpf eines luftfahrzeugs
FR3085664A1 (fr) * 2018-09-06 2020-03-13 Airbus Operations Systeme de porte ameliore pour fuselage d'aeronef
US11548611B2 (en) 2018-09-06 2023-01-10 Airbus Operations Sas Door system for aircraft fuselage

Also Published As

Publication number Publication date
GB2406320A (en) 2005-03-30
US20050116106A1 (en) 2005-06-02
GB2406320B (en) 2006-09-06
GB0420858D0 (en) 2004-10-20
DE10343627B4 (de) 2014-03-06
FR2859975A1 (fr) 2005-03-25
US20090173824A1 (en) 2009-07-09
US7503523B2 (en) 2009-03-17
FR2859975B1 (fr) 2009-01-16
US7909289B2 (en) 2011-03-22

Similar Documents

Publication Publication Date Title
DE10343627A1 (de) Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs
AT500017B1 (de) Schwenkschiebetür für fahrzeuge
DE102007053554A1 (de) Verriegelung für ein Frachttor in einem Flugzeug
DE602005000111T2 (de) Flugzeugtür und ein Flugzeug mit einer solchen Tür
EP2112314A3 (de) Türanordnung mit einer Flügeltür- und einer Schiebetürfunktion, die mittels eines einzigen Betätigungselements betätigt werden können
DE102010013715B4 (de) Verriegelungsmechanismus für eine Luftfahrzeugtür, Verfahren zum Verriegeln einer Luftfahrzeugtür und Flugzeugtür
EP2724929A1 (de) Vorrichtung zur schocksicheren Tür- oder Lukenanordnung auf Marineschiffen
EP1857375A1 (de) Behälterverschluss mit Verschlussplombe für Kunststoffbehälter
EP2402532B1 (de) Türband, insbesondere für Hohlprofilzargen
EP2241705A3 (de) Schließzylinder für ein Kraftfahrzeug
DE102006007111B3 (de) Vorrichtung mit einem Verschlusselement und einem Grundkörper
AT521373A4 (de) Anordnung zur Führung einer Schiebetür
DE102019112336B4 (de) Türeinheit für ein Fahrzeug
EP1331335A3 (de) Duschabtrennung
DE4140289C2 (de) Türscharnier für eine Kraftfahrzeugtür
DE102018130527B3 (de) Türanordnung mit Gelenkarm, Flugzeugbereich mit Türanordnung und Flugzeug mit Flugzeugbereich
EP1705324A2 (de) Scharnierelement innenliegender Bauart
DE741677C (de) UEberwurf-Spannverschluss fuer Kisten, Kasten, Koffer u. dgl.
EP2653636A3 (de) Schwenkhebelverschluss mit einem für einen variablen Schließmitteleinsatz eingerichteten Schwenkhebel
DE940755C (de) Fluegel fuer Fenster, insbesondere Dachfenster
DE688068C (de) Gasdichter Schluessellochverschluss
DE102020112803A1 (de) Gepäckraumabdeckung zur Anordnung an einer Heckklappe
DE647685C (de) Verschluss, insbesondere fuer Tueren o. dgl.
DE102004050229A1 (de) Seitentür für einen Kraftwagen
DE704206C (de) Verschluss fuer Schiebetueren

Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
R084 Declaration of willingness to licence

Effective date: 20110915

R016 Response to examination communication
R018 Grant decision by examination section/examining division
R081 Change of applicant/patentee

Owner name: AIRBUS DEFENCE AND SPACE GMBH, DE

Free format text: FORMER OWNER: EADS DEUTSCHLAND GMBH, 85521 OTTOBRUNN, DE

Effective date: 20140819

R020 Patent grant now final
R020 Patent grant now final

Effective date: 20141209

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee