WO2010001210A3 - Aircraft door with supporting control arm arrangement - Google Patents

Aircraft door with supporting control arm arrangement Download PDF

Info

Publication number
WO2010001210A3
WO2010001210A3 PCT/IB2009/005997 IB2009005997W WO2010001210A3 WO 2010001210 A3 WO2010001210 A3 WO 2010001210A3 IB 2009005997 W IB2009005997 W IB 2009005997W WO 2010001210 A3 WO2010001210 A3 WO 2010001210A3
Authority
WO
WIPO (PCT)
Prior art keywords
door
fuselage
aircraft
door leaf
hinge
Prior art date
Application number
PCT/IB2009/005997
Other languages
French (fr)
Other versions
WO2010001210A2 (en
Inventor
Matthias Sterr
Dirk Trott
Original Assignee
Eurocopter 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
Priority to DE200810030696 priority Critical patent/DE102008030696A1/en
Priority to DE102008030696.7 priority
Application filed by Eurocopter Deutschland Gmbh filed Critical Eurocopter Deutschland Gmbh
Publication of WO2010001210A2 publication Critical patent/WO2010001210A2/en
Publication of WO2010001210A3 publication Critical patent/WO2010001210A3/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/14Windows; 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
    • B64C1/1407Doors; surrounding frames
    • B64C1/1423Passenger doors
    • B64C1/143Passenger doors of the plug type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/14Windows; 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
    • B64C1/1407Doors; surrounding frames

Abstract

An aircraft door in an aircraft fuselage (1), in particular a passenger door (2) for commercial aircraft, comprising a door leaf (3), a lever device (5, 7) for deflecting the weight of the door leaf (3) onto the aircraft fuselage (1), comprising two parallel control arms for parallel pivoting the door leaf (3) during opening and closing, in each case with a hinge (9; 13) on the door side and a hinge (11; 15) on the fuselage side, in each case comprising essentially vertical axes (27; 29), wherein the one hinge axis (29) on the fuselage side is arranged so as to be axially offset relative to the other hinge axis (27) on the fuselage side such that the connecting lines (6; 8) of the hinge axes, on the door side and on the fuselage side, of the respective control arm (5; 7) at no position of the door leaf (3) cover each other in a parallel manner during movement of said door leaf (3).
PCT/IB2009/005997 2008-07-01 2009-06-19 Aircraft door with supporting control arm arrangement WO2010001210A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE200810030696 DE102008030696A1 (en) 2008-07-01 2008-07-01 Airplane door with support arm arrangement
DE102008030696.7 2008-07-01

Publications (2)

Publication Number Publication Date
WO2010001210A2 WO2010001210A2 (en) 2010-01-07
WO2010001210A3 true WO2010001210A3 (en) 2010-04-08

Family

ID=41110681

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2009/005997 WO2010001210A2 (en) 2008-07-01 2009-06-19 Aircraft door with supporting control arm arrangement

Country Status (2)

Country Link
DE (1) DE102008030696A1 (en)
WO (1) WO2010001210A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012177258A1 (en) * 2011-06-23 2012-12-27 The Boeing Company Doorway width restriction system
DE102011109652A1 (en) * 2011-08-05 2013-02-07 Airbus Operations Gmbh Support arm arrangement, door and means of transport
FR3071222B1 (en) * 2017-09-20 2020-11-27 Latecoere SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER
DE102018121240A1 (en) * 2018-08-30 2020-03-05 Airbus Operations Gmbh Door arrangement for an aircraft and aircraft
FR3087189A1 (en) * 2018-10-10 2020-04-17 Latecoere METHOD FOR OPENING / CLOSING AN AIRCRAFT DOOR AND AIRCRAFT FOR IMPLEMENTING SUCH A METHOD

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB452679A (en) * 1935-07-20 1936-08-27 George Harold Wenham Improvements in, or relating to, means for hanging vehicle doors
US2564988A (en) * 1946-10-10 1951-08-21 Glenn L Martin Co Door hinge linkage
GB868390A (en) * 1958-07-04 1961-05-17 Vickers Aircraft Holdings Ltd Improvements in doors for pressurized fuselages of aircraft
EP1418121A1 (en) * 2002-11-06 2004-05-12 Eaton Fluid Power GmbH Emergency door actuator system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2819782B1 (en) 2001-01-25 2003-04-11 Eads Airbus Sa Hinge device for an aircraft door and aircraft door with integrated device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB452679A (en) * 1935-07-20 1936-08-27 George Harold Wenham Improvements in, or relating to, means for hanging vehicle doors
US2564988A (en) * 1946-10-10 1951-08-21 Glenn L Martin Co Door hinge linkage
GB868390A (en) * 1958-07-04 1961-05-17 Vickers Aircraft Holdings Ltd Improvements in doors for pressurized fuselages of aircraft
EP1418121A1 (en) * 2002-11-06 2004-05-12 Eaton Fluid Power GmbH Emergency door actuator system

Also Published As

Publication number Publication date
WO2010001210A2 (en) 2010-01-07
DE102008030696A1 (en) 2010-01-14

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