EA200501931A3 - Механизм открытия и закрытия люка, преимущественно ниши шасси летательного аппарата - Google Patents

Механизм открытия и закрытия люка, преимущественно ниши шасси летательного аппарата

Info

Publication number
EA200501931A3
EA200501931A3 EA200501931A EA200501931A EA200501931A3 EA 200501931 A3 EA200501931 A3 EA 200501931A3 EA 200501931 A EA200501931 A EA 200501931A EA 200501931 A EA200501931 A EA 200501931A EA 200501931 A3 EA200501931 A3 EA 200501931A3
Authority
EA
Eurasian Patent Office
Prior art keywords
lateral
pivot support
auxiliary
hatch
landing gear
Prior art date
Application number
EA200501931A
Other languages
English (en)
Other versions
EA009541B1 (ru
EA200501931A2 (ru
Inventor
Лара Сантос Рубио
Хосе Луис Чичарро Гонсалес
Original Assignee
Эрбус Эспанья, С. Л.
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 Эрбус Эспанья, С. Л. filed Critical Эрбус Эспанья, С. Л.
Publication of EA200501931A2 publication Critical patent/EA200501931A2/ru
Publication of EA200501931A3 publication Critical patent/EA200501931A3/ru
Publication of EA009541B1 publication Critical patent/EA009541B1/ru

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
    • 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
    • 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
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B64D1/06—Bomb releasing; Bomb doors
    • 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
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/32—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing
    • E06B3/48—Wings connected at their edges, e.g. foldable wings
    • E06B3/481—Wings foldable in a zig-zag manner or bi-fold wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Hinges (AREA)
  • Retarders (AREA)
  • Elevator Door Apparatuses (AREA)
  • Mechanically-Actuated Valves (AREA)
  • Transmission Devices (AREA)
  • Extensible Doors And Revolving Doors (AREA)

Abstract

В заявке описан механизм открытия и закрытия люка, преимущественно ниши шасси летательного аппарата, содержащий боковую закрывающую панель (1) и вспомогательную закрывающую панель (4), шарнирно соединенные между собой, боковую поворотную опору (5), которая своей нижней частью крепится к боковой панели (1) и соединяется с неподвижным элементом (7) конструкции при помощи боковых средств (6) шарнирного сочленения, вспомогательную поворотную опору (8), которая своей нижней частью крепится к вспомогательной панели (4), боковой силовой цилиндр (10), шарнирно соединенный с неподвижным элементом конструкции и боковой поворотной опорой (5), и промежуточный силовой цилиндр (13), который соединен с боковой поворотной опорой (5) в первой точке (14) соединения, расположенной между боковыми (6) и промежуточными (9) средствами шарнирного сочленения, а также со вспомогательной поворотной опорой (8) во второй точке (15) соединения, и который может приводиться в действие независимо от бокового силового цилиндра (10).
EA200501931A 2004-12-31 2005-12-30 Механизм открытия и закрытия люка, преимущественно ниши шасси летательного аппарата EA009541B1 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200403173A ES2281227B1 (es) 2004-12-31 2004-12-31 Un mecanismo de accionamiento de una trampa, particularmente para un tren de aterrizaje de un avion.

Publications (3)

Publication Number Publication Date
EA200501931A2 EA200501931A2 (ru) 2006-08-25
EA200501931A3 true EA200501931A3 (ru) 2006-12-29
EA009541B1 EA009541B1 (ru) 2008-02-28

Family

ID=35703589

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200501931A EA009541B1 (ru) 2004-12-31 2005-12-30 Механизм открытия и закрытия люка, преимущественно ниши шасси летательного аппарата

Country Status (6)

Country Link
US (1) US7677497B2 (ru)
EP (1) EP1752374B1 (ru)
AT (1) ATE393090T1 (ru)
DE (1) DE602005006273T2 (ru)
EA (1) EA009541B1 (ru)
ES (2) ES2281227B1 (ru)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0214119D0 (en) * 2002-06-19 2002-07-31 Airbus Uk Ltd Landing gear door assembly
FR2869013B1 (fr) * 2004-04-20 2007-07-13 Airbus France Sas Deflecteur de flux aerodynamique pour train d'atterrissage d'aeronef
GB0619615D0 (en) * 2006-10-04 2006-11-15 Airbus Uk Ltd A door for opening and closing a door aperture in an aircraft
US9243920B2 (en) 2007-04-17 2016-01-26 Esther Abramovich Ettinger System and method for adapting the routing information provided by a mapping or routing device
ITTO20080099A1 (it) * 2008-02-08 2009-08-09 Alenia Aeronautica Spa Struttura di porta per un vano nella fusoliera o nell'ala di un velivolo
RU2555073C2 (ru) * 2013-07-01 2015-07-10 Николай Евгеньевич Староверов Устройство для поворота детали на угол до 330 градусов (варианты)
CN103600837B (zh) * 2013-10-25 2016-03-09 中国商用飞机有限责任公司 用于控制飞机起落架舱门的连杆机构
FR3025492A1 (fr) * 2014-09-05 2016-03-11 Airbus Operations Sas Aeronef comportant deux portes de train d'atterrissage et un systeme de manœuvre desdites portes
US10836473B2 (en) * 2017-10-24 2020-11-17 Embraer S.A. Mechanisms, systems and methods to allow step-ajdustment of aerodynamic surfaces
CN111071475B (zh) * 2019-12-13 2022-07-12 西安飞机工业（集团）有限责任公司 一种飞机主起维护舱门闭合方法及助力装置
EP3929075B1 (en) * 2020-06-24 2022-10-19 Airbus Operations, S.L.U. Landing gear door system and operation method
DE102022128630B3 (de) * 2022-10-28 2024-03-14 Airbus Defence and Space GmbH Fahrzeugrumpf mit Kavität in der Außenhaut und einer verschließenden Türanordnung

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3088694A (en) * 1960-12-29 1963-05-07 Gen Electric Wing-fan doors
FI40140C (fi) * 1961-11-27 1968-10-10 Konstruktioner & Experiment Ab Anordning för manövrering av i sicksack sammanvikbara lastrumsluckor
FR1352138A (fr) * 1962-09-25 1964-02-14 Aviation Louis Breguet Sa Porte de soute pour fuselage d'aéronefs
SE312995B (ru) * 1967-06-26 1969-07-28 Ass Cargo Gear Ab
US3430675A (en) * 1967-12-08 1969-03-04 Ass Cargo Gear Ab Hatch cover
GB1347690A (en) * 1970-10-10 1974-02-27 British Aircraft Corp Ltd Doors
DE2914469C2 (de) * 1979-04-10 1986-02-27 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Betätigungsvorrichtung für eine Klappe, die insbesondere an einer Flugzeugzelle, einem Raumfahrzeug oder dergleichen schwenkbar angeordnet ist und insbesondere zum Verschließen einer Luftansaugöffnung für die Starterturbine eines Flugzeugtriebwerks dient
US4568045A (en) * 1983-08-17 1986-02-04 The Boeing Company Door operated linkage for support of retracted airplane landing gear
DE3513631A1 (de) * 1985-04-16 1986-10-16 Efaflex Transport- und Lager-Technik GmbH, 8301 Bruckberg Falttor
DE4134499C2 (de) * 1991-10-18 1994-09-22 Deutsche Aerospace Airbus Klappe zum Schließen einer Beladeöffnung
RU2078714C1 (ru) * 1993-08-20 1997-05-10 Воронежское конструкторское бюро авиационного научно-технического комплекса им.А.Н.Туполева Привод створок люка
US5803405A (en) * 1995-06-07 1998-09-08 Northrop Grumman Corporation Expandable aircraft section
US6068215A (en) * 1995-12-21 2000-05-30 Mcdonnall Douglas Expandable aircraft cargo bay and method
US5975463A (en) * 1995-12-21 1999-11-02 Mcdonnell Douglas Expandable aircraft bay and method
US5716030A (en) * 1996-02-06 1998-02-10 Hughes Aircraft Company Aperture door and calibration source for spacecraft remote sensing devices
US5947417A (en) * 1997-07-25 1999-09-07 Mcdonnell Douglas Fairing for an expandable bay
FR2800707B1 (fr) * 1999-11-10 2002-01-18 Aerospatiale Matra Airbus Indicateur de defaut de fermeture, notamment pour des capots de nacelle d'un moteur d'avion
US6352221B1 (en) * 2000-03-03 2002-03-05 The Boeing Company Rotary landing gear assembly
US6345786B1 (en) * 2000-03-03 2002-02-12 The Boeing Company Linked multi-segment landing gear door for aircraft
US6536711B1 (en) * 2000-10-18 2003-03-25 Lockheed Martin Corporation Single aperture conformal aircraft bays
GB0214119D0 (en) * 2002-06-19 2002-07-31 Airbus Uk Ltd Landing gear door assembly
FR2866313B1 (fr) * 2004-02-13 2007-04-20 Airbus France Trappe articulee pour train d'atterrissage d'aeronef
GB0619615D0 (en) * 2006-10-04 2006-11-15 Airbus Uk Ltd A door for opening and closing a door aperture in an aircraft

Also Published As

Publication number Publication date
EP1752374B1 (en) 2008-04-23
ATE393090T1 (de) 2008-05-15
EA009541B1 (ru) 2008-02-28
DE602005006273T2 (de) 2009-07-16
US7677497B2 (en) 2010-03-16
EA200501931A2 (ru) 2006-08-25
US20060157621A1 (en) 2006-07-20
DE602005006273D1 (de) 2008-06-05
ES2281227A1 (es) 2007-09-16
EP1752374A1 (en) 2007-02-14
ES2306003T3 (es) 2008-11-01
ES2281227B1 (es) 2008-09-16

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Legal Events

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TC4A Change in name of a patent proprietor in a eurasian patent

Designated state(s): AM AZ BY KZ KG MD TJ TM RU

MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): RU