EP2094924B1 - Serrure pour portes d'aéronefs, en particulier d'hélicoptères - Google Patents

Serrure pour portes d'aéronefs, en particulier d'hélicoptères Download PDF

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Publication number
EP2094924B1
EP2094924B1 EP20070856019 EP07856019A EP2094924B1 EP 2094924 B1 EP2094924 B1 EP 2094924B1 EP 20070856019 EP20070856019 EP 20070856019 EP 07856019 A EP07856019 A EP 07856019A EP 2094924 B1 EP2094924 B1 EP 2094924B1
Authority
EP
European Patent Office
Prior art keywords
door
catch
hook
locking
locking hook
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.)
Not-in-force
Application number
EP20070856019
Other languages
German (de)
English (en)
Other versions
EP2094924A2 (fr
Inventor
Klaus KÖPPEL
Alexander Rowbut
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 Helicopters Deutschland GmbH
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
Application filed by Eurocopter Deutschland GmbH filed Critical Eurocopter Deutschland GmbH
Publication of EP2094924A2 publication Critical patent/EP2094924A2/fr
Application granted granted Critical
Publication of EP2094924B1 publication Critical patent/EP2094924B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B83/00—Vehicle locks specially adapted for particular types of wing or vehicle
    • E05B83/16—Locks for luggage compartments, car boot lids or car bonnets
    • E05B83/24—Locks for luggage compartments, car boot lids or car bonnets for car bonnets
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B83/00—Vehicle locks specially adapted for particular types of wing or vehicle
    • E05B83/16—Locks for luggage compartments, car boot lids or car bonnets
    • 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
    • Y10T292/08—Bolts
    • Y10T292/0911—Hooked end
    • Y10T292/0926—Spring projected
    • 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
    • Y10T292/08—Bolts
    • Y10T292/1043—Swinging
    • Y10T292/1044—Multiple head
    • Y10T292/1045—Operating means
    • Y10T292/1047—Closure
    • 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
    • Y10T70/00—Locks
    • Y10T70/50—Special application
    • Y10T70/5093—For closures
    • Y10T70/5155—Door

Definitions

  • the invention relates to a door lock for doors of aircraft, in particular of helicopters according to the preamble of claim 1.
  • Such doors are known for the approach of the pilot formed as gullwing doors. Unlike land vehicles, the doors which are provided there within the openings provided in the fuselage structure must be absolutely securely closed - infiltrated - in aircraft, whereby so-called gas pressure springs are generally provided for the necessary sealing between door and door opening.
  • the doors of a helicopter make the first contact with the aircraft and thus determine the first impression to the respective user. There is therefore a requirement that doors are self-explanatory of their operability and function and do not already constitute the first manual and / or technical obstacle when entering the helicopter.
  • the functions of the door lock should also be understandable and logical without additional signs and instructions for everyone.
  • a generic, all features of the preamble of claim 1 having door locking device for doors of helicopters is available for the helicopter Eurocopter EC 135 as an optional extra and in use.
  • a device for locking a front hood of a motor vehicle has at least one main closure and at least one additional closure, each one Include rotary latch with pawl and lockable by the catch in the closed position of the front cover closing member.
  • the closing member of the additional closure is designed so that when unlocked main lock only after a desired opening stroke of the front hood uses a locking action between closing member and rotary latch of the additional closure.
  • a disadvantage here proves that in pre-locking position, ie after activation of the catch between the front hood and body remains a gap.
  • the DE 195 30 723 A1 discloses an engine hood closure device for a motor vehicle having at least one hood fastener attached to the body, which has a catch and a pawl interacting with the catch, at least one striker associated with the hood and attached to the engine hood of the motor vehicle, and a securing position by means of a catch spring spring-loaded catch hook for holding the hood in an opening ready position.
  • the pawl can be lifted via a arranged in the interior of the motor vehicle actuator from a detent of the catch, the hood can be raised by the catch with excavated pawl in the opening ready position and wherein the hood after manual actuation of the catch hook from the opening ready position can be raised to the open position.
  • the bonnet closure has an electrically controllable opening actuator, which has an associated with the pawl actuator.
  • the invention is therefore an object of the invention to provide a new door lock device, which is better than previously suppressed while maintaining the locking security.
  • the new door lock is surprisingly advantageous.
  • the catch hook according to the invention which is in geared engagement with the locking hook, namely the affected, designed as a hinged door door in the Schileßlage before the effective date of the locking hook, in the Schileßlage, in which the locking hook is only in the region of the catch, "caught", so alone by further moving the locking hook in its closed position over the said handle, the door is in its final closed position can be transferred, without this is a holding / tightening / pressing the door in the present in the hull structure opening by hand is necessary.
  • the geared connection which according to the invention as arranged perpendicular to the pivot axis of the locking and catch hook spring-loaded
  • Swivel wedge is formed, the catch hook released for a new closing operation.
  • Wedge surface and catch level of the pivoting wedge are arranged at its end faces of catch and locking hooks facing effective surface, which acted upon by a torsion spring in relation to its bearing pin counter-clockwise swivel wedge, as soon as the catching stage is in operative connection with an extension of the fishing hook, this in his in Attachment to the stop pin got locked position.
  • the inventive design of the door lock facilitates the safe closing of such doors considerably and therefore significantly increases the ease of use for the crew of a helicopter.
  • a locking device for the not shown wing door of an aircraft is in the Fig. 1 to 5 only one of the hinged door firmly connected to the locking devices 10 which are actuated via a likewise not shown a hand lever exhibiting linkage and each cooperating with a fastened to the fuselage structure of the aircraft as a detent 11 fitting.
  • Each of the locking devices 10 has an angular support plate 12, whose angled by about 90 ° part forms a flange 13, the oblique - see Fig. 4 - Is arranged for approximately horizontal plane of action of the locking device.
  • the respective locking device is attached to the wing door of the helicopter by means of screws, not shown here.
  • the flange 13 carries a bearing pin 15 for a pivotally mounted pivoting wedge 16, which is acted upon by a torsion spring 17 in the counterclockwise direction cf.
  • a plate-shaped extension 18 of the support plate 12 carries a bearing pin 19 for receiving the locking members to be described and has at its free end to the bolt 20 of the catch 11 facing slot-shaped opening 22.
  • the trailing edge 23 of the slot-shaped opening 22 serves as a stop and thus as a limitation of the movement of the hinged door in its closed position.
  • the pivoting wedge 16 engages through an opening 24 provided in its region in the extension 18 of the carrier plate 12 into the pivoting range of the locking members to be described.
  • the pivot wedge 16 has for the purpose of leadership in the opening 24 of the support plate 12 has a lateral extension 26 which forms a common wedge surface 28 with the end face of the free end of the pivoting wedge; see. FIG. 5 , Furthermore, laterally offset from the wedge surface 28 is a catching step 29 - FIG. 2 - provided, which, as will be described, the temporary locking of one of the locking members is used.
  • the said locking members comprise a catch hook 30 designed as a two-armed lever and adjacent thereto a locking hook 31, which also acts as a two-armed lever, acts as a so-called rotary latch and acts as a rotary latch - which are pivotally mounted on the bearing pin 19 of the support plate 12.
  • a Torsionsfeder 34 acts on the fishing hook 30 in a clockwise direction with respect to the bearing pin 19 - see.
  • FIG. 1 The movement of the fishing hook 30 in the counterclockwise direction is limited by a stop pin 32 which is fixed in the plate-shaped extension 18 of the support plate 12.
  • the catch hook 30 has at its the bolt 20 facing the free end to a downwardly directed slot-shaped opening 36, the bolt facing the boundary terminates in a wedge surface 37.
  • the opposite lever arm of the fishing hook carries a support plate facing extension 38 which cooperates with the catching step 29 of the pivoting wedge 16; see.
  • FIG. 2 The opposite lever arm of the fishing hook carries a support plate facing extension 38 which cooperates with the catching step
  • the bolt 20 facing the free end of the two-armed locking hook 31 also has a slot-shaped opening 39, which merges at its free end in a wedge surface 40; see. FIG. 3 , Said wedge surfaces 36 and 39 of the associated locking members, namely the catch hook 30 and the locking hook 31 support the catching and locking movement of the locking members clockwise about their bearing pin on the bolt 20 as soon as the hinged door is manually transferred to a position close to the closed position.
  • the remote lever arm of the locking hook 31 carries a provided with a ball head 42 bearing pin 43 - see.
  • FIG. 2 - Which projects by means of a bushing 44 in the pivoting range of catch and locking hooks, as well as in the region of the wedge surface 28 of the pivoting wedge 16 in order to move them, as will be described.
  • the catch lever 30 is in contact with the catching lever 30 via the wedge surface 28 by means of the bolt 20 Fig. 3 pivoted clockwise about the bearing pin 19 against the action of the spring 34 by a small angular amount.
  • the catch hook with its opening 36 of a lever arm, the bolt 20 and moves with its other lever arm facing away from the pivot wedge 16 by means of its extension 38 -.
  • FIG. 2 - Against the action of the spring 17 in a clockwise direction until the illustrated locked position is reached, are locked together in the spline 16 and fishing hooks 30 on the catching stage 29 of the pivoting wedge and the attacking there extension 38 of the fishing hook.
  • the hinged door is held in the position just taken, so is "trapped".
  • the linkage not shown by means of his hand lever - which has taken his normal position so far and is now moved to the closed position - the locking hook 31 about the bearing pin 19 with respect to Fig. 3 moved in a clockwise direction, so this now fully engages with its slot-shaped opening 39, the bolt 20 and locked while tightening the door in the door opening within the fuselage structure of the helicopter, this in the closed position.
  • the locking hook 31 carries, as already mentioned, at its free lever arm the bolt 43 with the ball head 42, which is in operative connection with said linkage for locking the door.

Landscapes

  • Lock And Its Accessories (AREA)

Claims (6)

  1. Serrure (10) pour portes d'hélicoptère, comportant un crochet de verrouillage (31) affecté à la structure de porte et un mentonnet (11) comportant un boulon (20), affecté à la structure du fuselage et disposé approximativement à angle droit vis-à-vis du crochet de verrouillage (31), moyennant quoi le crochet de verrouillage (31) peut être amené en liaison active avec le boulon (20) par une tringlerie actionnable manuellement après le déplacement de la porte en position de fermeture, pour tirer la porte dans l'ouverture de porte se trouvant dans la structure du fuselage lors du mouvement du crochet de verrouillage (31) en position de verrouillage et la verrouiller dans cette position ou inversement pour la débloquer en position de déverrouillage par un mouvement du crochet de verrouillage (31), caractérisée en ce qu'un crochet de retenue à ressort relié fonctionnellement au crochet de verrouillage est affecté à ce dernier (31), lequel crochet de retenue peut être mis en prise avec le boulon (20) avant l'entrée en effet du crochet de verrouillage (31) pour retenir la porte jusqu'à ce que la porte soit transférée dans sa position de fermeture définitive par un autre mouvement du crochet de verrouillage (31), dans laquelle le crochet de retenue (30) est à nouveau débloqué par la liaison active engrenée.
  2. Serrure selon la revendication 1, caractérisée en ce que le crochet de verrouillage (31) et le crochet de retenue (30) sont conçus sous forme de leviers à deux bras et sont montés équiaxialement au moyen d'un boulon de palier (19) sur une plaque de support (12), moyennant quoi les bras de levier faisant face au boulon (20) comportent des ouvertures en forme de crochet (39, 36) et sont conçus avec une longueur différente, tandis qu'une clavette pivotante (16) à ressort comportant une surface de clavette (28) et un épaulement de retenue (29) est affectée aux bras de levier opposés qui sont également de longueur différente, pour servir de liaison fonctionnelle engrenée.
  3. Serrure selon la revendication 2, caractérisée en ce que la clavette pivotante à ressort (16) est montée de manière à pouvoir pivoter sur la plaque de support (12) au moyen d'un boulon de palier (15), moyennant quoi le boulon de palier (15) est disposé de façon approximativement perpendiculaire au boulon de palier (19) des crochets de retenue et de verrouillage (30, 31).
  4. Serrure selon la revendication 2 ou 3, caractérisée en ce que la clavette pivotante (16) montée sur une courbure de la plaque de support (12) servant de flasque se dresse par un passage (24) dans la plaque de support (12) de façon approximativement orthogonale au plan de débattement des crochets de verrouillage et de retenue (31, 30).
  5. Serrure selon l'une quelconque des revendications 2 à 4, caractérisée en ce que la surface de clavette (26) et l'épaulement de retenue (29) de la clavette pivotante (16) sont situés sur sa surface active faisant face aux régions terminales des crochets de retenue et de verrouillage (30, 31), et en ce que la clavette pivotante (16), sollicitée par un ressort à torsion (17) dans le sens inverse des aiguilles d'une montre par rapport à son boulon de palier (15), bloque le crochet de retenue dans sa position dans laquelle le contact a été produit avec le doigt de butée (32) dès que l'épaulement de retenue est en liaison active avec un prolongement (38) du crochet de retenue (30).
  6. Serrure selon l'une quelconque des revendications précédentes, caractérisée en ce que l'extrémité dégagée de la plaque de support (12) faisant face au mentonnet (11) comporte une ouverture (22) en forme de fente, dont le bord arrière (23) sert de butée terminale pour la porte.
EP20070856019 2006-11-28 2007-11-26 Serrure pour portes d'aéronefs, en particulier d'hélicoptères Not-in-force EP2094924B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006056442A DE102006056442B4 (de) 2006-11-28 2006-11-28 Türschloss für Türen von Luftfahrzeugen, insbesondere von Hubschraubern
PCT/DE2007/002125 WO2008064650A2 (fr) 2006-11-28 2007-11-26 Serrure pour portes d'aéronefs, en particulier d'hélicoptères

Publications (2)

Publication Number Publication Date
EP2094924A2 EP2094924A2 (fr) 2009-09-02
EP2094924B1 true EP2094924B1 (fr) 2011-01-05

Family

ID=39338798

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20070856019 Not-in-force EP2094924B1 (fr) 2006-11-28 2007-11-26 Serrure pour portes d'aéronefs, en particulier d'hélicoptères

Country Status (6)

Country Link
US (1) US8360483B2 (fr)
EP (1) EP2094924B1 (fr)
CN (1) CN101600842B (fr)
AT (1) ATE494444T1 (fr)
DE (2) DE102006056442B4 (fr)
WO (1) WO2008064650A2 (fr)

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CN102337813A (zh) * 2011-08-23 2012-02-01 中国北方车辆研究所 一种车辆车门定位装置

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KR101372022B1 (ko) * 2012-08-24 2014-03-07 기아자동차주식회사 차량용 2단 가이드 후드 래치 장치
CN103603555B (zh) * 2013-08-23 2016-08-10 中国航空工业集团公司西安飞机设计研究所 一种舱门锁
DE102015000750A1 (de) * 2015-01-22 2016-07-28 D. la Porte Söhne GmbH Nah- und fernbetätigbares Fahrzeugtürschloss
EP3168138B1 (fr) * 2015-11-10 2018-06-06 Airbus Operations GmbH Ensemble porte d'aéronef
CN105502026B (zh) * 2015-11-26 2017-09-12 庆安集团有限公司 一种飞机集装系统的防滑出限动装置
CN106150243B (zh) * 2016-08-30 2018-01-05 中航沈飞民用飞机有限责任公司 一种民用飞机舱门锁定闩轴的提升锁定机构
CN107060545B (zh) * 2017-06-09 2018-08-17 河北天启通宇航空器材科技发展有限公司 舱门的锁紧机构及其报警系统

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CN102337813A (zh) * 2011-08-23 2012-02-01 中国北方车辆研究所 一种车辆车门定位装置

Also Published As

Publication number Publication date
DE502007006215D1 (de) 2011-02-17
WO2008064650A2 (fr) 2008-06-05
WO2008064650A3 (fr) 2008-08-21
CN101600842B (zh) 2012-06-27
DE102006056442B4 (de) 2010-10-28
CN101600842A (zh) 2009-12-09
US8360483B2 (en) 2013-01-29
EP2094924A2 (fr) 2009-09-02
ATE494444T1 (de) 2011-01-15
DE102006056442A1 (de) 2008-06-05
US20100064740A1 (en) 2010-03-18

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