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EP2094923B1 - Dispositif de verrouillage pour portes coulissantes d'aéronefs, en particulier d'hélicoptères - Google Patents

Dispositif de verrouillage pour portes coulissantes d'aéronefs, en particulier d'hélicoptères Download PDF

Info

Publication number
EP2094923B1
EP2094923B1 EP20070856018 EP07856018A EP2094923B1 EP 2094923 B1 EP2094923 B1 EP 2094923B1 EP 20070856018 EP20070856018 EP 20070856018 EP 07856018 A EP07856018 A EP 07856018A EP 2094923 B1 EP2094923 B1 EP 2094923B1
Authority
EP
European Patent Office
Prior art keywords
door
catch
latch
sliding
spring
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
EP20070856018
Other languages
German (de)
English (en)
Other versions
EP2094923A2 (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 EP2094923A2 publication Critical patent/EP2094923A2/fr
Application granted granted Critical
Publication of EP2094923B1 publication Critical patent/EP2094923B1/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
    • E05B79/00—Mounting or connecting vehicle locks or parts thereof
    • E05B79/10—Connections between movable lock parts
    • E05B79/20—Connections between movable lock parts using flexible connections, e.g. Bowden cables
    • 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
    • Y10T70/5173—Sliding door
    • Y10T70/519—Projecting or extending bolt

Definitions

  • the invention relates to a locking device for sliding doors of aircraft, in particular of helicopters according to the preamble of claim 1.
  • sliding doors are, similar to land vehicles, laterally guided laterally along the outer surface of the fuselage structure over lateral guide rails to the height of the door opening and then suitably bent ends of the guide rails in the door opening drawn.
  • the sliding door is to be moved by hand and also to lock in the closed position by hand.
  • the doors provided there within the openings provided in the fuselage structure must be securely entrenched and closed. The closure of such sliding doors therefore requires three consecutive manual operations, namely closing the door, holding the door in this state and then locking it.
  • At least two door locks are connected to the door structure, the tumblers cooperating with fastened to the hull structure fittings can be actuated together via a suitable handle having a linkage. It is therefore necessary when closing such doors for the last two operations special skill, since the respective door is to hold firmly when locking in the closed position. If the door has not been pushed closed enough, it can happen that one or the other lock is "in the void" and therefore the affected door is not properly closed. As a rule, both hands of the person concerned are therefore required for closing the door.
  • 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 door locking system for a helicopter door with a translationally movable locking system is from the DE 3 707 324 A1 known.
  • a disadvantage here proves to be that the helicopter door is locked when locking in the closed position, so that both hands are required to close the door.
  • a so-called flap door is known, which assumes a pre-locked position during a closing movement and before reaching the final closed position.
  • the invention is therefore an object of the invention to provide a new door lock device that is better than previously operated while maintaining the security lock.
  • the new door lock is surprisingly advantageous.
  • the catch catch according to the invention which is in geared engagement with the latch, namely the affected, designed as a sliding door door in the position in which the latch is only in the catch, "caught", so alone by further moving the latch in the firing position, the door can be moved to its final closed position, without the need for holding / tightening the door in the manual opening provided in the fuselage structure.
  • the latch in its final closed position by means of said handle is released via the geared connection between catch and latch, which is inventively designed as a sliding wedge, the catch for a new closing operation.
  • the inventive design of the door lock facilitates the safe closing of such sliding doors considerably and therefore significantly increases the ease of use for the crew of a helicopter. Also, the ergonomic requirements for the flight crew during flight of the helicopter with open sliding doors for sliding the door in flight are significantly reduced.
  • a locking device for the sliding door, not shown, of an aircraft also not shown, in particular a helicopter is in the Fig. 1 to 4 only one of the locking device 10 fixedly connected to the sliding door is shown.
  • the locking devices are operated together via a likewise not shown a hand lever exhibiting linkage and each cooperate with a fixed to the fuselage structure of the aircraft a detent 11 having fitting 12 together.
  • a rack bolt 26 is connected, at the effective end of which is mounted on a spring 15 acted upon in the axial direction by a spring 15 pin 16, the sliding door can be locked.
  • the roller 16 engages behind the detent 11 of the attached to the hull structure also not shown fitting 12, which is located on the rear frame profile of the sliding door guide, also not shown.
  • the free end 15a of the roller 16 overlying pin 15 of the serves Fig. 3 apparent rack bolt 26.

Landscapes

  • Lock And Its Accessories (AREA)

Claims (4)

  1. Dispositif de verrouillage pour portes coulissantes d'hélicoptère, actionnables en translation sur des rails de guidage, comportant un verrou à crémaillère (26) affecté à la structure de la porte et un taquet d'enclenchement (11) affecté à la structure de fuselage, qui peut être mis en prise avec le verrou à crémaillère (26), dès que le verrou à crémaillère (26) est déplacé par une tringlerie actionnable manuellement en position de fermeture dans laquelle la porte est tirée dans l'ouverture de porte se trouvant dans la structure du fuselage et est bloquée dans cette position ou est débloquée par un mouvement du verrou à crémaillère (26) en position de déverrouillage, caractérisé en ce qu'un loquet de capture à ressort (15a) relié fonctionnellement au verrou à crémaillère (26) par l'intermédiaire d'un coulisseau à ressort (22) est affecté au verrou à crémaillère, lequel loquet de capture pouvant être mis en prise avec le coulisseau (22) avant l'entrée en effet du verrou à crémaillère (26) pour capturer la porte coulissante au moyen du coulisseau (22) logé dans une ferrure de capture de la porte (20), et le loquet de capture (15a) peut être à nouveau déverrouillé dans sa position de fermeture définitive par un autre mouvement de la porte coulissante.
  2. Dispositif de verrouillage pour porte selon la revendication 1,
    caractérisé en ce que le coulisseau à ressort (22) servant de liaison fonctionnelle entre le loquet de capture (15a) et le loquet de fermeture (13) comporte à sa surface faisant face au loquet de capture un biseau de capture (23) et, sur sa surface latérale orientée vers le loquet de capture (15a), un biseau d'ouverture (24), et est maintenu par un ressort en appui avec la surface latérale (27) orientée vers le loquet de capture (15a) de la ferrure de capture de porte (20).
  3. Dispositif de verrouillage pour porte selon l'une quelconque des revendications 1 et 2,
    caractérisé en ce que la broche (15) du loquet de fermeture (13) logée de manière mobile, portant la molette (16), est contrainte par un ressort (14) dans le sens axial.
  4. Dispositif de verrouillage pour porte selon l'une quelconque des revendications 1 à 3,
    caractérisé en ce qu'en ouvrant la porte coulissante, par l'intermédiaire de l'extrémité libre (15a) de la broche (15) agissant comme un loquet de capture, étant en interaction avec le biseau d'ouverture (24), le coulisseau à ressort (22) est mobile dans la trajectoire de déplacement de la porte coulissante et le mouvement d'ouverture peut être ainsi débloqué.
EP20070856018 2006-11-28 2007-11-26 Dispositif de verrouillage pour portes coulissantes d'aéronefs, en particulier d'hélicoptères Not-in-force EP2094923B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006056441A DE102006056441B4 (de) 2006-11-28 2006-11-28 Verriegelungsvorrichtung für Schiebetüren von Hubschraubern
PCT/DE2007/002124 WO2008064649A2 (fr) 2006-11-28 2007-11-26 Dispositif de verrouillage pour portes coulissantes d'aéronefs, en particulier d'hélicoptères

Publications (2)

Publication Number Publication Date
EP2094923A2 EP2094923A2 (fr) 2009-09-02
EP2094923B1 true EP2094923B1 (fr) 2010-04-28

Family

ID=39326458

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20070856018 Not-in-force EP2094923B1 (fr) 2006-11-28 2007-11-26 Dispositif de verrouillage pour portes coulissantes d'aéronefs, en particulier d'hélicoptères

Country Status (6)

Country Link
US (1) US8146864B2 (fr)
EP (1) EP2094923B1 (fr)
AT (1) ATE466156T1 (fr)
DE (2) DE102006056441B4 (fr)
RU (1) RU2413826C2 (fr)
WO (1) WO2008064649A2 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9604713B2 (en) * 2013-10-22 2017-03-28 Bell Helicopter Textron Inc. Door migration prevention system
EP3045386B1 (fr) 2015-01-14 2018-06-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Agencement pour déplacer une porte dans des mouvements pivotant et de coulissement
CN105002646B (zh) * 2015-08-13 2017-05-24 广东溢达纺织有限公司 门锁
AT519593B1 (de) 2017-01-18 2019-05-15 Facc Ag Verriegelungsvorrichtung
CA3086333A1 (fr) 2017-12-18 2019-06-27 Pegasus Integrated Solutions Ltd. Nouveau verrou
US11220852B2 (en) 2019-05-02 2022-01-11 Textron Innovations Inc. Aircraft having versatile door systems
RU2757608C1 (ru) * 2020-12-30 2021-10-19 Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") Распашная дверь с телескопическим подкосом открытого положения
RU2762465C1 (ru) * 2021-03-30 2021-12-21 Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") Запорное устройство двери кабины
USD1038743S1 (en) * 2021-12-27 2024-08-13 Klein Iberica, S.A.U. Holding device for sliding doors
CN114165124A (zh) * 2021-12-31 2022-03-11 湖南宏工智能科技有限公司 一种用于犁刀混合机观察窗的锁扣组件
CN114537639B (zh) * 2022-03-24 2024-07-23 山西汾西重工有限责任公司 可快速拆卸的舱口盖及航行器

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3210924A1 (de) 1982-03-25 1983-09-29 Fichtel & Sachs Ag, 8720 Schweinfurt Sperreinrichtung fuer das stellorgan eines stellelementes, insbesondere fuer zentral-verriegelungs-einrichtung an kraftfahrzeugen
US4593945A (en) 1984-03-14 1986-06-10 The Stanley Works Oven latch assembly
DE3707324A1 (de) * 1987-03-07 1988-09-15 Messerschmitt Boelkow Blohm Tuerverriegelungssystem
US5259576A (en) * 1992-05-18 1993-11-09 Howard D U External sliding aircraft door
DE9311255U1 (de) * 1993-07-28 1994-12-01 Ed. Scharwächter GmbH + Co KG, 42855 Remscheid Türschließeinrichtung für Kraftwagentüren
US6325428B1 (en) * 1999-11-10 2001-12-04 Hartwell Corporation Latch assembly including sensor
DE10360484A1 (de) * 2003-12-22 2005-07-28 Airbus Deutschland Gmbh Flugzeugtor

Also Published As

Publication number Publication date
DE102006056441B4 (de) 2010-06-02
DE102006056441A1 (de) 2008-05-29
ATE466156T1 (de) 2010-05-15
DE502007003632D1 (de) 2010-06-10
US8146864B2 (en) 2012-04-03
EP2094923A2 (fr) 2009-09-02
US20100064741A1 (en) 2010-03-18
RU2413826C2 (ru) 2011-03-10
RU2009119722A (ru) 2011-01-10
WO2008064649A3 (fr) 2008-08-14
WO2008064649A2 (fr) 2008-06-05

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