EP2094923A2 - 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

Info

Publication number
EP2094923A2
EP2094923A2 EP07856018A EP07856018A EP2094923A2 EP 2094923 A2 EP2094923 A2 EP 2094923A2 EP 07856018 A EP07856018 A EP 07856018A EP 07856018 A EP07856018 A EP 07856018A EP 2094923 A2 EP2094923 A2 EP 2094923A2
Authority
EP
European Patent Office
Prior art keywords
door
catch
sliding
spring
locking device
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
EP07856018A
Other languages
German (de)
English (en)
Other versions
EP2094923B1 (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

Links

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

  • Locking device for sliding doors of aircraft in particular helicopters
  • 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, whose tumblers cooperating with fastenings attached to the fuselage structure can be actuated together by means of a suitable linkage having a handle.
  • 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 hindrance to entry into 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 known from DE 3 707 324 A1.
  • 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 based on the object to provide a new Matverriegelungsvor- direction, which is better while maintaining the locking security than previously operated.
  • a run guided by rails translationally operable sliding door with at least one detent engaging behind, designed as a rack lock latch this object is achieved according to the invention by the characterizing features of claim 1.
  • the new door lock is surprisingly advantageous.
  • Fangfaile which is in operative connection with the latch bolt, namely the affected, designed as a sliding door door in the position in which the latch is only in the area of the catch, "caught" before the lock catch comes into effect, so alone by further movement of the lock latch in the firing position, the door can be transferred to its final closed position, without the need for holding / tightening / pressing the door into the manual opening 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.
  • FIG. 1 is an isometric view of a specific for a sliding door of a helicopter locking device according to the invention in the tuck position
  • FIG. 2 shows the locking device of FIG. 1 in the unlocked position
  • Fig. 3 is a side view of the locking latch associated with the latch of the locking device of FIG. 1 catch in cooperation with a door catch fitting and
  • Fig. 4 the door catch fitting in isometric single view
  • a locking device for the sliding door not shown, of an aircraft, not shown, in particular a helicopter, is shown in Figs. 1 to 4, only one of the sliding door firmly connected to the locking devices 10.
  • the locking devices are actuated jointly by a handrail, which is likewise not shown, and in each case interact with a fitting 12 having a catch 11 attached to the fuselage structure of the aircraft.
  • 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 1 1 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 supporting pin 15 of the apparent from Fig. 3 rack bar 26 is used.
  • the free end 15a of the pin 15 of the rack bolt 26 of the laterally spaced from the fuselage structure guided by guide rails sliding door is attached to the fuselage structure on the rear door frame profile door catch fitting 20.

Landscapes

  • Lock And Its Accessories (AREA)
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 true EP2094923A2 (fr) 2009-09-02
EP2094923B1 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
WO2019123454A1 (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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2008064649A2 *

Also Published As

Publication number Publication date
WO2008064649A2 (fr) 2008-06-05
WO2008064649A3 (fr) 2008-08-14
DE102006056441B4 (de) 2010-06-02
EP2094923B1 (fr) 2010-04-28
US20100064741A1 (en) 2010-03-18
DE502007003632D1 (de) 2010-06-10
US8146864B2 (en) 2012-04-03
ATE466156T1 (de) 2010-05-15
RU2009119722A (ru) 2011-01-10
DE102006056441A1 (de) 2008-05-29
RU2413826C2 (ru) 2011-03-10

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