EP2724929A1 - Device for shock-proof door or porthole assembly on naval ships - Google Patents

Device for shock-proof door or porthole assembly on naval ships Download PDF

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Publication number
EP2724929A1
EP2724929A1 EP13003957.1A EP13003957A EP2724929A1 EP 2724929 A1 EP2724929 A1 EP 2724929A1 EP 13003957 A EP13003957 A EP 13003957A EP 2724929 A1 EP2724929 A1 EP 2724929A1
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EP
European Patent Office
Prior art keywords
frame
locking
wing
adjustable
sash
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
EP13003957.1A
Other languages
German (de)
French (fr)
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EP2724929B1 (en
Inventor
Rainer Karallus
Jörg DRAEGER
Wolfram Determann
Gerardo Salazar
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.)
ThyssenKrupp Marine Systems GmbH
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ThyssenKrupp Marine Systems GmbH
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Publication date
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Priority to PL13003957T priority Critical patent/PL2724929T3/en
Publication of EP2724929A1 publication Critical patent/EP2724929A1/en
Application granted granted Critical
Publication of EP2724929B1 publication Critical patent/EP2724929B1/en
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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05CBOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C3/00Fastening devices with bolts moving pivotally or rotatively
    • E05C3/12Fastening devices with bolts moving pivotally or rotatively with latching action
    • E05C3/14Fastening devices with bolts moving pivotally or rotatively with latching action with operating handle or equivalent member rigid with the latch
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B19/00Arrangements or adaptations of ports, doors, windows, port-holes, or other openings or covers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B19/00Arrangements or adaptations of ports, doors, windows, port-holes, or other openings or covers
    • B63B19/12Hatches; Hatchways
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B43/00Improving safety of vessels, e.g. damage control, not otherwise provided for
    • B63B43/24Arrangements of watertight doors in bulkheads
    • B63B43/32Arrangements of watertight doors in bulkheads of non-sliding type
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B17/00Accessories in connection with locks
    • E05B17/20Means independent of the locking mechanism for preventing unauthorised opening, e.g. for securing the bolt in the fastening position
    • E05B17/2007Securing, deadlocking or "dogging" the bolt in the fastening position
    • E05B17/203Securing, deadlocking or "dogging" the bolt in the fastening position not following the movement of the bolt
    • E05B17/2038Securing, deadlocking or "dogging" the bolt in the fastening position not following the movement of the bolt moving rectilinearly
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B51/00Operating or controlling locks or other fastening devices by other non-mechanical means
    • E05B51/02Operating or controlling locks or other fastening devices by other non-mechanical means by pneumatic or hydraulic means
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B63/00Locks or fastenings with special structural characteristics
    • E05B63/0052Locks mounted on the "frame" cooperating with means on the "wing"
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05CBOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C19/00Other devices specially designed for securing wings, e.g. with suction cups
    • E05C19/001Other devices specially designed for securing wings, e.g. with suction cups with bolts extending over a considerable extent, e.g. nearly along the whole length of at least one side of the wing
    • EFIXED CONSTRUCTIONS
    • E06DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06BFIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00Window 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
    • E06B3/32Arrangements 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
    • E06B3/34Arrangements 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 with only one kind of movement
    • EFIXED CONSTRUCTIONS
    • E06DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06BFIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B5/00Doors, windows, or like closures for special purposes; Border constructions therefor
    • E06B5/10Doors, windows, or like closures for special purposes; Border constructions therefor for protection against air-raid or other war-like action; for other protective purposes
    • E06B5/12Doors, windows, or like closures for special purposes; Border constructions therefor for protection against air-raid or other war-like action; for other protective purposes against air pressure, explosion, or gas

Definitions

  • the invention relates to a device for shock-proof door or hatch arrangement on naval ships, wherein in a frame hinges pivotally arranged wing in the closed position is receivable and the wing with the frame with the involvement of seals by adjustable via a handle interlocking corresponding locking elements for fixing the wing in the frame for a locking position.
  • the object of the invention is to provide a training for a claimable by shock load standing door, which ensures unintentional popping and also allows remote controlled door opening and closing.
  • the frame has on two opposite longitudinal sides continuous locking strips as locking elements which are receivable in corresponding grooves of a sash, wherein the pivotally connected to the frame side of the wing a stationary locking bar for engaging in the groove of the Sash has at a closing movement of the wing and on the opposite side of an adjustable locking bar in the frame is guided, which can be inserted via adjusting elements in the closed position of the wing in a groove of the sash.
  • a simple control is that the adjusting elements for the locking bar are formed by pneumatic cylinders and / or pivotable actuating lever.
  • the adjustable locking bar has a parallel associated safety bar in the frame, which is arranged via an associated actuating lever vertically adjustable to the locking bar.
  • the securing rod is formed in a region as a rack, in which a corresponding toothed element of the pivot axis of the actuating lever engages for adjustment.
  • the profiles of the sash frame associated with the frame have a chamfer in the region of the associated locking strips for feeding into the groove.
  • pivotable actuating lever act via a Kochtotrioslagerung in the locked position via bolts on the locking bar.
  • the outer surfaces of the wing and the frame have corresponding, in the closed position against each other supporting, attachment elements as a shock limiter.
  • a wing 1 as a door element via hinges 2 is pivotally connected to close an opening 3 on a fixedly connected to a bulkhead 4 frame 5.
  • a pneumatic actuating cylinder associated with the wing 1 to make a remote control via an electropneumatic control.
  • the frame 5 on the hinge side with the connected side of the wing 1 has a stationary locking bar 6 for engagement or insertion in a corresponding groove 7 of a sash 8, wherein the profile of the sash 8 has a chamfer for feeding the locking bar 6 in the groove 7 ,
  • a covering outer region of the casement 8 has a seal 9, which rests against the frame 5 in the closed state of the wing 1.
  • the stationary locking bar 6 is adjustably arranged in the frame 5.
  • the frame 5 on the opposite side has a guided in the frame 5 and adjustable locking bar 10 which is inserted via a pneumatic cylinder 11 and pivotally arranged actuating lever 12 in a corresponding groove 13 of the sash 8 for locking and is held in this locking position.
  • the pneumatic cylinder 11 and the actuating lever 12 thereby engage via bolts 14 on the locking bar 10, wherein the pivoted actuating lever 12 are held in the locking position via a Studentstotddlinglagerung.
  • a parallel securing rod 17 is arranged in the frame 5, which prevents a locking of the locking bar in the region of the guide 15 after locking of the wing 1 in its closed position.
  • the vertical displacement is adjustable via an actuating lever 16, wherein securing rod 17 is formed in the engagement region of the actuating lever 16 as a rack 18, in which engages a corresponding tooth element of the pivot axis of the actuating lever 16 for adjustment.
  • abutting attachment elements 20 and 21 are applied, which serve as a shock limiter.

Abstract

The marine ship has a leaf (1) that is received in a trim (5) in closing position and pivoted over hinges. Two longitudinal sides of trim have locking elements engaged in corresponding grooves of a wing frame. A stationary locking lath in side of leaf is pivotally connected with trim, for engaging with groove during closing movement of leaf. An adjustable locking lath is guided in trim and inserted into groove over position elements (12) in closing position of leaf. A parallel backup bar of adjustable locking lath is arranged vertically in the trim over operation lever.

Description

Die Erfindung bezieht sich auf eine Vorrichtung zur schocksicheren Tür- oder Lukenanordnung auf Marineschiffen, wobei in einer Zarge ein über Scharniere verschwenkbar angeordneter Flügel in der Schließstellung aufnehmbar ist und der Flügel mit der Zarge unter Einschaltung von Dichtungen durch über eine Handhabe einstellbare ineinander greifende korrespondierende Verriegelungselemente zur Fixierung des Flügels in der Zarge für eine Verriegelungsposition aufweist.The invention relates to a device for shock-proof door or hatch arrangement on naval ships, wherein in a frame hinges pivotally arranged wing in the closed position is receivable and the wing with the frame with the involvement of seals by adjustable via a handle interlocking corresponding locking elements for fixing the wing in the frame for a locking position.

Bei derartigen Anordnungen auf Marineschiffen besteht die Schwierigkeit, die Kräfte aus Schockereignissen in die Zarge überzuleiten, um ein unbeabsichtigtes Aufspringen im Schockfall zu verhindern.With such arrangements on naval ships, there is the difficulty of transferring the forces from shock events into the frame in order to prevent unintended popping in the event of shock.

Hierzu ist es bereits bekannt, gemäß DE 10 2006 041 141 B3 eine Verriegelung zwischen Flügel und Zarge über eine Vielzahl über den Umfang verteilte korrespondierende Laschen über verschiebbare Gestängeelemente vorzunehmen und einen geschlossenen umlaufenden Betätigungsring über Kugelelemente in Eckbereichen zu bilden. Die Schwierigkeiten bestehen hierbei in der Betätigung durch zusätzliche fernsteuerbare Handhabung und der Gefahr, dass nach Schockbeanspruchung Gestänge nicht mehr ordnungsgemäß handhabbar sind.For this it is already known, according to DE 10 2006 041 141 B3 to perform a locking between the wing and frame over a plurality of distributed over the circumference corresponding tabs on sliding linkage elements and a closed circumferential actuating ring over To form ball elements in corner areas. The difficulties here are in the operation by additional remote controllable handling and the risk that after shock stress linkage are no longer properly handled.

Die Aufgabe der Erfindung besteht darin, eine Ausbildung für eine stark durch Schockbelastung beanspruchbare Standkrafttür zu schaffen, die ein unbeabsichtigtes Aufspringen gewährleistet und auch eine fernsteuerbare Türöffnung und -schließung ermöglicht.The object of the invention is to provide a training for a claimable by shock load standing door, which ensures unintentional popping and also allows remote controlled door opening and closing.

Die Lösung dieser Aufgabe erfolgt erfindungsgemäß dadurch, dass die Zarge an zwei sich gegenüberliegenden Längsseiten durchgehende Verriegelungsleisten als Verriegelungselemente aufweist, die in korrespondierende Nuten eines Flügelrahmens aufnehmbar sind, wobei die mit der Zarge verschwenkbar verbundene Seite des Flügels eine ortsfeste Verriegelungsleiste zum Eingreifen in die Nut des Flügelrahmens bei einer Schließbewegung des Flügels aufweist und an der gegenüberliegenden Seite eine in der Zarge verstellbare Verriegelungsleiste geführt ist, die über Stellelemente in der Schließstellung des Flügels in eine Nut des Flügelrahmens einsetzbar ist.The solution of this object is achieved according to the invention in that the frame has on two opposite longitudinal sides continuous locking strips as locking elements which are receivable in corresponding grooves of a sash, wherein the pivotally connected to the frame side of the wing a stationary locking bar for engaging in the groove of the Sash has at a closing movement of the wing and on the opposite side of an adjustable locking bar in the frame is guided, which can be inserted via adjusting elements in the closed position of the wing in a groove of the sash.

Durch diese Anordnung ist eine Zuordnung der einzelnen Elemente mit relativ geringem Spiel möglich und eine durchgehende Aufnahme von auftretenden Schockbelastungen ohne Beeinträchtigungen gewährleistet.By this arrangement, an assignment of the individual elements with relatively little play is possible and ensures a continuous recording of shocks occurring without adverse effects.

Eine einfache Ansteuerung besteht darin, dass die Stellelemente für die Verriegelungsleiste durch Pneumatikzylinder und/oder verschwenkbare Betätigungshebel gebildet sind.A simple control is that the adjusting elements for the locking bar are formed by pneumatic cylinders and / or pivotable actuating lever.

Weiterhin wird zur Sicherung und Vermeidung einer Verschiebung in der Schließstellung vorgeschlagen, dass die verstellbare Verriegelungsleiste eine parallel zugeordnete Sicherungsstange in der Zarge aufweist, die über eine zugeordneten Betätigungshebel vertikal zur Verriegelungsleiste verstellbar angeordnet ist. Hierbei ist zusätzlich vorgesehen, dass die Sicherungsstange in einem Bereich als Zahnstange ausgebildet ist, in die ein korrespondierendes Zahnelement der Schwenkachse des Betätigungshebels zur Verstellung eingreift.Furthermore, it is proposed for securing and avoiding a shift in the closed position, that the adjustable locking bar has a parallel associated safety bar in the frame, which is arranged via an associated actuating lever vertically adjustable to the locking bar. Here, it is additionally provided that the securing rod is formed in a region as a rack, in which a corresponding toothed element of the pivot axis of the actuating lever engages for adjustment.

Um ein geringes Spiel zwischen Flügel und Zarge zu ermöglichen, ist vorgesehen, dass die der Zarge zugeordneten Profile des Flügelrahmens eine Abschrägung im Bereich der zugeordneten Verriegelungsleisten zur Zuführung in die Nut aufweisen.In order to allow a slight clearance between the sash and the frame, it is provided that the profiles of the sash frame associated with the frame have a chamfer in the region of the associated locking strips for feeding into the groove.

Ferner ist vorteilhaft, dass die verschwenkbaren Betätigungshebel über eine Übertotpunktlagerung in der Verriegelungsposition über Bolzen auf die Verriegelungsleiste einwirken.It is also advantageous that the pivotable actuating lever act via a Übertotpunktlagerung in the locked position via bolts on the locking bar.

Als zusätzliche Sicherung ist vorgesehen, dass die aussenliegenden Flächen von Flügel und Zarge korrespondierende, in der Schliessposition sich gegeneinander abstützende, Aufsatzelemente als Schockbegrenzer aufweisen.As an additional safeguard, it is provided that the outer surfaces of the wing and the frame have corresponding, in the closed position against each other supporting, attachment elements as a shock limiter.

In der Zeichnung ist ein Ausführungsbeispiel der Erfindung schematisch dargestellt. Es zeigen:

Fig. 1
eine Gesamtdarstellung einer Türanordnung in geöffneter Position;
Fig. 2
eine Darstellung wie Fig. 1 in geschlossener Position mit einem zusätzlichen Stellzylinder zum Öffnen und Schließen;
Fig. 3
eine Darstellung einer verstellbaren Verriegelungsleiste;
Fig. 4
eine Seitenansicht als Schnitt der Zarge mit den Stellelementen für die verstellbare Verriegelungsleiste;
Fig. 5
eine verkürzte Schnittdarstellung gemäß Linie V-V der Fig. 2 mit den Verriegelungsleisten in einer Verriegelungsposition;
Fig. 6
eine Perspektivdarstellung einer verstellbaren Verriegelungsleiste mit seinen Stellelementen und einer Seilzugstange;
Fig. 7
eine vergrößerte Darstellung eines Teilbereiches gemäß Fig. 6 und
Fig. 8
einen verstellbaren Betätigungshebel für eine verstellbare Verriegelungsleiste
In the drawing, an embodiment of the invention is shown schematically. Show it:
Fig. 1
an overall view of a door assembly in the open position;
Fig. 2
a representation like Fig. 1 in the closed position with an additional actuating cylinder for opening and closing;
Fig. 3
an illustration of an adjustable locking bar;
Fig. 4
a side view as a section of the frame with the adjusting elements for the adjustable locking bar;
Fig. 5
a shortened sectional view according to line VV of Fig. 2 with the locking strips in a locking position;
Fig. 6
a perspective view of an adjustable locking bar with its adjusting elements and a cable pull rod;
Fig. 7
an enlarged view of a portion according to Fig. 6 and
Fig. 8
an adjustable operating lever for an adjustable locking strip

Bei der dargestellten Anordnung ist ein Flügel 1 als Türelement über Scharniere 2 schwenkbar zum Verschließen einer Öffnung 3 an einer mit einem Schott 4 ortsfest zugeordneten Zarge 5 verbunden. Für die Stellbewegung ist gemäß Fig. 2 ein pneumatischer Stellzylinder dem Flügel 1 zugeordnet, um über eine elektropneumatische Steuerung eine Fernsteuerung vorzunehmen.In the illustrated arrangement, a wing 1 as a door element via hinges 2 is pivotally connected to close an opening 3 on a fixedly connected to a bulkhead 4 frame 5. For the adjusting movement is according to Fig. 2 a pneumatic actuating cylinder associated with the wing 1 to make a remote control via an electropneumatic control.

Die Zarge 5 an der Scharnierseite mit der verbundenen Seite des Flügels 1 besitzt eine ortsfeste Verriegelungsleiste 6 zum Eingriff bzw. Einsetzen in eine korrespondierende Nut 7 eines Flügelrahmens 8, wobei das Profil des Flügelrahmens 8 eine Abschrägung zur Zuführung der Verriegelungsleiste 6 in die Nut 7 aufweist. Ein überdeckender Außenbereich des Flügelrahmens 8 besitzt eine Dichtung 9, die an der Zarge 5 in geschlossenem Zustand des Flügels 1 anliegt. Die ortsfeste Verriegelungsleiste 6 ist dabei justierbar in der Zarge 5 angeordnet.The frame 5 on the hinge side with the connected side of the wing 1 has a stationary locking bar 6 for engagement or insertion in a corresponding groove 7 of a sash 8, wherein the profile of the sash 8 has a chamfer for feeding the locking bar 6 in the groove 7 , A covering outer region of the casement 8 has a seal 9, which rests against the frame 5 in the closed state of the wing 1. The stationary locking bar 6 is adjustably arranged in the frame 5.

Die Zarge 5 an der gegenüberliegenden Seite besitzt dagegen eine in der Zarge 5 geführte und verstellbare Verriegelungsleiste 10, die über einen Pneumatikzylinder 11 und verschwenkbare angeordnete Betätigungshebel 12 in eine korrespondierende Nut 13 des Flügelrahmens 8 zur Verriegelung einsetzbar ist und in dieser Verriegelungsstellung gehalten wird. Die Pneumatikzylinder 11 und die Betätigungshebel 12 greifen dabei über Bolzen 14 an der Verriegelungsleiste 10 an, wobei die verschwenkten Betätigungshebel 12 über eine Übertotpunktlagerung in der Verriegelungsposition gehalten sind.The frame 5 on the opposite side, however, has a guided in the frame 5 and adjustable locking bar 10 which is inserted via a pneumatic cylinder 11 and pivotally arranged actuating lever 12 in a corresponding groove 13 of the sash 8 for locking and is held in this locking position. The pneumatic cylinder 11 and the actuating lever 12 thereby engage via bolts 14 on the locking bar 10, wherein the pivoted actuating lever 12 are held in the locking position via a Übertotpunktlagerung.

Gemäß Fig. 7 ist parallel zur verstellbaren Verriegelungsleiste 6 eine parallele Sicherungsstange 17 in der Zarge 5 angeordnet, die nach Verriegelung des Flügels 1 in ihrer Schließstellung eine Verschiebung der Verriegelungsleiste im Bereich der Führung 15 verhindert. Die Vertikalverschiebung ist über einen Betätigungshebel 16 einstellbar, wobei Sicherungsstange 17 im Angriffsbereich des Betätigungshebels 16 als Zahnstange 18 ausgebildet ist, in die ein korrespondierendes Zahnelement der Schwenkachse des Betätigungshebels 16 zur Verstellung eingreift.According to Fig. 7 is parallel to the adjustable locking bar 6 a parallel securing rod 17 is arranged in the frame 5, which prevents a locking of the locking bar in the region of the guide 15 after locking of the wing 1 in its closed position. The vertical displacement is adjustable via an actuating lever 16, wherein securing rod 17 is formed in the engagement region of the actuating lever 16 as a rack 18, in which engages a corresponding tooth element of the pivot axis of the actuating lever 16 for adjustment.

Zusätzlich sind an den außenliegenden Flächen von Flügel 1 und Zarge 5 in der Schließposition gegeneinanderstoßende Aufsatzelemente 20 und 21 aufgebracht, die als Schockbegrenzer dienen.In addition, against the outer surfaces of the wing 1 and frame 5 in the closed position abutting attachment elements 20 and 21 are applied, which serve as a shock limiter.

Claims (7)

Vorrichtung zur schocksicheren Tür- oder Lukenanordnung auf Marineschiffen, wobei in einer Zarge ein über Scharniere verschwenkbar angeordneter Flügel in der Schließstellung aufnehmbar ist und der Flügel mit der Zarge unter Einschaltung von Dichtungen durch über eine Handhabe einstellbare ineinander greifende korrespondierende Verriegelungselemente zur Fixierung des Flügels in der Zarge für eine Verriegelungsposition aufweist, dadurch gekennzeichnet, dass die Zarge (5) an zwei sich gegenüberliegenden Längsseiten durchgehende Verriegelungsleisten (6, 10) als Verriegelungselemente aufweist, die in korrespondierende Nuten (7, 13) eines Flügelrahmens (8) aufnehmbar sind, wobei die mit der Zarge (5) verschwenkbar verbundene Seite des Flügels (1) eine ortsfeste Verriegelungsleiste (6) zum Eingreifen in die Nut (7) des Flügelrahmens (8) bei einer Schließbewegung des Flügels (1) aufweist und an der gegenüberliegenden Seite eine in der Zarge (5) verstellbare Verriegelungsleiste (10) geführt ist, die über Stellelemente (11, 12) in der Schließstellung des Flügels (1) in eine Nut (13) des Flügelrahmens (8) einsetzbar ist.Device for shock-proof door or hatch arrangement on naval ships, wherein in a frame hinges pivotally arranged wings in the closed position is receivable and the wing with the frame with the involvement of seals by adjustable via a handle interlocking corresponding locking elements for fixing the wing in the Having a frame for a locking position, characterized in that the frame (5) on two opposite longitudinal sides continuous locking strips (6, 10) as locking elements, which in corresponding grooves (7, 13) of a sash (8) are receivable, wherein the with the frame (5) pivotally connected side of the wing (1) has a fixed locking strip (6) for engaging in the groove (7) of the sash (8) in a closing movement of the wing (1) and on the opposite side in the Frame (5) adjustable locking strip (10) is guided, which can be inserted via adjusting elements (11, 12) in the closed position of the wing (1) in a groove (13) of the sash (8). Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Stellelemente (11, 12) für die Verriegelungsleiste (10) durch Pneumatikzylinder und/oder verschwenkbare Betätigungshebel gebildet sind.Apparatus according to claim 1, characterized in that the adjusting elements (11, 12) for the locking strip (10) are formed by pneumatic cylinders and / or pivotable actuating lever. Vorrichtung nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, dass die verstellbare Verriegelungsleiste (10) eine parallel zugeordnete Sicherungsstange (17) in der Zarge (5) aufweist, die über eine zugeordneten Betätigungshebel (16) vertikal zur Verriegelungsleiste (10) verstellbar angeordnet ist.Device according to one of claims 1 or 2, characterized in that the adjustable locking strip (10) has a parallel associated securing rod (17) in the frame (5), which arranged via an associated actuating lever (16) vertically to the locking bar (10) adjustable is. Vorrichtung nach Anspruch 3, dadurch gekennzeichnet, dass die Sicherungsstange (17) in einem Bereich als Zahnstange (18) ausgebildet ist, in die ein korrespondierendes Zahnelement der Schwenkachse des Betätigungshebels (16) zur Verstellung eingreift.Apparatus according to claim 3, characterized in that the securing rod (17) is formed in a region as a rack (18), in which engages a corresponding tooth element of the pivot axis of the actuating lever (16) for adjustment. Vorrichtung nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass die der Zarge (5) zugeordneten Profile des Flügelrahmens (8) eine Abschrägung im Bereich der zugeordneten Verriegelungsleisten (6, 10) zur Zuführung in die Nut (7, 13) aufweisen.Device according to one of claims 1 to 4, characterized in that the frame (5) associated profiles of the sash (8) have a chamfer in the region of the associated locking strips (6, 10) for feeding into the groove (7, 13). Vorrichtung nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass die verschwenkbaren Betätigungshebel (12) über eine Übertotpunktlagerung in der Verriegelungsposition über Bolzen (14) auf die Verriegelungsleiste (10) einwirken.Device according to one of claims 1 to 5, characterized in that the pivotable actuating lever (12) via a Übertotpunktlagerung in the locking position via bolts (14) acting on the locking bar (10). Vorrichtung nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass die aussenliegenden Flächen von Flügel (1) und Zarge (5) korrespondierende, in der Schliessposition sich gegeneinander abstützende, Aufsatzelemente (20, 21) als Schockbegrenzer aufweisen.Device according to one of claims 1 to 6, characterized in that the outer surfaces of wing (1) and frame (5) corresponding, in the closing position against each other supporting, attachment elements (20, 21) have as a shock limiter.
EP13003957.1A 2012-10-23 2013-08-08 Device for shock-proof door or porthole assembly on naval ships Active EP2724929B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL13003957T PL2724929T3 (en) 2012-10-23 2013-08-08 Device for shock-proof door or porthole assembly on naval ships

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102012021583 2012-10-23

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EP2724929A1 true EP2724929A1 (en) 2014-04-30
EP2724929B1 EP2724929B1 (en) 2017-11-08

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US (1) US8984812B2 (en)
EP (1) EP2724929B1 (en)
KR (1) KR101832009B1 (en)
AU (1) AU2013245574B2 (en)
BR (1) BR102013026598B1 (en)
CA (1) CA2830060C (en)
DE (1) DE102013016963A1 (en)
ES (1) ES2657045T3 (en)
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US9726288B2 (en) * 2014-04-29 2017-08-08 Eminent Technologies, Llc Pressure vessel closure
CN108222788A (en) * 2018-02-06 2018-06-29 张阳鑫 A kind of linkage lock anti-reflective bullet closed guard gate using Fluid pressure
RU188854U1 (en) * 2019-02-27 2019-04-25 Общество с ограниченной ответственностью "ВС-ГРУПП" AUDIT HATCH
RU2717401C1 (en) * 2019-05-13 2020-03-23 Общество с ограниченной ответственностью "Феррумленд" Outer loop fast-action water-and-gas steel
US11414907B2 (en) * 2019-07-01 2022-08-16 Gulfstream Aerospace Corporation Door assembly and method for making the same, and aircraft including a door assembly
CN111852240A (en) * 2020-07-13 2020-10-30 临沂矿业集团有限责任公司 Automatic opening and closing device for airtight door
USD991134S1 (en) * 2020-07-23 2023-07-04 Peter J. Luciani, JR. Deck hatch
CN112796636B (en) * 2021-01-13 2022-08-09 铜陵市金鑫人防工程防护设备有限公司 Tunnel positive line protective airtight door for civil air defense engineering
US11732528B2 (en) * 2021-06-29 2023-08-22 Toshiba International Corporation Door fastener retaining assembly, system, and method
CN114809824B (en) * 2022-05-06 2023-10-03 北京奔驰汽车有限公司 Method and device for opening and closing heavy door, computer equipment and storage medium

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US6123370A (en) * 1999-03-31 2000-09-26 Hartwell Corporation Increased strength dogging mechanism
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AU2013245574B2 (en) 2017-05-18
CA2830060A1 (en) 2014-04-23
NO2838843T3 (en) 2018-03-03
BR102013026598B1 (en) 2021-10-26
BR102013026598A2 (en) 2014-12-09
DE102013016963A1 (en) 2014-04-24
AU2013245574A1 (en) 2014-05-08
CA2830060C (en) 2019-07-09
KR20140051769A (en) 2014-05-02
BR102013026598A8 (en) 2021-08-17
KR101832009B1 (en) 2018-02-23
US20140109480A1 (en) 2014-04-24
PL2724929T3 (en) 2018-04-30
US8984812B2 (en) 2015-03-24
ES2657045T3 (en) 2018-03-01
EP2724929B1 (en) 2017-11-08

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