公开(公告)号：EP1411201A3

公开(公告)日：2007-12-26

申请号：EP03021408.4

申请日：2003-09-26

申请人： ROTO FRANK AG

发明人： Wolf, Edgar

IPC分类号： E05D11/00 ,  E05B17/20 ,  E05C3/12

CPC分类号： E05D11/0027 ,  E05D15/30 ,  E05F7/005 ,  E05Y2600/13 ,  E05Y2600/41 ,  E05Y2900/132 ,  E05Y2900/148

摘要： Bei einem Beschlag zum Einbau zwischen einem Flügel (2) eines Fensters (1), einer Tür oder dergleichen und einem zugeordneten festen Rahmen (3), wobei an einem Flügelfalz (9) und einem diesem gegenüberliegenden Rahmenfalz (8) einerseits ein erstes Beschlagteil (6, 20, 40, 60) und andererseits ein zweites Beschlagteil (7) angebracht ist, weist das erste Beschlagteil (6) einen Grundkörper (10) und ein an dem Grundkörper (10) gehaltenes Stützteil (11) auf, das bei geschlossenem Flügel (2) das zweite Beschlagteil senkrecht zur Flügelhauptebene abstützt, wobei das Stützteil (11) aufgrund der Relativbewegung des ersten und zweiten Beschlagteils (6; 7) beim Schließen und/oder Öffnen des Flügels (2) gegen die Wirkung einer Rückstellkraft quer zur Wirksichtung der Abstützung auslenkbar ist. Durch diese Maßnahme wird von außen auf den Flügel (2) wirkender Druck aufgenommen.

摘要翻译： 在叶之间的装配用于装配（2）的窗口（1），一个门或类似物和相关联的固定的框架（3），在窗框（9）和相对该帧回扣（8）在一方面的第一嵌合部（ 6安装，20，40，60）和在另一方面的第二嵌合部（7），所述第一装配件上的基体（10）和一个（在基体10）的一部分（6）保持，当所述叶闭合支撑构件（11） （2）支撑所述第二嵌合部垂直于所述主翼面，其中，所述支撑构件（11）由于第一和第二装配部分的相对运动（6; 7）的叶（2）克服复位力的作用横向于Wirksichtung的关闭和/或打开期间 支持是可变的。 通过这个措施，从机翼外侧（2）吸收作用压力。

公开(公告)号：EP1070185A4

公开(公告)日：2007-11-07

申请号：EP99916396

申请日：1999-04-05

申请人： DETEX CORP

发明人： HAECK PAUL ,  DRAKE GREG ,  RANZAU ALBERT E III

IPC分类号： E05B17/06 ,  E05B63/18 ,  E05B65/10 ,  E05C3/12

CPC分类号： E05B65/1053 ,  E05B17/06 ,  E05B63/18 ,  E05B65/1006 ,  E05B65/104 ,  E05B65/1093 ,  E05C3/124 ,  Y10S292/53 ,  Y10S292/65 ,  Y10S292/66 ,  Y10T70/5159 ,  Y10T70/8541 ,  Y10T70/8973 ,  Y10T292/0908

摘要： The panic exit door hardware device suitable for use on doors in schools, hospitals, public buildings and other commercial buildings includes the following features: (1) an improved latch deadlocking mechanism (142); (2) an improved latch to pad mechanism (160); (3) a pad lock down features (112); (4) an improved universal mounting plate (174) and easily mounted strike (190); and (5) a vertical rod-bottom bolt deadlocking mechanism (200) in its center case. The latch deadlocking mechanism includes a deadlock link (142/144), which in the event of a fire, will block movement of the latch bolt (116).

公开(公告)号：EP1076143B1

公开(公告)日：2007-09-12

申请号：EP00116041.5

申请日：2000-07-26

申请人： BSH Bosch und Siemens Hausgeräte GmbH

发明人： Feisthammel, Egon

IPC分类号： E05C19/06 ,  E05C3/12

CPC分类号： E05C19/06

公开(公告)号：EP1234935A3

公开(公告)日：2003-11-26

申请号：EP02003886.5

申请日：2002-02-21

申请人： Westinghouse Air Brake Technologies Corporation

发明人： Oakley, Robert L. ,  Payne, Robert

IPC分类号： E05B65/12 ,  E05B65/08 ,  E05B47/02 ,  E05B51/02 ,  E05C3/12 ,  B61D19/00 ,  E05B65/36 ,  E05B65/38 ,  E05B47/00

CPC分类号： E05B47/023 ,  E05B17/007 ,  E05B47/0002 ,  E05B63/0069 ,  E05B65/0003 ,  E05B65/0811 ,  E05B65/0829 ,  E05B77/00 ,  E05B77/46 ,  E05B77/50 ,  E05B81/10 ,  E05B81/64 ,  E05B83/363 ,  E05B83/40 ,  E05B83/42 ,  E05C2007/007

摘要： A locking device (10) for attachment to a fixed portion of a transit vehicle door system is for locking one or more doors of the transit vehicle door system in either a fully locked position or a pushback lock position. The locking device (10) has a simple lock arm (30), biased toward the locking position and rotatably attached to the fixed portion of the transit vehicle door system at a first pivot (32) of the rotary lock arm (30), the rotary lock arm (30) having at least one door engagement portion for engaging a portion of the door(s) for locking the door(s) when the rotary lock arm (30) is in at least one of the locking position and the pushback position thereof. A linear actuator (20), rotating the lock arm (30) to the unlocked position when energized, is attached to the fixed portion of the transit vehicle door system and connected to a second pivot (34) of the lock arm, said second pivot (34) offset from the first pivot (32). A lock actuator sensing switch (40) provides a feedback on the actuator position to the transit vehicle control system. Means are provided within linear actuator to manually rotate lock arm toward unlocked position for opening doors during an emergency.

公开(公告)号：EP0116543B1

公开(公告)日：1989-01-11

申请号：EP82903603.7

申请日：1982-08-20

申请人： THE BOEING COMPANY

发明人： FITZGERALD, James, Thomas

IPC分类号： E05C3/24 ,  E05C3/12 ,  E05B3/00 ,  B64C1/14

CPC分类号： B64C1/143 ,  B64C1/1407

摘要： Actuating mechanisms (106 and 122) for latching and unlatching an aircraft plug-type door (50) which is laterally and vertically translatable along tracks (55, 56 and 60) for movement into and out of an ingress/egress door opening (51) formed in the aircraft fuselage (52) and vertically along a path following the interior contour of the fuselage (52). The interior actuating mechanism (106) includes an interior door handle (99) mounted in the fuselage (52) adjacent the ingress/egress opening (51) and swingable between first and second positions, with the interior door handle (99) being operably associated with locking means (119, 120) for locking the door (50) upon closure thereof and for unlocking the door (50) preparatory to opening thereof. The external actuating mechanism (122) includes an exterior door handle (124) mounted in and flush with the fuselage (52) adjacent the ingress/egress opening (51) and swingable between first and second positions, with the exterior actuating mechanism (122) being normally disassociated with the interior actuating mechanism (106) so as to permit independent interior manipulation of the latter. Means (126, 134) are provided which are accessible only from the exterior of the aircraft for operatively associating the exterior door handle (124) with the interior door handle (99) and slaving the two together so as to permit door locking and unlocking from the exterior of the aircraft. The aircraft includes an emergency escape slide normally stowed within and carried by the door (50), and means (70, 75) for arming the emergency evacuation system to attach the escape slide to the passenger deck (74) and for disarming the system so that the escape slide is attached to the door (50). Locking means (89, 91, 94 and 95) are provided for releasably but positively locking the escape slide to the door (50) when the emergency evacuation system is disarmed. The door (50) may be opened from the interior of the aircraft with the emergency evacuation system armed or disarmed. Means (126, 141) are provided on the exterior of the aircraft for automatically disarming the emergency evacuation system preparatory to opening the door (50) from the exterior of the aircraft.