公开(公告)号：EP2140088A1

公开(公告)日：2010-01-06

申请号：EP08749202.1

申请日：2008-04-28

申请人： Airbus Operations GmbH

发明人： WAGNER, Konstantin ,  MOISEENKO, Sergej ,  FRITZSCHE, Sebastien

IPC分类号： E05D3/06 ,  E05D3/08 ,  E05D11/10 ,  B64C1/14

CPC分类号： E05D3/12 ,  E05D3/08 ,  E05D3/127 ,  E05D11/1007 ,  E05D11/1014 ,  E05D11/105 ,  E05D15/54 ,  E05F1/1215 ,  E05Y2201/218 ,  E05Y2201/236 ,  E05Y2800/25 ,  E05Y2800/746 ,  E05Y2900/502 ,  E05Y2900/531 ,  E05Y2900/532 ,  Y10T16/528 ,  Y10T16/546 ,  Y10T16/547

摘要： The hinge (10) has a swiveling axle (32) that is connected with hinge units (12, 14) in an operating condition of the hinge, such that a hinge side piece (22) of the hinge unit (14) is swivelable in a swiveling direction around the swiveling axle for releasing a door opening limited by a door frame. The swiveling axle is decoupled from the hinge units in another operating condition of the hinge. Another swiveling axle is connected with the hinge units, such that two hinge units are swivelable around the latter swiveling axle in another swiveling direction for releasing the opening.

公开(公告)号：EP2054571B1

公开(公告)日：2011-03-30

申请号：EP07786298.5

申请日：2007-07-24

申请人： Airbus Operations GmbH

发明人： STEINBECK, Herbert ,  WAGNER, Konstantin

IPC分类号： E05B65/08 ,  E05C3/04

CPC分类号： F16B5/0084 ,  E05B17/0025 ,  E05B65/006 ,  E05B65/0817 ,  E05C3/045 ,  F16B2/185 ,  Y10S292/55 ,  Y10T70/5164 ,  Y10T292/0863 ,  Y10T292/0886 ,  Y10T292/1039 ,  Y10T292/1043

摘要： The invention relates to a device (10) for the detachable connection of structural parts (80, 84) in an aircraft, comprising a clamping lever arrangement (12) associated with a first structural part (80) and a clamping pin (14) associated with a second structural part (84), wherein the clamping lever arrangement (12) comprises an eccentric shaft (20) rotatably mounted about a rotation axis (A) on the first structural part (80), a clamping lever (16) mounted eccentrically and swivellably with respect to the eccentric shaft (20), and a driving bushing (18) rotatably mounted relative to the eccentric shaft (20) about the rotation axis (A) and coupled in a geared manner to the clamping lever (16), wherein the clamping lever arrangement (12) can furthermore be displaced between a release position, a readiness position and a locking position, wherein the damping lever (16) in the release position releases the clamping pin (14) and wherein the clamping lever (16) in the locking position engages the locking pin (14) in an interlocking positive manner on account of a relative rotation of the eccentric shaft (20) and driving bushing (18) as well as the clamping lever (16).