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公开(公告)号:EP4311762A1
公开(公告)日:2024-01-31
申请号:EP22400007.5
申请日:2022-07-29
摘要: The invention relates to an aircraft door (7) with an inner door space (7d); a door opening system (8) arranged at least partly in the inner door space, comprising: at least one locking device (8c) for locking the aircraft door in a locked state, actuation kinematics (8b) for actuating the at least one locking device, and at least one transmission rod (8d) coupling the actuation kinematics with the at least one locking device; wherein the at least one transmission rod is displaceable in the inner door space by means of the actuation kinematics for actuating the at least one locking device; and an anti-vibration device (9) mounted in the inner door space to the at least one transmission rod for absorbing vibrations of the at least one transmission rod, wherein the anti-vibration device is displaceable in the inner door space together with the at least one transmission rod.