Airbus Operations Gmbh

Airbus Deutschland Gmbh

Konstantin Wagner

Herbert Steinbeck

Sergej Moiseenko

Sebastian Fritzsche

A door hinge comprises a first hinge element fastenable to a door frame and a second hinge element fastenable to a door leaf and includes first and second hinge blade. A first pivot axis is connected, when the door hinge is in a first operating condition, to first and second hinge elements such that the second hinge blade is pivotable relative to the first hinge element, in a first pivot direction, for unblocking a door aperture. The first pivot axis is decoupled from the first or the second hinge element when the door hinge is in a second operating condition. A second pivot axis is connected to the first and second hinge elements such that said first and second hinge elements are pivotable relative to one another, in a second pivot direction which is opposed to the first pivot direction, for unblocking the door aperture.

Door hinge and door arrangement

A device () for the detachable connection of structural parts (80, 84) in an aircraft, comprising a clamping lever arrangement () associated with a first structural part () and a clamping pin () associated with a second structural part (), wherein the clamping lever arrangement () comprises an eccentric shaft () rotatably mounted about a rotation axis (A) on the first structural part (), a clamping lever () mounted eccentrically and swivellably with respect to the eccentric shaft () and a driving bushing () rotatably mounted relative to the eccentric shaft () about the rotation axis (A) and coupled in a geared manner to the clamping lever (), wherein the clamping lever arrangement () can furthermore be displaced between a release position, a readiness position and a locking position.

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Laupheim, Germany

Konstantin Wagner