Airbus Operations (s.a.s.)

Airbus Operations Gmbh

Airbus (Sas)

Benjamin Vignoboul

Wolfgang Brochard

Laurent Cazeaux

Benoit Letay

Virginie Audart-Noel

Michael Galinier

Loïc Dussol

Nicolas Viallet

A locking mechanism situated in an inner zone and comprising at least one component that is adjustable in a longitudinal direction and that is linked to a support by a link having a rod secured to the adjustable component. The link includes a guideway link, linking the rod and the support, and an adjustment system. The adjustment system comprises a pivoting control pivoting on itself and having a first end accessible from an outer zone, an intermediate piece configured to pivot on itself, an angle transmission converting a pivoting movement of the pivoting control into a pivoting movement of the intermediate piece, and a helical link converting a pivoting movement of the intermediate piece into a translational movement of the rod. The locking mechanism allows for adjustment from the outer zone. An aircraft comprising at least one such locking mechanism is also provided.

Locking mechanism for at least one movable element situated in a first zone and comprising a component that can be adjusted from a second zone, and aircraft comprising at least one such locking mechanism

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Toulouse, France

Benjamin Vignoboul