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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United States of America Patent
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Issued Date -
Aug 24, 2023
app pub date -
Feb 22, 2023
filing date -
Feb 24, 2022
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Abstract
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.
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