A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
MÉCANISME DE VERROUILLAGE D'AU MOINS UN ÉLÉMENT MOBILE SITUÉ DANS UNE PREMIÈRE ZONE ET COMPORTANT UN COMPOSANT RÉGLABLE DEPUIS UNE DEUXIÈME ZONE, AÉRONEF COMPRENANT AU MOINS UN TEL MÉCANISME DE VERROUILLAGE
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.
MÉCANISME DE VERROUILLAGE D'AU MOINS UN ÉLÉMENT MOBILE SITUÉ DANS UNE PREMIÈRE ZONE ET COMPORTANT UN COMPOSANT RÉGLABLE DEPUIS UNE DEUXIÈME ZONE, AÉRONEF COMPRENANT AU MOINS UN TEL MÉCANISME DE VERROUILLAGE
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.
MÉCANISME DE VERROUILLAGE D'AU MOINS UN ÉLÉMENT MOBILE SITUÉ DANS UNE PREMIÈRE ZONE ET COMPORTANT UN COMPOSANT RÉGLABLE DEPUIS UNE DEUXIÈME ZONE, AÉRONEF COMPRENANT AU MOINS UN TEL MÉCANISME DE VERROUILLAGE
LOCKING MECHANISM FOR AT LEAST ONE MOBILE ELEMENT LOCATED IN A FIRST AREA AND COMPRISING A COMPONENT ADJUSTABLE FROM A SECOND AREA, AIRCRAFT COMPRISING AT LEAST ONE SUCH LOCKING MECHANISM
VERRIEGELUNGSMECHANISMUS FÜR MINDESTENS EIN IN EINEM ERSTEN BEREICH ANGEORDNETES BEWEGLICHES ELEMENT MIT EINEM AUS EINEM ZWEITEN BEREICH VERSTELLBAREN BAUTEIL, LUFTFAHRZEUG, DAS MINDESTENS EINEN SOLCHEN VERRIEGELUNGSMECHANISMUS UMFASST
BROCHARD WOLFGANG (author) / CAZEAUX LAURENT (author) / VIGNOBOUL BENJAMIN (author)
2024-10-30
Patent
Electronic Resource
French
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