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An aircraft landing gear includes a landing gear provided with a yoke supporting a spindle on which is mounted a capture pin to be hooked by a hook of a locking box to be mounted on a structure of an aircraft to immobilize the landing gear in a given position with respect to the structure. The capture pin includes a body provided with a longitudinal opening enabling the capture pin to be mounted on the spindle, and an outer surface of revolution having a central portion having a convex profile to cooperate with the hook. A central portion of the outer surface is formed on a central ring which is mounted so as to rotate freely on a central portion of the body.
An aircraft landing gear includes a landing gear provided with a yoke supporting a spindle on which is mounted a capture pin to be hooked by a hook of a locking box to be mounted on a structure of an aircraft to immobilize the landing gear in a given position with respect to the structure. The capture pin includes a body provided with a longitudinal opening enabling the capture pin to be mounted on the spindle, and an outer surface of revolution having a central portion having a convex profile to cooperate with the hook. A central portion of the outer surface is formed on a central ring which is mounted so as to rotate freely on a central portion of the body.
OLIVE POUR CROCHET DE VERROUILLAGE
CAPTURE PIN FOR A LOCKING HOOK
FANGSTIFT FÜR EINEN VERSCHLUSSHAKEN
DUFAY LUDOVIC (author)
2022-11-16
Patent
Electronic Resource
French
DISPOSITIF DE VERROUILLAGE D’UN VOLET MASQUANT UN ESPACE, À CROCHET COUPLÉ À UN AXE
European Patent Office | 2021
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