Aircraft landing gear comprising an operation strut device...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/14 (2006.01) B64C 25/18 (2006.01)

Patent

CA 2627935

The invention relates to an aircraft landing gear (1) comprising a leg (2), a bracket (10) which defines the axis of rotation of the leg on the operating plane (P) defined by the leg (2) extension and retraction positions and a leg operating device consisting of at least one strut (3, 4) whose first end is provided with a first means (5) for connecting to the landing gear element and second end is provided with a second means (6) for connecting to the element (7a) of the gear-receiving landing gear casing for which said at least one strut expands outside of the operating plane of the gear leg.

L'objet de l'invention est un atterrisseur (1) d'aéronef comprenant une jambe (2), une potence (10) définissant un axe de rotation de la jambe dans un plan de manoeuvre (P) défini par une position sortie de la jambe (2) et une position rentrée de la jambe (2) et un dispositif de manoeuvre de la jambe comprenant au moins une contrefiche (3, 4) comportant une première extrémité pourvue d'un premier moyen de liaison (5) avec un élément de l'atterrisseur et une seconde extrémité pourvu d'un second moyen de liaison (6) avec un élément (7a) d'une case de train recevant l'atterrisseur pour lequel ladite au moins une contrefiche s'étend hors du plan de manoeuvre de la jambe de l'atterrisseur.

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