Aircraft landing gear comprising an operation strut device and aircraft provided therewith
AssigneeAirbus France
InventorsPaul De Ruffray, Rodolphe Morel
Life of this patent
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Abstract
An aircraft landing gear including a leg, a bracket which defines the axis of rotation of the leg on the operating plane defined by the leg extension and retraction positions and a leg operating device consisting of at least one strut whose first end is provided with a first means for connecting to the landing gear element and second end is provided with a second means for connecting to the element of the gear-receiving landing gear casing for which the at least one strut expands outside of the operating plane of the gear leg.
Claims12
An aircraft landing gear comprising a leg, a bracket defining a rotation axis of the leg on the operating plane defined by the leg extension and retraction positions and a leg operating device including at least one strut comprising a first end equipped with a first means of connection with an element of the landing gear and a second end equipped with a second means of connection with an element of the gear-receiving landing gear box for which the aforementioned (at least) one strut extends out of the operating plane of the gear leg.
Dependencies are inferred from the claim text.