Aircraft
AssigneeAirbus Operations GmbH
InventorsNicholas Hancock, Christopher James Perkins
Life of this patent
Estimating the term…
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AssigneeAirbus Operations GmbH
InventorsNicholas Hancock, Christopher James Perkins
Estimating the term…
An aircraft has a landing gear with a main leg, a support leg, and a wheel arm which has a wheel support and is pivotably connected to the main leg and support leg. The main leg and support leg are pivotably connected to the airframe of the aircraft, and can be pivoted aft to move the wheel arm aft and upward and move the landing gear from a deployed configuration to a stowed configuration. With the landing gear in the deployed configuration, the support leg is positioned forward of the main leg. The main leg, support leg and wheel arm form a triple-rocker four bar linkage such that pivoting the main leg and support leg aft pivots the wheel arm and retracts the wheel support.
An aircraft having a forward direction and an aft direction and having a landing gear which is movable between stowed and deployed configurations, the landing gear comprising:
A method of retracting a landing gear of an aircraft which has a forward direction and an aft direction, the landing gear comprising:
Dependencies are inferred from the claim text.