Landing gear steering using eccentric bearings
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United States of America Patent
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Nov 3, 2015
Grant Date -
Feb 20, 2014
app pub date -
Dec 21, 2011
filing date -
Jan 11, 2011
priority date (Note) -
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Abstract
A landing gear assembly for an aircraft, the landing gear assembly including: an elongate bogie beam; a first axle bearing having an outer part rotatably coupled to an inner part, the outer part being coupled to the bogie beam, the inner part including a mounting aperture; and an elongate axle provided through the mounting aperture of the inner part and coupled thereto, wherein the axle is coupled to the inner part of the first axle bearing in a configuration such that the longitudinal axis of the axle is spaced from the axis of rotation of the inner part, such that rotation of the inner part causes a change in the orientation of the axle relative to the bogie beam.
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