Composite twin beam main landing gear for an aircraft
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United States of America
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Mar 22, 2022
Grant Date -
Dec 3, 2020
app pub date -
May 30, 2019
filing date -
May 30, 2019
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Abstract
A main landing gear assembly for an aircraft has an upper beam and a lower beam. The proximal ends of the upper and lower beams are each connected to a trunnion assembly that is mounted on the fuselage or wing of the aircraft. The distal ends of the upper and lower beams are each affixed to an axel support structure on which a main wheel of the landing gear assembly is mounted. In the gear assembly, the upper beam and the lower beam are coplanar and act together, in combination, to accommodate a planar flexure of the gear assembly during aircraft takeoffs and landings.
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