Landing gear
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United States of America Patent
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-
May 19, 2020
Grant Date -
Feb 8, 2018
app pub date -
Jul 27, 2017
filing date -
Aug 3, 2016
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft include a landing gear is disclosed. The landing gear comprises a main strut and an inboard stay assembly connected to the aircraft fuselage such that landing gear loads can be transferred from the inboard stay assembly into the fuselage. The landing gear also comprises a sidestay connected to the wing such that landing gear loads can be transferred from the sidestay into the wing and a link assembly connected to the aircraft such that landing gear loads can be transferred via the link assembly into the aircraft. The landing gear is arranged such that, in use, when the landing gear is extended, substantially all the landing gear loads are transferred from the landing gear to the aircraft via one or more of the inboard stay assembly, the sidestay and the link assembly.
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