A landing gear support arrangement may comprise a cylinder, a pin pivotally coupled to the cylinder, a head attached to the pin having a portion extending radially from the pin, and a bracket coupled to the portion of the head configured to axially support the pin.
LANDING GEAR WITH STRUCTURAL LOAD PATH DIVERTER BRACKET
12.05.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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