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
2016-05-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |