A pitch trimmer assembly for an aircraft landing gear having a damping element arranged to be connected between a first and a second element of an aircraft landing gear and arranged to exert a first damping force when in a first state and a second damping force in a second state, the damping element being switchable between the first and second states in dependence on the relative positions of the first and second landing gear elements.
РЕГУЛИРУЮЩИЙ ПРИВОД С ИЗМЕНЯЕМОЙ СТЕПЕНЬЮ ДЕМПФИРОВАНИЯ
2017-03-10
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |