A landing gear system may include: a casing coupled to a fuselage of an aircraft, such as an urban air mobility vehicle; a steering , one side of which is inserted into the casing and the other side of which is connected to a tire; a magnetorheological (MR) damper including a cylinder coupled to the casing and a piston coupled to the steering rod; a sensor unit configured to measure a condition of the urban air mobility vehicle; and a controller configured to control damping force of the MR damper based on measurement data of the sensor unit. The sensor unit may include a first sensor for measuring a stroke of the MR damper and a second sensor for measuring an acceleration of the casing.
LANDING GEAR SYSTEM WITH MAGNETORHEOLOGICAL DAMPER
FAHRWERKSYSTEM MIT MAGNETORHEOLOGISCHEM DÄMPFER
SYSTÈME DE TRAIN D'ATTERRISSAGE AVEC AMORTISSEUR MAGNÉTORHÉOLOGIQUE
2024-06-12
Patent
Electronic Resource
English