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
12.06.2024
Patent
Elektronische Ressource
Englisch
Design and analysis of a magnetorheological damper for airplane landing gear [10595-55]
British Library Conference Proceedings | 2018