Landing gear system with magnetorheological damper

The present disclosure relates to a landing gear system that may include: a sleeve coupled to a fuselage of an aircraft, such as a city aerial mobile vehicle; a steering lever, one side of which is inserted into the sleeve and the other side of which is connected to a tire; a magnetorheological (MR)...

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Bibliographische Detailangaben
Hauptverfasser:	LEE JUNG-HYUN, HUANG YOUZHEN, KIM JONG-HYUNG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MEANS FOR DAMPING VIBRATION MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICS SHOCK-ABSORBERS SPRINGS TARIFF METERING APPARATUS TESTING THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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