Abstract
Normal 0 21 false false false TR X-NONE X-NONE In this work, an aircraft landing gear vibrations having passive suspension system, has been tried to reduce by a MR damper semi-active suspension system. MR damper being a semi-active component, has a nonlinear character and its damping force can be changed with the voltage applied to MR damper. For this purpose, the design of voltage sent to MR damper was done depending on the status of volt 2. The damping force is changed with the voltage determined and vibrations can be reduced with the help of MR dampers. The result of simulation works showed that the voltage applied to the MR damper has an active role in reducing vibration.
Keywords
Damper
Suspension (topology)
Vibration
Voltage
Work (physics)
Vibration control
Damping torque
Structural engineering
Control theory (sociology)
Nonlinear system
Engineering
Computer science
Physics
Control (management)
Acoustics
Mechanical engineering
Mathematics
Electrical engineering
Subject Areas
Mechanical Engineering and Vibrations Research
·Mechanical Engineering ·Physical Sciences
Vehicle Dynamics and Control Systems
·Automotive Engineering ·Physical Sciences
Hydraulic and Pneumatic Systems
·Mechanical Engineering ·Physical Sciences
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