The invention discloses a variable-stiffness
magnetorheological fluid elastic vibration isolator for a variable-speed rotorcraft, which comprises a
closed cavity formed by a
magnetic flux outer cylinder, a
magnetic flux inner cylinder and an annular
magnetorheological elastomer connected between the
magnetic flux outer cylinder and the magnetic flux inner cylinder,
inertia liquid is filled in the cavity, and a
magnet exciting coil is arranged in an outer ring groove of the magnetic flux inner cylinder. The magnetic flux outer cylinder, the
magneto-rheological
elastomer and the magnetic flux inner cylinder form a closed
magnetic circuit, and the
magnetic field intensity is changed by adjusting the current of the
magnet exciting coil, so that the
shear modulus of the
magneto-rheological
elastomer is continuously and reversibly adjusted and controlled, and online adjustment of the rigidity of the vibration
isolator is achieved. The inner cylinder connected with the magnetic flux inner cylinder is provided with an
inertia channel, when external vibration is introduced, liquid flows in the channel, and
inertia force opposite to exciting force is generated at an anti-
resonance frequency point to achieve efficient
vibration isolation. The variable vibration frequency of the rotor wing is dynamically matched through the electronic control rigidity, the problems that a traditional vibration
isolator is narrow in
frequency band, and a mechanical
frequency conversion scheme is slow in response and complex in structure are solved, and the vibration isolator has the advantages of being fast in response and compact in structure.