An electromechanical chassis actuator includes a single electric motor and two screw drives. The two screw drives use a common threaded spindle. A spindle nut of the first screw drive is rotationally fixed to the electric motor's rotor and engages the threaded spindle in a back-driveable manner. A spindle nut of the second screw drive is selectively coupled to the electric motor's rotor by a coupler and engages the threaded spindle in a self-locking (not back-driveable) manner. When the coupler is in an engaged position, the actuator operates in a level-adjustment mode. When the coupler is in a released position, the actuator operates in a damping mode.

A vibration absorber which, in addition to a main mass which is fixed thereto and moved along a curved trajectory by a driving mechanism, comprises a substantially smaller variably adjustable rotating flywheel mass which is moved together with the main mass along the trajectory thereof, enabling the adjustment of the frequency of the absorber. The rotating flywheel mass is driven by a novel belt device independently of the driving mechanism. A rotating vibration absorber which, along with the main mass and the rotating flywheel mass, comprises its own damping unit, such as an eddy-current damping unit.

An electric adjustable magnetic control damper comprises a force applied unit, a magnetic control unit, a driving unit, and a control unit; a driving rod drives the force applied unit displaced linearly, and a screw sleeve for the screw sleeve to displace linearly and for the screw rod and the magnetic ring to be rotatable, the magnetic control unit has a fixing seat able to displace linearly, and the fixing seat has a the permanent magnet, the driving unit has a motor and a gear train, the control unit can input the required damper value to drives the motor to rotate; whereby the motor and the gear train drives the fixing seat displaced, and create a required gap between the permanent magnet of the fixing seat and the rotor of the magnetic ring to create eddy load for being dampers of axial displacement of the driving rod and rotation of the rotor, and the damper achieves the effect of fitness exercise.

An electric adjustable magnetic control damper comprises a force applied unit, a magnetic control unit, a driving unit, and a control unit; a driving rod drives the force applied unit displaced linearly, and a screw sleeve for the screw sleeve to displace linearly and for the screw rod and the magnetic ring to be rotatable, the magnetic control unit has a fixing seat able to displace linearly, and the fixing seat has a the permanent magnet, the driving unit has a motor and a gear train, the control unit can input the required damper value to drives the motor to rotate; whereby the motor and the gear train drives the fixing seat displaced, and create a required gap between the permanent magnet of the fixing seat and the rotor of the magnetic ring to create eddy load for being dampers of axial displacement of the driving rod and rotation of the rotor, and the damper achieves the effect of fitness exercise.

The invention describes a fluid damper for furniture parts that are movable relative to one another, said fluid damper comprising a piston (4) guided movably in a cylinder (1) along a longitudinal axis. At least one through opening (4.1, 4.2) for fluid flowing through is provided in the piston (4) and/or between the piston (4) and cylinder (1). A sleeve (2) is arranged so as to be radially rotatable, relative to the piston (4) against a spring loading, about the longitudinal axis or about an axis running parallel thereto, which sleeve comprises, on its circumference, a number of wings (2.1, 2.2, 2.1, 2.2) corresponding to the number of through openings (4.1, 4.2). The spring loading is directed such that the wing (2.1, 2.2, 2.1, 2.2) exposes the through opening (4.1, 4.2) when the piston (4) is stationary in the cylinder (1) and in the event of a movement in a movement direction of the piston (4) and of the cylinder (1) relative to one another along the longitudinal axis, and progressively closes said through opening in the event of a movement against the movement direction with increasing relative speed between the piston (4) and cylinder (1) along the longitudinal axis. The fluid damper comprises a hollow-cylindrical part of the piston (4), which surrounds the sleeve (2) and the at least one wing (2.1, 2.2, 2.1, 2.2), which is arranged on the circumference of said sleeve, along at least part of the longitudinal axis thereof.

A suspension is provided which can not only generate a damping force between sprung mass and unsprung mass but also steer a wheel. A suspension includes: a shaft coupled to sprung mass of a vehicle, the shaft having a screw groove and a spline groove formed thereon; a ball screw nut assembled to the shaft via a ball; a ball spline nut assembled to the shaft via a ball; a ball screw-specific motor connected to the ball screw nut; a ball spline-specific motor connected to the ball spline nut; and a case coupled to unsprung mass of the vehicle, the case being configured to hold the ball screw-specific motor and the ball spline-specific motor. The ball spline-specific motor rotates the ball spline nut and the shaft relative to the case.

A multidirectional adaptive re-centering torsion isolator is used for isolating buildings, tanks and bridges from earthquakes. The multidirectional adaptive re-centering torsion isolator includes a flat and/or articulated slider and four or more cylindrical energy dissipaters. The flat and/or articulated slider positioned on top of the column provides vertical load transmission, low friction and horizontal displacement capacity. The cylindrical energy dissipaters provide displacement, re-centering and damping in any of the horizontal directions.

A kit for a helicopter is described, the helicopter comprising a fuselage and a rotor; the kit comprises at least one device adapted to dampen the vibrations transmitted from the rotor to the fuselage and to be interposed between the fuselage and the rotor; the device, in turn, comprises a first threaded element operatively connectable to the rotor and adapted to, in use, vibrate parallel to a first axis; a second threaded element operatively connectable to the fuselage and operatively connected to the first threaded element so as to, in use, rotationally vibrate about the first axis; and a plurality of threaded rollers, which are screwed on the first and second threaded elements; the rollers being rotatable about their respective second axes parallel to and separate from the first axis with respect to the first and second threaded elements; the rollers are also rotatable about the first axis with respect to the first threaded element and the second threaded element.

A kit is described that comprises a device adapted to dampen the vibrations transmitted by the rotor to the fuselage; the device comprises two first elements movable along a first axis; two second elements rotatable about the first axis; a first inerter with a first female screw, a first screw, and first rollers rotatable about respective second axes and around the first axis with respect to the first female screw and first screw; a second inerter with a second female screw, a second screw operatively connected to the second female screw; and a plurality of second rollers rotatable about second axes and around the first axis with respect to the second female screw and second screw; the first and second female screws defining the first threaded elements, and the first and second screws defining the second threaded elements; or the first and second screws defining the first threaded elements and the first and second female screws defining the second threaded elements.

An automatic pressure regulating pneumatic cylinder includes: a pneumatic cylinder, arranged with a connecting element for sealing the pneumatic cylinder, a piston slidably configured above the connecting element, a upper air chamber formed above the piston, and a lower air chamber formed between the piston and connecting element, the pneumatic cylinder further configured with first and second air entering passages allowing external air to one-way flow into the upper air chamber and a first guide passage allowing the external air to one-way flow into the lower air chamber; an air flow control unit, embedded inside the connecting element, an exhaust floating piston of the air flow control unit allowed to correspondingly form an air passage for opening or closing through normal speed and rapid displacement of the piston and further cause the internal air of the lower air chamber to generate different air pressure resistance for automatic internal pressure regulation.