A rotary damper includes a rotating input member rotating about a rotation axis; a first cylinder and a second cylinder coaxially arranged on opposite sides of the rotation axis; a first and a second pistons slidable inside the first and second cylinders and defining a first and a second working chambers containing incompressible working fluids, respectively; motion conversion mechanisms converting the rotary motion of the rotating input member about the rotation axis into reciprocating motion of the first and second pistons; a third cylinder; a fourth cylinder; and a third and fourth pistons, slidable inside the third and fourth cylinders, respectively and separating the inner volume of the respective cylinder into a respective main chamber in fluid communication with the first working chamber and auxiliary chambers; and the second working chamber and auxiliary chambers respectively.

A damping arrangement (1) for damping radial vibrations in a rotating shaft (2), the damping arrangement (1) comprising at least one first damping element (3), at least one second damping element (4), and a bearing arrangement (5) operably engaging the first damping element (3) and the second damping element (4). The bearing arrangement (5) comprises a first bearing member (6), a second bearing member (7), and a reference (8). The first bearing member (6) is rotatably mounted on the shaft (2) so that radial movement of the shaft (2) is transferred to the first bearing member (6), and is operably connected to the second bearing member (7) by the first damping element (3) and by a first steering structure (9). The first steering structure (9) allows only reciprocating movement of the first bearing member (6), and the shaft (2), in a first radial direction (D1), and the first damping element (3) dampens the reciprocating movement in the first radial direction (D1) with respect to the second bearing member (7). The second bearing member (7) is operably connected to the reference (8) by the second damping element (4) and by a second steering structure (10) allowing only reciprocating movement of the second bearing member (7), the first bearing member (6), and the shaft (2), in a second radial direction D2. The second damping element (4) dampens the reciprocating movement in the second radial direction (D2) with respect to the reference (8).

A damper device includes an outer cylinder, an inner cylinder disposed inside the outer cylinder and having an inner chamber, a lower open end, and an upper closed end wall with a vent hole, a piston disposed in the inner chamber and having a passageway, a check valve coupled to the passageway to permit only upward flowing of a working fluid in the inner chamber through the passageway, and a piston rod having a lower rod end disposed outwardly of the outer cylinder, and an upper rod mounted to permit the piston to slide with the piston rod. The sliding of the piston rod is dampened by sliding of the piston in the inner chamber. A hinge assembly including the damper device is also disclosed.

Provided is an adjusting method for a resonance frequency of a vibration isolator, the vibration isolator including first to n-th elastic member groups and/or an n+1-th elastic member group, the first to n-th elastic member groups and/or the n+1-th elastic member group being located on an xy plane of an xyz coordinate system, and an xy coordinate system of the xyz coordinate system being a coordinate system obtained by, when a tensor of inertia I with respect to an XYZ coordinate system having an origin in a center of gravity of a vibration sensing side structure or a vibration source side structure is represented as I, rotating an XY coordinate system by =tan.sup.1(2I.sub.XY/(I.sub.XXI.sub.YY)) around a Z axis, the adjusting method including, when rigidity K.sub.i of the first to n-th elastic member groups is represented as $\left[K_i\right]=\left[\begin{array}{ccc}{k}_{i\_\mathrm{xx}}& 0& 0\\ 0& k_{i\_\mathrm{yy}}& 0\\ 0& 0& k_{i\_\mathrm{zz}}\end{array}\right],$
rigidity K.sub.n+1 of the n+1-th elastic member group is represented as $ [ K n + 1 ] = [ RACK AND PINION DAMPER 20200386294 · 2020-12-10 · KINEMATICS, LLC · Adam P. Plesniak A rack and pinion damper provides controllable rotary motion of a pinion by actuating a rack inside a fluid disposed within a housing. The rack includes one or two cylindrical heads which further include flow-control mechanisms. Two plugs maybe threaded into the ends of the rack sections of the housing to limit a maximum clockwise rotation and a maximum counterclockwise rotation of the pinion. The pinion maybe coupled with an external unit, such as a torque tube, to control its rotational motion. DAMPER DEVICE AND HINGE ASSEMBLY INCLUDING THE SAME 20200378168 · 2020-12-03 · Waterson CHEN A damper device includes an outer cylinder, an inner cylinder disposed inside the outer cylinder and having an inner chamber, a lower open end, and an upper closed end wall with a vent hole, a piston disposed in the inner chamber and having a passageway, a check valve coupled to the passageway to permit only upward flowing of a working fluid in the inner chamber through the passageway, and a piston rod having a lower rod end disposed outwardly of the outer cylinder, and an upper rod mounted to permit the piston to slide with the piston rod. The sliding of the piston rod is dampened by sliding of the piston in the inner chamber. A hinge assembly including the damper device is also disclosed. IMPROVEMENTS IN DAMPED HINGE ASSEMBLIES 20200370352 · 2020-11-26 · TITUS D.O.O. DEKANI · David Pecar A damped hinge assembly for mounting a first member for rotational movement relative to a base member about a hinge axis is provided. The assembly includes a first linearly acting damping device, and first camming means for converting rotational movement of the first member in a first direction into linear actuation of the first damping device to cause it to impart a damped resistive force to the first member over at least part of its movement in said first direction. The first damping device is mounted with its linear axis coincident with the hinge axis, with the first damping device acting as a fulcrum for said rotational movement of the first member. Unmanned aerial vehicle (UAV) recovery system 10800547 · 2020-10-13 · The United States Of America, As Represented By The Secretary Of The Navy · Shawn Kerry McGann, Nicholas McGaha A UAV recovery system. The UAV recovery system may comprise: a mast having a mast pulley with a swivel, a base, upper and lower booms extending somewhat horizontally from the mast, a cable and pulley arrangement, a shock absorber, and a mast cable coupled between the mast pulley and the shock absorber. The cable and pulley arrangement may comprise: upper boom pulleys coupled near an associated end of the upper boom, lower boom pulleys coupled near an associated end of the lower boom, and a cable forming a loop around the upper and lower boom pulleys. The cable and pulley arrangement may also comprise a net for capturing the UAV. The shock absorber may urge the mast to rotate into a neutral position, but permit the mast to rotate not more than a controlled-tensioned position. Damper Device 20200124112 · 2020-04-23 · Suzuki Motor Corporation · Hiroki Inata A damper device according to the present invention includes an input shaft member to which a driving force from a crankshaft of an internal combustion engine is input, an output shaft member capable of outputting the driving force transmitted from the input shaft member, an input side cam and an output side cam respectively connected to the input shaft member and the output shaft member, and a damper bearing pivotable on the input side cam or the output side cam, wherein a damper bearing assembly has a bearing shaft supporting a plurality of damper bearings, bearing axes of the plurality of damper bearings are arranged along a bearing shaft axis of the bearing shaft, the bearing shaft is orthogonal to a rotation axis, and a shaft support portion supporting the bearing shaft, is provided between the adjacent damper bearings of the damper bearing assembly. Active control stewart vibration damping platform based on magnetic transmission 11927235 · 2024-03-12 · Chongqing University, SHANGHAI UNIVERSITY · Huayan Pu, Zhi Sun, Jun Luo, Jinglei Zhao, Jin Yi, Yi Qin, Shujin Yuan Disclosed is an active control Stewart vibration damping platform, including a load-bearing platform, a base, and six telescopic rods. Each telescopic rod includes a driving motor, a rotating shaft, a sleeve, and a moving rod. One end, away from the driving motor, of the rotating shaft is provided with a cylindrical cavity, one end of the moving rod penetrates through the cylindrical cavity, and the sleeve is sleeved outside the rotating shaft. The rotating shaft is in running fit with the sleeve through a first bearing, and the moving rod is in sliding fit with the sleeve through a second bearing. The moving rod and the rotating shaft are respectively provided with a spiral permanent magnet. The spiral permanent magnet on the rotating shaft can drive the moving rod to move in an axial direction of the rotating shaft through the spiral permanent magnet on the moving rod when rotating. $