Abstract: The invention relates to an axial spring element (6) having two peripheral ring elements (61, 62) that are spaced from one another in the axial direction and are connected to one another in a spring-elastic manner, wherein at least one of the ring elements (61) comprises one or more retaining elements (64) in order to brace the spring element with a rotor (5) and thereby hold the spring element on the rotor (5).

Abstract: An actuator noise reducer reduces the noise output of an HVAC actuator. The noise reducer has a spring arm with a sliding bearing surface which is pressed against a side of the rotating motor shaft. The spring arm introduces a generally radial force on the motor shaft, taking up bearing play and gently pressing the motor shaft into its bearing. A cylindrical hoop mount of the noise reducer mates with and encircles a cylindrical portion of the electrical motor adjacent the shaft for mounting the actuator noise reducer on the motor by axial sliding.

Abstract: A vibration damping mechanism (90) for damping vibrations to prevent coupling of vibration modes of the carrier structure (106) with vibration modes of a rotor (100) secured to the carrier structure (106). The mechanism comprises a support (3) suitable for being fastened to the rotor (100) and at least one resonator (1) including a mass (5) carried by the support (3) via mobile mounts (6) for mounting the mass (5) to move on the support (3), the mechanism (90) including at least one damper (8) for damping the resonator (1), with the damper being interposed between the resonator (1) and an engagement member (9) on the support (3).

Abstract: An active torque cancellation system is provided. The system includes a generator set having a combustion engine and mounted to an application structure. The system also includes an active power management module coupled to the engine which actively reduces vibrations in the application structure.

Abstract: A rotary supporting member supports a parallel member rotatably with respect to an upper beam. A first brace connects an opposite-end side of the parallel member with an opposite-end side of a lower beam. A second brace connects another opposite-end side of the parallel member with another opposite-end side of the lower beam. An intersection position of the first brace with the second brace is positioned more adjacent to a side of the upper beam than where an intermediate position between the upper beam and the lower beam is present. Damper members dispose respectively so as to be interposed between the parallel member and the upper beam, connecting the parallel member with the upper beam, and being disposed to make a pair at least on both sides each of which is separated away from the rotary supporting member to interpose the rotary supporting member therebetween.

Abstract: A system and method of controlling engine vibration mounted within a vehicle including at least one hydraulic mount, each mount including a fluid chamber. A pair of accelerometers sense relative acceleration across the mount between the engine and the frame and generate a relative acceleration signal. A control unit is electrically connected to the accelerometers. The control unit is adapted to generate an electronic control signal in response to the relative acceleration signal. The control device is responsive to the electric control signal for controlling the damping force of the hydraulic mount. A control algorithm calibrates the control unit such that maximum vibration damping occurs at and around the engine resonance bounce frequency.

Abstract: The invention relates to a type of shock and vibration isolator which has almost identical rigidity and damping properties in any translatory direction, wherein the device is disposed between a reference object (A) which is subjected to vibrations and shocks, and a means (B) which is only to be subjected to translatory damped vibrations and shocks in all directions, where a center bar (2) and wire rope holders (3) are designed for attachment to any one of the reference objects (A) or (B), characterized in that the center bar (2) and the wire rope holders (3) are rigidly interconnected to three or more independent wire rope series (4), each of which is formed of two or more wire rope loops where the configuration of a wire rope series (4) is based on essentially as many wire rope loops with opposite geometrical angles of inclination (A1 and A2), each wire rope series forming a symmetry along a center axis relative to an unloaded neutral position for the isolator and where the three or more wire rope series (4)

Abstract: Suspension spring for a refrigeration compressor of the type which comprises a shell and a block, forming, with the stator of an electric motor, a stationary assembly which is mounted in the interior of the shell by means of an assembly of helical springs. The helical spring presents, for a predetermined dimensional range of one of the spring parameters defined by the spring average diameter, the pitch of its coils, the spring wire diameter and the active height, a ratio between at least two of each pair of the other three parameters, defined to provide, to said helical suspension spring, for a desired frequency band, a stiffness corresponding, at minimum, to that of structural reliability of the suspension, and an attenuation in its acoustic transmissibility, in relation to the springs dimensioned only as a function of their suspension structural requirements for a desired frequency band.

Abstract: An impact-absorbing structure includes a vertical hollow column that telescopically receives a post. A coil spring surmounts a centrally apertured support plate that receives and is secured to the hollow column. A coil spring stands atop the support plate and the upper end of the coil spring is secured to a top plate that surmounts the post. A centrally apertured spacer plate is parallel to the top plate and is downwardly spaced apart from it. A plurality of bolts interconnects the top plate and spacer plate. The post retracts within the hollow column and the coil spring is compressed when a downwardly directed force is applied to the top plate. The coil spring unloads and restores the top plate and the spacer plate to their respective positions of repose when the downwardly directed force is removed. Each bolt is engaged by an eye loop at the end of a cable.

Abstract: A vibration damping device adapted to receive an electronic component and reduce vibration is provided. The vibration damping device includes a spring body extending along an axis, one or more slots formed in the spring body, and a shaft extending substantially coaxially within the spring body. The shaft may include an internal bore configured to extend substantially coaxially through the spring body and shaft. The vibration damping device further includes a damping mechanism configured to be positioned between the spring body and the shaft, wherein the one or more slots provides flexible movement of the spring body and the damping mechanism provides the damping of motion within the internal bore.

Abstract: The support (300) is intended to be fixed in a housing provided in the drone, through a mechanical interface (310) made of a material absorbing the mechanical vibrations. The mechanical interface, annular in shape, is intended to be attached to a corresponding annular shoulder provided in the housing. A fastening part (301) for fixing the support in the housing carries the mechanical interface (310), with at least one connection leg (302) supporting the navigation electronic card (320) and mounted free at one end on the fastening part. A battery (400) for the power supply of the drone is further accommodated in the support. The navigation electronic card may notably include a navigation sensor (321) such as an accelerometer, placed on the card in such a manner to be positioned at the barycenter of the drone.

Abstract: A metal shock absorber, an assembly of a metal shock absorber and a media recording unit, and a media recording device are provided. The metal shock absorber has a pair of horizontal portions, a perpendicular portion connected between the horizontal portions, and a pair of limiting portions. Each of the horizontal portions has a first arcuate protrusion protruding towards another first arcuate protrusion. The perpendicular portion is perpendicularly connected between the pair of horizontal portions, and has an assembling arm. The limiting portions are disposed at opposite sides of the perpendicular portion that are not connected with the horizontal portions. Since the thickness, the tolerance and costs of the metal shock absorber are less than those of the conventional rubber shock absorber, the assembly of the metal shock absorber with the media recording unit has a favorable assembly reliability, and therefore costs of the recording device are effectively lowered.

Abstract: To obtain vibration characteristics suited to a plurality of operating modes. A first member is mounted on at least one of a left side frame of a vehicle and a right side frame of the vehicle. The first member extends towards the right frame or the left frame. A second member is mounted to at least one of the right side frame of the vehicle and a left side frame. The second member extends towards the left frame or the right frame. A vibration insulating member is provided between the first member and the second member and elastically couples the first and second members to each other.

Abstract: An autopilot actuator includes first and second motors each including a rotatable motor output shaft such that either one or both of the motors can drive an actuator output shaft. An autopilot main unit enclosure is removably mounted to the helicopter proximate to a cyclic control and commonly houses autopilot actuators as well as main autopilot electronics. A cyclic vibration isolator is removably supported by an actuator shaft for co-rotation and coupled to the cyclic control to attenuate a cyclic vibration frequency at the actuator shaft while output rotations of the actuator shaft below a resonant frequency are coupled to the cyclic control. A force limited link includes first and second ends and a variable length between. The force limited link having a relaxed length when less than an unseating force is applied and the variable length changes when an applied force exceeds the unseating force to permit pilot override.

Abstract: In accordance with one embodiment of the present disclosure, an apparatus includes a connection body and a connection element arranged at least partially within the connection body. The connection body is operable to couple to a first element in a link arrangement and the connection element is operable to couple to a second element in the link arrangement. The apparatus further includes a metallic spring system arranged circumferentially around at least a portion of the connection element. The metallic spring system is operable to compress in response to relative movement between the connection body and the connection element.

Abstract: A device (10) for damping the vibration of a structure is provided. The device includes a main mass (12) and an auxiliary mass (20) mounted on a support (11) that is suitable for having one end held fixedly in the structure (1). The auxiliary mass (20) includes a threaded member (21) arranged around a drive screw (40) inside a casing (30) fastened to the main mass (12). The device includes manual drive (50) engaging the drive screw (40) to move the auxiliary mass (20) along the drive screw (40).

Abstract: A vibration isolator is disclosed having a housing which defines a fluid chamber. A piston, which is movable to and from a down position, is disposed within the housing. A vibration isolation fluid is disposed within the fluid chamber. A passage having a predetermined diameter extends through the piston to permit the vibration isolation fluid to flow from one fluid chamber to the other. An elastic element is provided for reducing transmission of vibrations from the piston to the housing when the piston is at the down position.

Abstract: A crankcase of an internal combustion engine includes protruding portions formed on an outer surface of the crankcase which are constituted of a pair of left and right wall members, and a vibration isolating rubber is fitted between the wall members. The crankcase configured in this manner prevents the generation of sounds from a protruding portion of the crankcase and is light-weight.

Abstract: A damper mass damper assembly includes a rod, and a casing disposed annularly about the rod and defining a primary fluid chamber therebetween. The rod includes an annular wall that defines a first and a second expansion chamber disposed at a first and a second end of the rod respectively. The rod further defines a first and a second expansion port connecting the first and the second expansion chambers respectively with the primary fluid chamber in fluid communication. As fluid within the primary fluid chamber expands from heating, the fluid may weep into the first and/or second expansion chambers through the first and/or second expansion ports respectively to maintain the integrity of a first and second cap bearing seal, which seal the fluid within the primary fluid chamber.

Abstract: Dissipative structures include at least one panel and a cell structure disposed adjacent to the at least one panel having interconnected cells. A deformable material, which may comprise at least one hydrogel, is disposed within at least one interconnected cell proximate to the at least one panel. Dissipative structures may also include a cell structure having interconnected cells formed by wall elements. The wall elements may include a mesh formed by overlapping fibers having apertures formed therebetween. The apertures may form passageways between the interconnected cells. Methods of dissipating a force include disposing at least one hydrogel in a cell structure proximate to at least one panel, applying a force to the at least one panel, and forcing at least a portion of the at least one hydrogel through apertures formed in the cell structure.

Abstract: A bearing sump includes an annular housing having a first axial length that is substantially equivalent to an axial length of the bearing sump; an annular bearing support disposed concentrically within the annular housing and having a second axial length that is less than about 50% of the first axial length; an annular space between the housing and the bearing support; and first and second axial ribs in the form of annular segments having a central angle of less than about 60 degrees and connecting with both the housing and the bearing support.

Abstract: An expansion valve includes a shaft for transmitting the drive force to a valve element and a vibration-proof spring, set between the body and the shaft, which generates the sliding friction by biasing the shaft. The vibration-proof spring includes a spring body of a hollow tube shape, a spring part, which is integrally formed with a side wall of the spring body, and a bulging portion formed on the spring part in a protruding manner such that the tip of the bulging portion is placed opposite to a part of the shaft. When the bulging portion abuts against the shaft inserted to the vibration-proof spring, the spring part is placed in a position along the spring body or is warped outwardly from the spring body, so that the elastically reactive force resulting from the warped spring part allows the shaft to slide in a stabilized manner.

Abstract: To expand a body weight adjustment range and achieve thinning. An initial position adjusting member 15 which can adjust initial resilient forces of two torsion bars 31, 41 is provided. Therefore, a body weight adjustment range is expanded as compared with a conventional configuration where a resilient force of only one torsion bar is adjusted.

Abstract: Methods and systems for limiting sensor motion. An embodiment of the invention uses unattached stud bumps to create a shock cage between a spring-mounted pad and a base substrate or a stop ring.

Abstract: Spring having a first part (1) and a second part (2) moveable relative to each other along a longitudinal axis (L), a gap (3) being provided between the first part (1) and the second part (2), the first part (1) being provided with permanent magnets (4,4?), the second part (2) including soft magnetic material, the second part (2) having a variable permeability along the longitudinal axis (L) thereof for a magnetic field provided by the permanent magnets (4,4?) of the first part (1), wherein the second part (2), for providing the variable permeability for magnetic field, is provided with at least two teeth (5,5?) of soft magnetic material which each face a permanent magnet (4,4?) with a facing surface when the first part (1) is in an aligned position relative to the second part (2), the gap extending between the two teeth and the corresponding permanent magnets, wherein, when the first part is moving out of the aligned position relative to the second part along a longitudinal axis, the total area of the facing

Abstract: The present invention has an object of providing a cushioning device having a stable and superb vibration-damping property and a metal cover attachable by use of the cushioning device. A cushioning device, which is to be located between an exhaust manifold as a vibration source and a heat insulator as a connection target and connects the exhaust manifold and the heat insulator to each other and cushions transmission of a vibration from the exhaust manifold to the heat insulator, includes a multi-stage coiled and spiral spring for cushioning the vibration, a grommet for joining the multi-stage coiled and spiral spring and the heat insulator to each other, and a collar member located between an attaching bolt tightened to the exhaust manifold and the multi-stage coiled and spiral spring. The multi-stage coiled and spiral spring is formed of a wiring member having a spiral shape as seen in a plan view.

Abstract: An aircraft vehicular assembly is provided that includes a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface contiguous smooth inner surface segment, and a nonelastomeric inner member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer member. The assembly includes an elastomer encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomer has an inner bonding surface segment and an outer grooved elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner member outer bonding surface segment.

Abstract: A surgical retractor including a slab-shaped member having a first edge and a second opposing edge, wherein a deformable elongate member is provided affixed to said first edge, said elongate member comprising an external wall defining an internal chamber, wherein the external wall is configured to be compressible and moldable to a surface, in particular, a human tissue surface within a surgical incision. A curved flexural handle may be provided attached to the second edge.

Abstract: A damping device for damping pressure oscillations within a combustion chamber of a turbine is provided. The damping device has a radially extending damping device body. The damping device body has a radially inner circumferential edge portion and a radially outer circumferential edge portion. A through hole is formed in the damping device body and has a tapered shape.

Abstract: An apparatus and method for attenuating noise and vibration in a propeller aircraft comprises a tuned vibration absorber adapted to be mounted to the skin of a fuselage of a propeller aircraft. The tuned vibration absorber may be tuned to the second harmonic of a blade passage frequency of a propeller of the aircraft. The tuned vibration absorber may be connectable to a separately formed mount, which can be mounted to the fuselage skin independently of the tuned vibration absorber. The apparatus may include a cover to prevent interference between the tuned vibration absorber and other components in the aircraft. The apparatus may be used in combination with other attenuation systems to attenuate noise and vibration over a broad range of frequencies.

Abstract: A damping apparatus for an automobile is provided, capable of ensuring a high level of reliability while obtaining excellent damping effect with simple configuration. The damping apparatus for an automobile that reduces vibrations of an automobile body may include an actuator that is attached to the automobile body and drives an auxiliary mass; a current detector that detects a current flowing through an armature of the actuator; a section that detects a terminal voltage applied to the actuator; a calculation circuit that calculates an induced voltage of the actuator, and further calculates at least one of the relative velocity, relative displacement, and relative acceleration of the actuator, based on a current detected by the current detector and the terminal voltage; and a control circuit that drive-controls the actuator based on at least one of the relative velocity, relative displacement, and relative acceleration of the actuator calculated by the calculation circuit.

Abstract: A mount damper comprises electrode plates placed on a motor side and a support body side respectively, a control unit for adjusting voltage between the electrode plates, and an electrostrictive polymer member for changing a distance between the electrode plates by the voltage therebetween. The electrostrictive polymer member is also an elastic body sandwiched between the electrode plates and has a hardness changeable with a change in the interelectrode distance. A motor is mounted through this mount damper. The control unit adjusts voltage applied between the electrode plates to a value different from a value causing resonance of the motor and the electrostrictive polymer member, thereby absorbing vibration of the motor during rotation thereof, irrespective of a rotation speed. Thus, the mount damper and the image forming apparatus using it can reliably prevent resonance and absorb vibration constantly even if a device selectively uses plural levels of the rotation speed.

Abstract: A cushion for a scraper blade may comprise: a support plate having one or more members for engaging a support; a mounting plate opposite the support plate having a first end to which a scraper blade is mountable and having a second end remote from the first end; and a resilient cushioning material between and adhering to the support plate and the mounting plate. The cushion may further include one or more springs extending between the support plate and the mounting plate, or the resilient cushioning material surrounding the one or more springs, or the mounting plate having holes filled by the resilient cushioning material, or the second end of the mounting plate being formed to extend towards the support plate, or a combination thereof.

Abstract: Disclosed is a damper that is easy to mount and capable of attenuating to a sufficient degree a vibration generated by an electronic component; also disclosed are an electronic component and an electronic apparatus that are provided with such a damper. A mounting insertion portion is provided with a hard portion maintaining the configuration of the mounting insertion portion.

Abstract: A fluid filled type vibration damping device including: a partition member having a communication passage connecting a pressure receiving and equilibrium chambers; an obstructing rubber elastic plate juxtaposed against the communication passage from a pressure receiving chamber side, adapted to obstruct the communication passage, and arranged to be exposed to pressure of the pressure receiving and the equilibrium chamber at both faces; and a constraining member provided for retaining an outer peripheral section of the obstructing rubber elastic plate in contact against the partition member at multiple locations. The constraining member provides an opening/closing control member operated to induce the obstructing rubber elastic plate to push against the partition member and close off the communication passage, and to induce elastic deformation of the obstructing rubber elastic plate to be separated from the partition member.

Abstract: Embodiments of a low frequency isolation device are provided, as are embodiments of a spacecraft isolation system including a plurality of low frequency isolation devices. In one embodiment, the low frequency isolation device includes a three parameter isolator and a break frequency-reducing series spring mechanically coupled in series with the three parameter isolator and having a predetermined axial stiffness (KS AXIAL) and a predetermined lateral stiffness (KS LATERAL). The predetermined axial stiffness (KS AXIAL) of the break frequency-reducing series spring is less than the predetermined lateral stiffness (KS LATERAL) thereof.

Abstract: The invention relates to a damping device (1) for a pole, in particular a trekking, ski, hiking, or Nordic walking pole, having an attaching sleeve (4) by means of which the damping device (1) is attached to a first tube segment (11, 44) by inserting and attaching therein, and having an attaching element (3) by means of which the damping device (1) is attached to a pole handle (5) or a second tube segment (43) having a larger inner diameter than the first tube segment (11, 44).

Abstract: An item assembly and a shock attenuation method for protecting an item comprising providing an item internal to an assembly and encasing the item in a fluid material such that the material and the item are approximately in hydrostatic balance upon an impact event.

Abstract: Systems are provided for damping vibrations from a payload. In an embodiment, and by way of example only, the system includes an isolation strut and a gas line. The isolation strut includes a bellows and a piston. The bellows has a first end and a second end, the first end being enclosed, and the second end attached to the piston to define a chamber. The piston includes a damping annulus therethrough having a gas inlet and a gas outlet. The gas inlet provides flow communication to the chamber of the bellows. The gas line is coupled to the isolation strut and is in fluid communication with the gas outlet thereof. The system is hermetically sealed to contain a gas therein.

Abstract: A suspension system for a seat of a vehicle comprises a base, a linkage, and a seat attached to the base via the linkage. A pneumatic shock absorber provides a respective resistance level against movement of the seat with respect to the base based on a corresponding pressure level of air or gas within the pneumatic shock absorber. A set of cylindrical members are spaced apart beneath the seat. A tension member is arranged to engage the cylindrical members. The tension member is attached to the seat via a bracket. An electric motor is capable of driving one of the cylindrical members. A first sensor is arranged to detect first sensor data associated with an instantaneous position of the seat versus time. A controller generates a first control signal for the electric motor to change a height of the seat in opposition to a change in the instantaneous position of the seat and a second control signal to change the pressure level.

Abstract: An aircraft front nose landing gear having both elastomeric and nonelastomeric elements is provided along with a method of making the same. The aircraft front nose landing gear includes the ability to reduce/inhibit oscillating shimmy rotation vibrations. The method further provides for making a landing gear with a shimmy damper for further reducing oscillating rotations.

Abstract: A vibration absorbing device includes a main board having a pole, a first retaining board fixed to the main board, a second retaining board fixed to the first retaining board opposite to the main board, a loading board including a main body and a flange protruding from the main body, an elastic element located between the pole and the main body. A sliding groove and a compartment are both defined between the first retaining board and the second retaining board, the flange is located but slidable in the sliding groove, the main body is located in the compartment. The loading board can slide in the sliding groove in compliance with shocks or vibration, while the elastic element deforms and releases to absorb the motion of the loading board.

Abstract: A method and apparatus for an adaptive, multi-axis suspension support system providing both coarse and fine suspension to a payload. Coarse suspension control is provided to maintain the payload within a coarse range of position. Fine suspension control is provided by monitoring and analyzing vibration characteristics in both time and frequency domains to determine the required amount of damper resistance to be exerted by a magnetorheological (MR) device.

Abstract: A torsional vibration damping arrangement, particularly for a drivetrain with an automatic transmission, includes an input region and an output region, wherein a first torque transmission path and parallel thereto a second torque transmission path and a coupling arrangement for superposing the torques transmitted via the torque transmission paths are provided between the input region and the output region. The torsional vibration damping arrangement further includes at least in the first torque transmission path a phase shifter arrangement for generating a phase shift of rotational irregularities transmitted via the first torque transmission path relative to rotational irregularities transmitted via the second torque transmission path.

Abstract: A damping apparatus for an automobile is provided, capable of ensuring a high level of reliability while obtaining excellent damping effect with simple configuration. The damping apparatus for an automobile that reduces vibrations of an automobile body may include an actuator that is attached to the automobile body and drives an auxiliary mass; a current detector that detects a current flowing through an armature of the actuator; a section that detects a terminal voltage applied to the actuator; a calculation circuit that calculates an induced voltage of the actuator, and further calculates at least one of the relative velocity, relative displacement, and relative acceleration of the actuator, based on a current detected by the current detector and the terminal voltage; and a control circuit that drive-controls the actuator based on at least one of the relative velocity, relative displacement, and relative acceleration of the actuator calculated by the calculation circuit.

Abstract: A damping system for fittings, in particular for domestic appliances and furniture, comprises a first fitting part (2) which can be moved relative to a second fitting part (3), wherein a damping element (4, 4?) with a housing (5) and a piston (7, 14), which is mounted such that it can move in the housing (5), is provided in order to brake the relative movement of the first fitting part (2) to the second fitting part (3) before an end position is reached, wherein a knitted fabric (6) comprising threads is arranged in the housing (5), it being possible for said knitted fabric to be compressed by the piston (7, 14) for the purpose of damping the movement of the fitting parts (2, 3).

Abstract: The invention is an energy absorbing system for safeguarding structures from disruptive forces, which may be implemented into structures or devices to provide protection from seismic motion, blasts or other disruptive forces, due to the system's displacement and damping characteristics. The system's performance can be better molded analytically to predict performance of the structure under earthquake and wind motions, for example. By utilizing cost effective materials and a simple design, the present invention provides a more efficient cost-effective system for absorbing unwanted energy, for example, a base isolation system.

Abstract: A multipiece cushioning assembly adapted to be arranged in combination with a shock absorbing apparatus. The multipiece cushioning assembly is disposed between a pair of radial shoulders on first and second members telescoping members of the shock absorbing apparatus arranged in operable combination relative to each other. The radial shoulders on the first and second members limit travel of the shock absorbing apparatus, and with said multipiece cushioning assembly including a plurality of elastomeric bumpers arranged in a generally circular array for absorbing over-travel of the first and second members relative to each other and for readily permitting replacement of the multipiece cushioning assembly while maintaining the first and second members in operable combination relative to each other.

Abstract: A system for isolating vibration among a plurality of instruments on a spacecraft includes at least two platforms, each of which is configured to couple to and isolate vibration for a single one of the plurality of instruments. Each of the at least two platforms is configured to mount to the spacecraft. A device is also provided for isolating vibration for one instrument among a plurality of instruments on a spacecraft.

Abstract: A system installed in building foundations to absorb forces from earthquakes. The earthquake force absorption system includes a footing structure extending into a foundation hole, an anchoring substrate lining a bottom of the foundation hole, opposing springs disposed around the footing structure, and attachment plates coupling the springs to the footing structure and the anchoring substrate.