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37results about How to "Reduce micro vibration" patented technology

Six-degree-of-freedom micro vibration abatement platform and control method thereof

The invention discloses a six-degree-of-freedom micro vibration abatement platform. The six-degree-of-freedom micro vibration abatement platform comprises a foundation platform, a load platform, six sets of totally identical single-degree-of-freedom active / passive composite vibration insulating devices, and a controller; and the upper and lower two ends of each set of single-degree-of-freedom active / passive composite vibration insulating devices are respectively connected with the foundation platform and the load platform. A control method comprises logic shaft signal calculation, logic shaft control signal calculation, physical shaft real-time control signal calculation and transfer steps. The six-degree-of-freedom micro vibration abatement platform is simple in structure and adjustable in rigidity, can inhibit and isolate six-degree-of-freedom micro vibration in translation and rotation directions of axles X, Y and Z, can be suitable for different places, can effectively attenuate micro vibration on different frequency bands, provides reliable guarantee to precise machining and measuring equipment under micro vibration environments, solves the problems of complex structure and complex control mode in a traditional active / passive composite vibration insulating mechanism, and realizes multi-degree-of-freedom vibration inhibition.
Owner:HUAZHONG UNIV OF SCI & TECH

Linear vibration motor

The invention discloses a linear vibration motor which comprises a stator assembly, a vibrator assembly and an elastic supporting part, wherein the stator assembly comprises a shell with an accommodating cavity and a magnet positioned in the accommodating cavity and combined and fixed with the shell; the magnet comprises a hollow part; the vibrator assembly comprises a coil arranged on a concentrating flux plate and mass blocks surrounding the periphery of the coil; the hollow part extends along a vibrating direction of the vibrator assembly; when the vibrator assembly vibrates, the coil vibrates along with the vibrator assembly and is inserted into the hollow part of the magnet; the elastic supporting part is configured to suspend the vibrator assembly in the accommodating cavity of the shell; and the concentrating flux plate further comprises a through hole which corresponds to an inner cavity of the coil and runs through the upper surface and the lower surface of the concentrating flux plate. According to the linear vibration motor provided by the invention, the structure can utilize magnetism of the magnet to the greatest extent; utilization efficiency of the coil for magnetic force lines of the magnet is promoted; an electromagnetic driving force of the motor is promoted; and the assembling process is simple and convenient, and assembling accuracy is high, so that the motor can obtain better vibration performance.
Owner:GOERTEK INC

Static pressure air-float guide rail based on double-side symmetrical damp

InactiveCN101373146AClean and pollution-free rigidityHigh viscosityMeasurement apparatus componentsStep responseMotion direction
A static pressured air-float guide rail based on bilateral symmetric damping belongs to the technical field of the precision instrument and measurement. In view of the characteristics of small driving force and large inertia of the air-float guide rail, and according to the properties of step response and shock response of a closed loop control system of the guide rail, a two-way viscous damper is introduced to the system to constitute a part for rate feedback, so that the shortage of damping effect of a differential parameter in a PID controller is relieved, thus increasing the damping ratio of the system, reducing movement over-control, and eliminating proper vibrations caused by random disturbance. Two viscous dampers with the same parameter are symmetrically arranged at the two ends of an air-float cover to form a two-way viscous damper; the intensity of the damping force is proportional to the speed of the air-float cover; the direction of the damping force is aligned with the movement direction of the air-float cover; and the damping coefficient is accurate and adjustable, so that the movement over-control of the guide rail and the proper vibration in the movement direction after positioning are reduced, and the positioning precision and static stability of the guide rail are increased by about one order of magnitude.
Owner:HARBIN INST OF TECH

Three-dimensional vibration isolation device for rail transit

The invention relates to the technical field of vibration and noise control, and discloses a three-dimensional vibration isolation device for rail transit, which comprises an upper connecting plate, a vertical vibration isolation unit, a middle working plate, a horizontal vibration isolation unit and a lower connecting plate sequentially arranged from top to bottom, wherein the vertical vibration isolation unit comprises a box body, a first rubber layer, a spacing plate and a second rubber layer, the first rubber layer, the spacing plate and the second rubber layer are sequentially and fixedly connected in the box body from top to bottom, an opening is formed in one end of the box body, the upper connecting plate is fixed to the opening in a covering mode, and a plurality of vibration isolation springs are fixedly arranged on the first rubber layer and the second rubber layer. And the plurality of vibration isolation springs are coaxially arranged on the first rubber layer or the second rubber layer. Micro vibration induced by rail transit can be effectively reduced, the problem of vibration noise of the upper cover structure of the rail transit can be effectively solved, and a good vibration isolation effect can be achieved for multiple types of vibration sources and horizontal and vertical multi-dimensional vibration input.
Owner:GUANGZHOU UNIVERSITY

Magnetofluid cylindrical roller thrust bearing and processing technology thereof

The invention relates to the technical field of roller bearings, and discloses a magnetofluid cylindrical roller thrust bearing. The magnetofluid cylindrical roller thrust bearing comprises a bearing,a roller retainer, a bezel and a static rack from top to bottom in sequence, and rollers are arranged in the middle of the roller retainer in sequence; the roller retainer and the rollers are all arranged in an annular rolling passage at the upper portion of the bezel together, magnetofluid is injected into the annular rolling passage of the bezel, and an annular gasket and an annular axial permanent magnet are arranged inside an annular groove in the lower portion of the bezel. The invention further discloses a processing technology of the magnetofluid cylindrical roller thrust bearing. According to the magnetofluid cylindrical roller thrust bearing and the processing technology thereof, the magnetofluid is adopted as a thrust bearing lubricant, the bearing running requirements for low friction, micro-vibration and high bearing capacity can be met, the bezel is provided with the annular rolling passage serving as the system for lubrication of the magnetofluid and the rollers, and thepermanent magnet is adopted as an external magnetic field applying source and arranged at the lower portion of the magnetofluid. The magnetofluid cylindrical roller thrust bearing is reasonable in structural design, and particularly suitable for precise instruments with strict operation conditions.
Owner:NANCHANG INST OF TECH

Small hole throttling static pressure thrust gas bearing with accompanying throttling holes

The invention discloses a small hole throttling static pressure thrust gas bearing with accompanying throttling holes, and relates to gas bearings. An air inlet cavity of the bearing is formed in the normal direction of a thrust surface of a bearing body. A main throttling hole and the multiple accompanying throttling holes are connected to the tail end of the air inlet cavity, and the main throttling hole is parallel to the axis of the air inlet cavity. The axes of the accompanying throttling holes are circumferentially and uniformly distributed on the circumference which is away from the axis of the main throttling hole by a distance R. The axes of the accompanying throttling holes are parallel to the axis of the main throttling hole. A pressure cavity vertically communicates with the tail ends of the main throttling hole and the tail ends of the accompanying throttling holes, and the pressure cavity and the main throttling hole are coaxial. The flow of the main throttling hole vertically impacts on the bearing surface to provide main bearing force, along with generation of a large-scale vortex structure in the pressure cavity, the flow of the accompanying throttling holes around the main throttling hole vertically rushes into the pressure cavity, the vortex structure is damaged, the vortex scale is reduced, vortex development is restrained, the internal and external pressure difference of vortexes is reduced, and micro-vibration of the bearing is reduced. The working stability of the bearing is improved.
Owner:BEIHANG UNIV

A solar wing layout structure of a high-precision spacecraft

The invention discloses a solar wing layout structure of a high-precision spacecraft. A top solar wing main plate and top solar wing side plates form a top solar wing which is fixedly installed on a platform top plate through bolts; an included angle between the top solar wing main plate and each top solar wing side plate is 120 degrees; the section of a spacecraft platform is in the shape of a regular hexagon, the top solar wing main plate is rectangular, each top solar wing side plate is triangular, and a bottom solar wing is installed at the bottom of a platform bottom plate; top solar wing honeycomb sandwich embedded parts are pre-embedded in the top solar wing main plate and the top solar wing side plates, and platform top plate honeycomb sandwich embedded parts are pre-embedded in the platform top plate; and a top solar wing pressing rod is installed among the top solar wing main plate, the top solar wing side plates and a payload. The solar wing layout structure disclosed by the invention can effectively improve the connection stiffness between the solar wing and the spacecraft platform so as to reduce the micro-vibration of the solar wing and improve the attitude stability of the spacecraft platform, and has the advantages of simple configuration, convenient connection and obvious effect.
Owner:SHANGHAI SATELLITE ENG INST

Anti-sway vibration isolating device for reducing micro-vibration of flywheel

InactiveCN109356967ADecrease the swing displacement amplitudeReduce micro-vibrationNon-rotating vibration suppressionEngineeringFlywheel
The invention discloses an anti-sway vibration isolating device for reducing micro-vibration of a flywheel, and belongs to the technical field of aerospace equipment. The anti-sway vibration isolatingdevice is provided with a satellite capsule plate, and the upper portion of the satellite capsule plate is fixedly connected with a mounting bracket provided with the flywheel through the vibration isolating device; the vibration isolating device comprises a gasket, a vibration isolating pad and a shaft sleeve, the gasket is in contact with the upper end of the shaft sleeve, the lower end of theshaft sleeve is in contact with the upper surface of the satellite capsule plate, the exterior of the shaft sleeve is sleeved with the vibration isolating pad for absorbing vibration shock, and the vibration isolating pad and the mounting bracket are in flexible contact; and an anti-sway device comprises a sleeve and an anti-sway bar, the outer wall of the sleeve is fixedly connected with the mounting bracket, the inner wall of the sleeve is arranged outside the anti-sway bar in a sleeving manner, an overlapping area of one end of the anti-sway bar and the sleeve is fixedly connected with an energy sucking sleeve, the energy sucking sleeve is in clearance fit with the sleeve, and the other end of the anti-sway bar is fixedly connected with the satellite capsule plate through bolts. The anti-sway vibration isolating device reduces micro-vibration and swing of the flywheel and is simple in structure and light in weight.
Owner:CHANGGUANG SATELLITE TECH CO LTD

Vibration isolation device suitable for satellite control moment gyroscope

The invention provides a vibration isolation device suitable for a satellite control moment gyro, the vibration isolation device comprises a lower mounting plate, an upper mounting plate and a vibration isolation assembly, the vibration isolation assembly comprises a first vibration isolator array and a second vibration isolator array, and the first vibration isolator array is mounted between the lower mounting plate and the upper mounting plate. The second vibration isolator array is mounted on the upper mounting plate, each of the first vibration isolator array and the second vibration isolator array comprises four vibration isolators, and the four vibration isolators are arranged in parallel. According to the invention, the coupling characteristic is designed by considering the mounting requirement of the control moment gyroscope from the actual vibration reduction requirement; The installed vibration isolation assembly is symmetrically and coplanarly arranged, so that the planeness requirement of the control moment gyroscope during installation is ensured, the rigidity center passes through the mass center of the control moment gyroscope, good decoupling characteristics in all directions are achieved, the multi-direction vibration isolation effect is achieved, and more stable and more excellent performance is obtained.
Owner:SHANGHAI SATELLITE ENG INST

Vibration absorption device suitable for satellite platform and using method

The invention relates to a vibration absorption device suitable for a satellite platform and a using method, and the vibration absorption device suitable for the satellite platform comprises a base which is connected to the satellite platform, and the satellite platform is provided with vibration equipment and a sensitive load. A plurality of groups of vibration absorption assemblies are arranged on the base, each group of vibration absorption assembly comprises a mounting rod connected to the base and a mass block assembled on the mounting rod in an exchangeable manner, and the mounting position of the mass block on the mounting rod is adjustable. A mass spring damping system can be formed through the mounting rod and the mass block assembled on the mounting rod, the inherent frequency of the vibration absorption assemblies can be adjusted through the replaceable mass block and the adjustable position of the replaceable mass block on the mounting rod, and resonance of vibrations caused by the vibration absorption assemblies and vibration equipment is facilitated. Therefore, vibration energy generated by the vibration equipment is transferred to the vibration absorption assemblies in a mode that the base is connected with the satellite platform, so that the micro-vibration effect of the system is reduced.
Owner:北京微纳星空科技有限公司 +4

An Electromagnetic Positive and Negative Stiffness Parallel Low Frequency Vibration Isolation Device

The invention discloses an electromagnetic type positive and negative stiffness parallel low-frequency vibration isolation device. The device comprises a foundation platform, an electromagnetic suspension platform, a plurality of supports, center type negative stiffness mechanisms and an external power supply, wherein the electromagnetic suspension platform is fixedly connected with the foundationplatform, the plurality of supports are uniformly distributed along the axial direction of the electromagnetic suspension platform and are fixedly connected with the foundation platform, one center type negative stiffness mechanism is arranged between the electromagnetic suspension platform and each support, and the electromagnetic suspension platform is electrically connected with the external power supply. The device is simple in structure, on-line adjustable in rigidity, free of friction, low in system damping, capable of achieving low inherent frequency and inhibiting and isolating microvibration in the vertical direction, suitable for different cases, capable of effectively attenuating micro vibration in a large-frequency-band range and providing reliable guarantee for precision machining and measuring equipment in a micro-vibration environment.
Owner:SHANGHAI UNIV

Portable electric seismic source device for shallow seismic exploration

The invention provides a portable electric seismic source device for shallow seismic exploration, which comprises a chassis base, a support frame, a storage battery, an energy storage spring, a heavy hammer assembly and a driving assembly, and is characterized in that the support frame is fixed in the middle of the chassis base, and the heavy hammer assembly and the driving assembly are arranged on the support frame; the supporting frame comprises a plurality of stand columns and cross beams, the heavy hammer assembly comprises an upper connecting plate and a hammering rod, the hammering rod is sleeved with the upper connecting plate, stand column holes of the upper connecting plate are connected with the stand columns in a penetrating mode, and the stand columns are connected with the hammering rod in a sliding mode; an energy storage spring is arranged between the upper connecting plate and the cross beam; a motor in the driving assembly is in transmission connection with the input end of a speed reducer through a driving shaft, the driving shaft is arranged in a driving shaft barrel in a penetrating mode, the driving shaft barrel is in transmission connection with the output end of the speed reducer, a driving wheel arranged outside the driving shaft barrel is in transmission connection with a driven wheel arranged outside a driven shaft through a chain, and a stop pin of the chain can abut against a clamping block on the side portion of a hammering rod. The invention has the advantages of large impact energy, flexible control, high signal-to-noise ratio and various triggering styles.
Owner:EASTERN GANSU UNIVERSITY

Vibration-proof worktable for adjusting levelness of microscope and mounting method of vibration-proof worktable

The invention discloses a vibration-proof worktable for adjusting the levelness of a microscope and a mounting method. The worktable comprises a supporting bottom plate and at least three damping supporting units; the damping supporting units are disposed on the lower surface by first mounting holes arranged on the supporting bottom plate, the lower surface is opposite to the upper surface of the supporting bottom plate, each damping supporting unit comprises a spring system and a central shaft, each spring system comprises an upper cover plate, a lower cover plate and a connecting spring, a second mounting hole is arranged in the center of each upper cover plate, an accommodating groove is arranged in the center of each lower cover plate, and each connecting spring is disposed between the corresponding upper cover plate and the corresponding lower cover plate; and each central shaft is arranged in the corresponding spring system, one end of the central shaft is respectively connected with the second mounting hole of the corresponding upper cover plate and the corresponding first mounting hole of the supporting bottom plate in a threaded manner, the other end of the central shaft extends into the accommodating groove of the corresponding lower cover plate, and the other end of the central shaft can axially slide in the corresponding accommodating groove without being in direct contact with the bottom surface of the accommodating groove. By the vibration-proof worktable, the levelness of the microscope is obviously improved, and vibration is reduced.
Owner:PANZHIHUA IRON & STEEL RES INST OF PANGANG GROUP

A Small Orifice Throttle Hydrostatic Thrust Gas Bearing with Accompanying Orifice

The application discloses a small hole throttling static pressure thrust gas bearing with accompanying throttling holes, relating to the gas bearing. The air inlet chamber of the bearing is opened along the normal direction of the thrust surface of the bearing main body. The main throttling hole and multiple accompanying throttling holes are connected to the end of the intake cavity, and the main throttling hole is parallel to the axis of the intake cavity. The axis of the accompanying orifice is evenly distributed on the circumference at a distance R from the axis of the main orifice. The axis of the companion orifice is parallel to the axis of the main orifice. The pressure chamber is vertically communicated with the end of the main orifice and the accompanying orifice, and the pressure chamber is coaxial with the main orifice. The flow of the main orifice vertically impacts on the bearing surface to provide the main bearing capacity. Along with the generation of large-scale vortex structure in the pressure chamber, the flow of the accompanying orifice around the main orifice rushes into the pressure chamber vertically and destroys the vortex structure. Reduce the size of the vortex, inhibit the development of the vortex, and then reduce the pressure difference between the inside and outside of the vortex, reduce the micro-vibration of the bearing, and then improve the working stability of the bearing.
Owner:BEIHANG UNIV

Pouring type bus duct with anti-seismic effect and connection method thereof

The invention discloses a pouring type bus duct with an anti-seismic effect and a connecting method thereof.The pouring type bus duct comprises a bus duct shell and an adjusting assembly, a pouring main body is arranged in the bus duct shell, conductor connecting pieces are poured in the pouring main body, and the outer sides of the conductor connecting pieces are wrapped with insulating damping sleeves; a buffer filling plate is filled between the bus duct shell and the pouring body, an elastic buffer block is arranged in the bus duct shell, guide plate grooves are formed in the outer sides of the two ends of the bus duct shell, adjusting guide plates are connected in the guide plate grooves, adjusting grooves are formed in the adjusting guide plates, and clamping grooves are formed in the peripheries of the outer sides of the two ends of the bus duct shell. The two ends of the lower adjusting seat and the two ends of the upper adjusting seat are clamped at the connecting positions of the two bus duct shells respectively, the bus duct shells and the adjusting assemblies are fixedly connected through locking nuts, the problems that bus duct connection is not stable and the anti-seismic effect is poor due to bus duct vibration can be solved, meanwhile, the installation length of the bus duct can be adjusted, and the service life of the bus duct is prolonged. And the bus duct is convenient to install.
Owner:镇江苏恒电力自动化有限公司
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