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56results about How to "Meet the needs of vibration reduction" patented technology

Micro-vibration convergence type vibration isolation device used for satellite flywheel

ActiveCN104373503AEnsuring and improving designAchieve lightweightRotating vibration suppressionUpper jointFlywheel
The invention provides a micro-vibration convergence type vibration isolation device used for a satellite flywheel. The micro-vibration convergence type vibration isolation device comprises an upper platform, linings, lower joint pieces, a lower platform, fixed pieces, damping layers, movable pieces, vibration isolators and upper joint pieces. Three trapezoid corners which are evenly distributed are arranged on the upper platform in the circumferential direction, and a plurality of first apertures with the diameter of 3.3 mm are formed in the trapezoid corners and used for being connected with the upper joint pieces. Three grooves which are evenly distributed and used for being connected with the lower joint pieces are formed in the lower platform in the circumferential direction. The upper joint pieces, the vibration isolators, the movable pieces, the damping layers, the fixed pieces and the linings are combined to form three vibration isolator assemblies, the three axes of the three vibration isolator assemblies are converged at one point, and the convergence point is located above the upper platform. The upper platform and the lower platform are connected through the lower joint pieces and the vibration isolator assemblies. The damping layers are clamped between the fixed pieces and the movable pieces. The micro-vibration responses caused when the flywheel operates on orbit can be remarkably reduced, and the stability, reliability and safety of the high-accuracy sensitive load on a satellite are ensured.
Owner:SHANGHAI SATELLITE ENG INST

Micro-vibration parallel connection vibration isolation device for satellite control moment gyro group

The invention provides a micro-vibration parallel connection vibration isolation device for a satellite control moment gyro group. The control moment gyro group comprises m control moment gyros, wherein m is larger than or equal to 3 and is smaller than or equal to 6. The control moment gyros are evenly installed on the periphery close to the circle center of a satellite cellular board. The micro-vibration parallel connection vibration isolation device is mainly composed of vibration isolator assemblies located between a satellite load-bearing cylinder and a satellite cellular board. Each vibration isolator assembly comprises an upper connecting rod, a lower connecting rod, a vibration isolator, a movable plate, a damping layer and a static plate, wherein the upper connecting rod is connected with the load-bearing cylinder, the lower connecting rod is connected with the cellular board, and the vibration isolator, the movable plate, the damping layer and the static plate are located between the upper connecting rod and the lower connecting rod and sequentially connected through connecting pieces. The number of the vibration isolator assemblies is 2n, wherein n is larger than or equal to 3 and is smaller than or equal to 8. Every two adjacent vibration isolator assemblies form one set through an upper adapter and fixed to the satellite cellular board through a lower adapter. The n sets of vibration isolator assemblies are evenly distributed in the circumferential direction of the satellite cellular board. According to the micro-vibration parallel connection vibration isolation device, interference, formed by micro-vibration response caused during in-orbit operation of the CMGs, on sensitive loads can be remarkably lowered, and stability, reliability and safety of the satellite-borne high-precision sensitive loads during in-orbit operation are ensured.
Owner:SHANGHAI SATELLITE ENG INST

Vibration damping box with adjustable rigidity and damping

The invention discloses a vibration damping box with adjustable rigidity and damping, which is suitable for transporting various boxed materials with a vibration damping requirement and has the advantages of simple structure and convenience for use. Fixing supports are respectively at corners of a box body. A material fixing frame is arranged in the box body. The material fixing frame is provided with a plurality of material fixing holes. A vibration isolator is mounted between the material fixing frame and each fixing support. An acute angle formed by the bearing surface of each vibration isolator and a horizontal direction is 45 DEG. A gasket for adjusting the mounting size of the vibration isolator is arranged between each vibration isolator and the corresponding fixing support. The vibration damping box disclosed by the invention has the beneficial effects that the vibration isolators with different vibration damping properties can be mounted between the fixing supports and the material fixing frame by changing the mounting size of each vibration isolator, so that the different vibration damping requirements of the materials in the box can be met. The vibration damping box not only can meet the vibration damping requirements of the transported materials with different quality but also can meet the vibration damping requirements of the different transportation manners by mounting different models and different types of the vibration isolators.
Owner:MILITARY TRANSPORTATION UNIV PLA

Intelligent self-energized absorber

The invention discloses an intelligent self-energized absorber which comprises a piston, a piston rod, an outer cylinder and an inner cylinder. The piston rod is fixedly connected to the inner side of the outer cylinder, the piston is located inside the inner cylinder and is capable of moving up and down relative to the inner cylinder, a ball shaft sleeve is embedded on the inner wall of the outer cylinder, the outer wall of the inner cylinder is vertically sleeved with a plurality of piezoelectric rings, and the inner cylinder is then arranged in the ball shaft sleeve of the inner wall of the outer cylinder in a sleeved mode. Electrorheological elastic bodies are filled in the space, located above and below the piston, in the inner cylinder, and the electrorheological elastic bodies, the piezoelectric rings and an electronic control module are electrically connected. Energy generated by vibration of vehicles can be obtained, vehicle vibration information can be collected, the captured energy is used for supplying power for the electrorheological elastic bodies, the vibration information is used for self-adaptive control, different voltages are provided to control the damping of the electrorheological elastic bodies according to different road conditions, the absorber is made to meet the vibration reduction demands of the different road conditions, and therefore the riding comfortableness and the handling stability of vehicles can be improved.
Owner:HUNAN INSTITUTE OF ENGINEERING

Mechanical frequency modulation type dynamic absorber for satellite flywheel

The invention relates to a mechanical frequency modulation type dynamic absorber for a satellite flywheel. A guide rod is vertically fixed to the center of a bottom plate. A shock absorption mass block horizontally moves in the axial direction of the guide rod through a linear bearing. Linear modules are symmetrically arranged on the two sides of the guide rod. The mechanical frequency modulation type dynamic absorber comprises a guide rail, a ball screw, a ball nut sliding block, a leaf spring assembly and a motor connection seat, wherein the guide rail is fixed to the bottom plate, the ball screw is arranged on the guide rail, the ball nut sliding block is arranged on the ball screw, the leaf spring assembly is connected between the shock absorption mass block and the ball nut sliding block. The motor connection seat is fixed to one end of the guide rail. By adoption of the symmetrical structural design, the inherent structure frequency is adjusted according to the mechanical frequency modulation principle and changes of the rotation speed of the flywheel, vibration of the flywheel is controlled and restrained to a low order, stability and reliability of the on-satellite high-accuracy sensitivity load in-orbit operation are ensured, and the mechanical frequency modulation type dynamic absorber has the advantages that the frequency tracing speed is high, the vibration absorption performance is excellent, the structure is simple, reliability is high, assembly is convenient, and the manufacturing cost is low.
Owner:SHANGHAI SATELLITE ENG INST

Microvibration Parallel Vibration Isolation Device for Satellite Control Moment Gyroscope Group

The invention provides a micro-vibration parallel connection vibration isolation device for a satellite control moment gyro group. The control moment gyro group comprises m control moment gyros, wherein m is larger than or equal to 3 and is smaller than or equal to 6. The control moment gyros are evenly installed on the periphery close to the circle center of a satellite cellular board. The micro-vibration parallel connection vibration isolation device is mainly composed of vibration isolator assemblies located between a satellite load-bearing cylinder and a satellite cellular board. Each vibration isolator assembly comprises an upper connecting rod, a lower connecting rod, a vibration isolator, a movable plate, a damping layer and a static plate, wherein the upper connecting rod is connected with the load-bearing cylinder, the lower connecting rod is connected with the cellular board, and the vibration isolator, the movable plate, the damping layer and the static plate are located between the upper connecting rod and the lower connecting rod and sequentially connected through connecting pieces. The number of the vibration isolator assemblies is 2n, wherein n is larger than or equal to 3 and is smaller than or equal to 8. Every two adjacent vibration isolator assemblies form one set through an upper adapter and fixed to the satellite cellular board through a lower adapter. The n sets of vibration isolator assemblies are evenly distributed in the circumferential direction of the satellite cellular board. According to the micro-vibration parallel connection vibration isolation device, interference, formed by micro-vibration response caused during in-orbit operation of the CMGs, on sensitive loads can be remarkably lowered, and stability, reliability and safety of the satellite-borne high-precision sensitive loads during in-orbit operation are ensured.
Owner:SHANGHAI SATELLITE ENG INST

Leaf spring combined dynamic absorber for satellite flywheel

The invention discloses a leaf spring combined dynamic absorber for a satellite flywheel. A connecting base is fixed on a base plate; a guide rail is fixed at one end of the connecting base; a ball screw is arranged on the guide rail; a ball nut sliding block is arranged on the ball screw; a switchover block is arranged on the ball nut sliding block; a leaf spring assembly comprises two groups of leaf springs; one ends of the two groups of leaf springs are respectively connected with two sides of a vibration absorbing mass block, and the other ends of the two groups of leaf springs are respectively connected with the switchover block and the base plate. The leaf spring combined dynamic absorber disclosed by the invention is designed in a lightweight manner, utilizes the combined springs to modulate the frequency, adjusts the inherent frequency of the structure according to change of the revolving speed of the flywheel, controls and restrains the vibration of the flywheel at a lower magnitude, ensures high stability and reliability of in-orbit operation of the high-precision sensitive load on the satellite, and has the advantages of high frequency tracking speed, excellent vibration damping performance, simplicity in structure, high reliability, good convenience in assembly and low manufacturing cost.
Owner:SHANGHAI SATELLITE ENG INST

Production process for ethylene propylene diene monomer microporous base plate and product produced by production process

The invention discloses a production process for an ethylene propylene diene monomer microporous base plate. The production process comprises the following steps: adding ethylene propylene diene monomer into a kneading machine to knead, and then adding zinc oxide, stearic acid, carbon black, a moisture absorbent, an acid and alkali regulator, a softening agent and an inorganic filler into the kneading machine to knead, thereby preparing a master batch; adding the prepared master batch into an open mixing machine, adding a vulcanizing agent, a promoter, a foaming agent and a foaming aid, uniformly mixing, regulating roll spacing to 0.8-1.3 millimeters for thin-passing, carrying out triangular packaging for 3-4 times, regulating the roll spacing to 5-6 millimeters for discharging, so as to prepare a rubber compound, and standing the rubber compound for not smaller than 16 hours; putting the rubber compound on a cutter for cutting; feeding prepared rubber strips into a cold feeding extruder to extrude; sequentially feeding the prepared rubber strips into a high-temperature section, a microwave section and an oven section to carry out continuous vulcanizing until complete vulcanizing; and pulling the prepared vulcanized rubber into the cutter through a pulling machine, and cutting the prepared vulcanized rubber into a needed dimension, thereby obtaining a microporous base plate finished product. The invention further provides an ethylene propylene diene monomer microporous base plate.
Owner:ZHUZHOU TIMES NEW MATERIALS TECH

Vibration isolation device of satellite control moment gyro

The invention provides a vibration isolation device of a satellite control moment gyro, which is used for vibration isolation of the control moment gyro and comprises vibration isolator assemblies and a cellular plate, wherein the vibration isolator assemblies are disposed on the cellular plate; the vibration isolator assembly comprises a sealing cover, a connecting rod, a vibration isolator, a damping layer, a switch-over part and a base, the connecting rod, the vibration isolator, the damping layer, the switch-over part and the base are connected in sequence; the sealing cover is disposed on the outer side of the connecting rod, the vibration isolator and the damping layer; the base is connected to the cellular plate; and the connecting rod is used to connect the control moment gyro. Quantity of the vibration isolator assemblies is four; the four vibration isolator assemblies are distributed in a rectangular manner; and the two adjacent vibration isolator assemblies are distributed symmetrically. The vibration isolation device of the satellite control moment gyro provided by the invention is rational in structural design, can significantly reduce interference of micro-vibration responses caused by the control moment gyro during in-track running to a sensitive load, and ensures stability, reliability and safety of the high-precision sensitive load on a satellite during the in-track running.
Owner:SHANGHAI SATELLITE ENG INST

Single-rod air bag type magnetorheological damper

The invention discloses a single-rod air bag type magnetorheological damper, which comprises a working cylinder, an electric magnet, a damping bar and an air bag, wherein the working cylinder is cylindrical, and an end cover is respectively fixed on the upper end and the lower end of the working cylinder; a hole is arranged in the centre of the upper end cover and a sliding bearing is arranged inside the hole; the inner diameter of the working cylinder is larger than the outer diameter of the air bag; the distance between the upper end cover and the lower end cover of the working cylinder is greater than the height of the air bag; the air bag is installed on the bottom inside the working cylinder; one end of the air bag is fixed with the lower end cover of the working cylinder, and the other end of the air bag is fixed with one end of the damping bar; and the other end of the damping bar extends out of the interior of the working cylinder through a bearing on the upper end cover of the working cylinder; a magnetorheological fluid injected in the working cylinder is higher than the air bag and the height of the magnetorheological fluid injected in the working cylinder is less than the distance between the upper end cover and the lower end cover of the working cylinder; and the electric magnet is fixed on the outer circle of the working cylinder.
Owner:谢宁

Method for Improving Vibration Reliability of Metal-Rubber Joint and Metal-Rubber Joint Component

The invention provides a method for improving vibration attenuation reliability of metal rubber joints. The two metal rubber joints, an inner cylinder and an outer cylinder are included. The method is characterized in that the outer cylinder is arranged on the periphery of the inner cylinder to form an annular cylinder; the two metal rubber joints are both installed in the portion, between the inner cylinder and the outer cylinder, of the annular cylinder in a press-fit manner; a joint bearing is arranged between the two metal rubber joints; the inner cylinder is sleeved with an inner ring of the joint bearing; an outer ring of the joint bearing makes contact with the inner surface of the outer cylinder; deformation of the metal rubber joints makes the inner ring and the outer ring of the joint bearing slide relative to each other; the axial and radial rigidity of the metal rubber joints is increased through the joint bearing; overload protection is formed for the metal rubber joints; partial torsional rigidity of the metal rubber joints is reduced through the relative sliding of the inner ring and the outer ring of the joint bearing; and the purpose of improving the vibration attenuation reliability of the metal rubber joints is achieved. The invention further provides a metal rubber joint assembly.
Owner:ZHUZHOU TIMES NEW MATERIALS TECH

Self-Powered Smart Shock Absorber

The invention discloses an intelligent self-energized absorber which comprises a piston, a piston rod, an outer cylinder and an inner cylinder. The piston rod is fixedly connected to the inner side of the outer cylinder, the piston is located inside the inner cylinder and is capable of moving up and down relative to the inner cylinder, a ball shaft sleeve is embedded on the inner wall of the outer cylinder, the outer wall of the inner cylinder is vertically sleeved with a plurality of piezoelectric rings, and the inner cylinder is then arranged in the ball shaft sleeve of the inner wall of the outer cylinder in a sleeved mode. Electrorheological elastic bodies are filled in the space, located above and below the piston, in the inner cylinder, and the electrorheological elastic bodies, the piezoelectric rings and an electronic control module are electrically connected. Energy generated by vibration of vehicles can be obtained, vehicle vibration information can be collected, the captured energy is used for supplying power for the electrorheological elastic bodies, the vibration information is used for self-adaptive control, different voltages are provided to control the damping of the electrorheological elastic bodies according to different road conditions, the absorber is made to meet the vibration reduction demands of the different road conditions, and therefore the riding comfortableness and the handling stability of vehicles can be improved.
Owner:HUNAN INSTITUTE OF ENGINEERING

Frictional damping dynamic vibration absorber

ActiveCN107314072AHigh damping efficiencyReduce the quality ratio index requirementsShock absorbersRange of motionInverted-T shape
The invention discloses a frictional damping dynamic vibration absorber. The frictional damping dynamic vibration absorber comprises an inverted-T-shaped base (5) connected with the opening end of a spherical shell (3). An elastic sleeve (4) is fixedly connected between the inverted-T-shaped base and the opening end of the spherical shell. A vibration damping cavity (10) defined by the spherical shell (3) is filled with a plurality of vibration damping balls (2). An adjusting nut (1), which is screwed out upwards or screwed in downwards to change the size of the vibration damping cavity, is arranged on the upper part, corresponding to the opening of the spherical shell, of the spherical shell and is used for adjusting the movement range of the vibration damping balls in the vibration damping cavity. According to the inherent frequency of a printed-circuit board (PCB), the number of the vibration damping balls filling the vibration damping cavity is calculated through a dynamic vibration absorption theoretical formula. By adopting the frictional damping dynamic vibration absorber, the problems that an existing vibration absorber is provided with an electromagnetic source and a power source which are likely to generate radiated interference on electronic equipment, and cannot be used for damping vibration of a small thin-board structure of the PCB due to the large size and weight in the prior art are solved. The frictional damping dynamic vibration absorber has the characteristics of good vibration damping effect, small size and weight and the like and meets the requirements for vibration damping of PCBs under the condition of the high vibration magnitude.
Owner:10TH RES INST OF CETC

Cylindrical eddy current damping device, damping regulation method and bridge vibration attenuation structure

The invention discloses a cylindrical eddy current damping device, a damping regulation method and a bridge vibration attenuation structure, and relates to the technical field of vibration attenuationdevices. The damping device comprises a supporting frame, a mass block, an induction strong magnet, a straight line guide rail and a copper pipe, wherein the induction strong magnet comprises a firstinduction strong magnet and a second induction strong magnet; the copper pipe comprises a first copper pipe and a second copper pipe; the first induction strong magnet and the second induction strongmagnet are respectively arranged at two sides of the mass block; the first copper pipe and the second copper pipe are respectively arranged at two sides of the supporting frame; when the mass block vibrates, the first induction strong magnet and the second induction strong magnet respectively carry out reciprocating motion in the first copper pipe and the second copper pipe. According to the damping regulation method, the internal radius and the external radius of the copper pipe and the size of the induction strong magnet are regulated to realize different damping coefficients. The bridge vibration attenuation structure comprises the damping device. Through a Ferrari electromagnetic induction principle, the energy of structure vibration is adsorbed, and a damping proportionality coefficient can be conveniently regulated.
Owner:CHINA RAILWAY BRIDGE SCI RES INST LTD +1

Elevator traction machine shock absorber based on multi-layer metal rubber and its working method

The invention relates to an elevator tractor damper based on multilayer metal rubber. The elevator tractor damper comprises a base, wherein at least four cushion fixing seats are symmetrically arranged on the upper end surface of the base, a boss is arranged in the center of the cushion fixing seats, hemispherical high-density metal rubber is arranged above the cushion fixing seats, a groove whichis matched with the boss in the center of the cushion fixing seats so as to limit the high-density metal rubber to slide is formed in the center of the hemispherical plane of the high-density metal rubber, hemispherical low-density metal rubber is arranged above the high-density metal rubber, and a hemispherical groove which is matched with the hemispherical curved surface of the high-density metal rubber is formed in the center of the hemispherical plane of the low-density metal rubber. The invention further relates to a working method of the elevator tractor damper based on the multilayer metal rubber. According to the elevator tractor damper, vibration in all directions can be absorbed by the hemispherical high-density metal rubber and the hemispherical low-density metal rubber, and limiting can be performed by a limiting stop block.
Owner:FUZHOU UNIV
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