None-angular displacement parallel damping device

A vibration damping device and parallel technology, applied in the direction of non-rotational vibration suppression, etc., can solve the problems of limiting the application range of the device, inability to perform vibration isolation, and limiting applications, etc., and achieve the effects of high cost performance, simple structure, and simple processing

Inactive Publication Date: 2014-01-15
YANSHAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Patent CN201834213U proposes a double parallelogram non-angular displacement vibration damping device. The mechanism of this invention is simple, but the device can only reduce vibration in one direction, and cannot perform vibration isolation in other directions, which limits the application range of the device.
The patent publication number is CN101858402A The three-way angular displacement shock absorber proposed can complete three-way vibration isolation, but the mechanism is complicated and the weight is heavy, which limits the application in some cases

Method used

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Examples

Experimental program
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Effect test

Embodiment 1

[0016] figure 1 In the schematic diagram of the structure of the parallel damping device without angular displacement shown, the four branches are all RRC structures, and one end of the connecting rod one 3 in the branch is connected to the fixed platform 1 through the first rotating pair 2, and the above connecting rod one The other end is connected with one end of the connecting rod 2 5 through the second rotating pair 4, and the other end of the connecting rod 2 is connected with the moving platform 8 through the cylinder pair 6, and the above-mentioned second rotating pair is located outside the moving platform and the fixed platform, and the above-mentioned first The axis of the first rotary pair is parallel to the axis of the second rotary pair, and the axis of the second rotary pair is parallel to the axis of the cylindrical pair. The whole device is square, and the four branches are symmetrically and evenly distributed. The four corners between the fixed platform and t...

Embodiment 2

[0018] exist figure 2 In the schematic diagram of the structure of the parallel damping device without angular displacement shown, the four branches are all RRC structures, and one end of the connecting rod one 3 in the branch is connected to the fixed platform 1 through the first rotating pair 2, and the above connecting rod one The other end is connected with one end of the connecting rod 2 5 through the second rotating pair 4, and the other end of the connecting rod 2 is connected with the moving platform 8 through the cylinder pair 6, the above-mentioned second rotating pair is located inside the moving platform and the fixed platform, and the above-mentioned first The axis of the first rotary pair is parallel to the axis of the second rotary pair, and the axis of the second rotary pair is parallel to the axis of the cylindrical pair. The whole device is square, and the four branches are symmetrically and evenly distributed. The four corners between the fixed platform and...

Embodiment 3

[0020] exist image 3 In the schematic diagram of the structure of the parallel damping device without angular displacement shown in the figure, the four branches are all RPC structures, and one end of the connecting rod 3 in each branch is connected to the fixed platform 1 through the rotating pair 2, and the other end of the connecting rod 1 One end is connected with the connecting rod 2 5 through a moving pair 10, the first damping spring 7 is installed in the moving pair, the other end of the connecting rod 2 is connected with the moving platform 8 through a cylindrical pair 6, and the axis of the cylindrical pair is connected The axes of the cylinders are parallel to each other. At the same time, the second damping springs 9 are set on both sides of the cylinder pair respectively. The whole device is square, and the four branches are symmetrically and evenly distributed.

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Abstract

A none-angular displacement parallel damping device mainly comprises a movable platform, a fixed platform, four branches and damper springs, wherein the branches are used for connecting the two platforms and are identical with one another in structure. One end of a first connecting rod in the branches is connected with the fixed platform through a first revolute pair, the other end of the first connecting rod is connected with one end of a second connecting rod through a second revolute pair, and the other end of the second connecting rod is connected with the movable platform through a cylindrical pair. The axis of the first revolute pair is parallel to that of the second revolute pair, and the axis of the second revolute pair is parallel to that of the cylindrical pair. The whole device is square. The four branches are symmetrically and evenly distributed. Four corners between the fixed platform and the movable platform are respectively and perpendicularly provided with one first damper spring, and the two sides of the cylindrical pair are respectively sleeved with one second damper spring. The none-angular displacement parallel damping device is simple in structure, small in occupied size, easy to process and high in cost-performance ratio, and has broad application prospect in many fields.

Description

technical field [0001] The invention relates to a vibration damping device, in particular to a parallel vibration damping platform. Background technique [0002] In recent years, with the development of modern defense science and technology, various vehicle-mounted, ship-borne and airborne military equipment have been widely used. Among them, some precision testing equipment is very expensive and has strict environmental requirements. For example, the testing equipment in missile flight testing is often damaged due to strong vibration during missile flight. In order to protect these precision equipment, it is often necessary to install a vibration damping device between the detection equipment and the missile. Another example is the acquisition of reconnaissance intelligence, where the reconnaissance system is placed on an aircraft or satellite, which expands the dynamic field of view of the optical system, followed by the impact of the vibration of the moving carrier on th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16F15/04
Inventor 赵铁石李二伟崔潇
Owner YANSHAN UNIV
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