1. A space rod structure vibration damper is characterized in that: the particle damper comprises a plurality of particle dampers arranged on a space rod piece structure, wherein each particle damper comprises a shell with an internal closed cavity and a plurality of damping particles which are arranged in the cavity and form a particle medium contact stress network, when the vibration frequency of the space rod piece structure is less than 200Hz, the coefficient of restitution of the damping particles is 0.4-0.7, the coefficient of friction is 0.05-0.3, when the vibration frequency of the space rod piece structure is 200-1000 Hz, the coefficient of restitution of the damping particles is 0.1-0.4, and the coefficient of friction is 0.3-0.55.

2. A space bar structure vibration damper according to claim 1, wherein: the exterior of the damping particles is coated with a packaging layer made of flexible materials, and the flexible materials are plastics or rubber or fibers.

3. A space bar structure vibration damper according to claim 1, wherein: when the vibration frequency of the space rod piece structure is less than 200Hz, the filling rate of the damping particles is set to be between 85% and 90%; when the vibration frequency of the space rod piece structure is 200-1000 Hz, the filling rate of the damping particles is set between 90% and 98%.

4. A space bar structure vibration damper according to claim 1, wherein: when the vibration frequency of the space rod piece structure is less than 200Hz, the inside of the cavity is additionally provided with a partition board to divide the cavity into a plurality of cavities, and the length and the width of each cavity are 19-21 times of the diameter of the damping particles.

5. A space bar structure vibration damper according to claim 1, wherein: when the vibration frequency of the space rod piece structure is 200-1000 Hz, the inner wall surface of the cavity is designed to be an arc surface.

6. A space bar structure vibration damper according to claim 1, wherein: the space rod piece structure is formed by mutually connecting a plurality of parallel plane rod piece structures which are arranged at intervals, the plane rod piece structure comprises an upper chord, a lower chord which is arranged below the upper chord in parallel, a first vertical rod which is respectively fixedly connected with the upper chord and the lower chord to form a rectangular frame, a second vertical rod one end of which is fixedly connected with the center of the upper chord and the other end of which is fixedly connected with the center of the lower chord, first inclined rods which are respectively arranged at two sides of the second vertical rod and one end of which is fixedly connected with the upper chord and the other end of which is fixedly connected with the lower chord, transverse web members of which two ends are fixedly connected with the first inclined rods, and a plurality of second inclined rods, one end of each second inclined rod is fixedly connected with the first inclined rod, and the other end of each second inclined rod is fixedly connected with the second vertical rod; the bottom of the space rod structure is also provided with a base, and a plurality of vibration isolators are arranged between the space rod structure and the base.

7. A space bar structure vibration damper according to claim 1, wherein: the space rod piece structure is a solar wing.

8. A vibration damping method for a space rod structure is characterized in that: mounting a particle damper according to any of claims 1-7 on a spatial rod structure by the following method:

A1. determining the vibration frequency of the space rod piece structure;

A2. adjusting relevant characteristics of the particle damper according to the vibration frequency of the space rod structure:

A21. coefficient of restitution of damping particles: when the vibration frequency of the space rod piece structure is less than 200Hz, damping particles with the coefficient of restitution of 0.4-0.7 are selected; when the vibration frequency of the space rod piece structure is 200-1000 Hz, damping particles with the coefficient of restitution of 0.1-0.4 are selected;

A22. coefficient of friction of damping particles: when the vibration frequency of the space rod piece structure is less than 200Hz, damping particles with the friction coefficient of 0.05-0.3 are selected; when the vibration frequency of the space rod piece structure is 200-1000 Hz, damping particles with the friction coefficient of 0.3-0.55 are selected.

A3. Establishing a finite element model of the space rod structure, adding constraints, carrying out modal analysis on the space rod structure, determining the maximum displacement position or the vibration energy intersection of each order of frequency modes of the space rod structure, and installing the particle damper obtained by adjusting in the step A2 at the maximum displacement position or the energy intersection.

9. A method of damping vibration of a spatial rod structure according to claim 8, wherein: the adjustment of the relevant characteristics of the particle damper in A2 further comprises:

A23. filling rate of damping particles: when the vibration frequency of the space rod piece structure is less than 200Hz, the filling rate of the damping particles is set to be between 85% and 90%; and when the vibration frequency of the space rod piece structure is 200-1000 Hz, setting the filling rate of the damping particles between 90% and 98%.

A24. A cavity structure: when the vibration frequency of the space rod piece structure is less than 200Hz, the interior of the cavity is additionally provided with a partition board to divide the cavity into a plurality of chambers, and the length and width of each chamber are 19-21 times of the diameter of damping particles; and when the vibration frequency of the space rod piece structure is 200-1000 Hz, setting the inner wall surface of the cavity as an arc surface.

10. A method of damping vibration of a spatial rod structure according to claim 8, wherein: the installation positions of the particle damper in A3 are as follows:

when the vibration frequency of the spatial rod structure is close to the Nth order modal frequency, the installation position of the particle damper is the Nth order modal maximum displacement position of the spatial rod structure, wherein N is 1 or 2 or 3; and when the vibration frequency of the space rod structure is close to the modal frequency of more than 3 orders, the installation position of the particle damper is the vibration energy intersection of the space rod structure.

Background

Space bar structures were first found in the aerospace and construction fields and have found widespread use. Solar cell panel supports, radio communication antennas, telescopic mechanical arms, steel frame towers, bridges and the like of satellites and space stations are basically formed by space rod piece structures. The space rod structure is widely applied to a plurality of fields, but the vibration problem of the space rod structure is difficult to avoid all the time, and serious influence is easily caused.

For example, in the field of ships, vibration is generated during the navigation of the ships, which easily affects the safety of the ships and the health of people on the ships, and certain vibration isolation measures are required to be taken for control.

In the building field, as for some high-rise building truss structures, vibration can be generated temporarily when wind power disturbance or earthquake occurs, on one hand, fatigue damage is generated on the structure, the reliability of the structure is reduced, the safety and the durability of the structure are affected, the life and property safety of residents is threatened, on the other hand, noise is generated, the normal life of residents is affected, and vibration needs to be reduced through building vibration isolation products.

In the field of aerospace, as a spacecraft gradually develops towards the direction of high precision and high stability, the loaded payload has high requirement on the attitude stability of a platform, the micro-vibration of the spacecraft platform needs to be reduced as much as possible to improve the attitude stability of the platform, and one of the main sources of the micro-vibration of the spacecraft is the flexible vibration of the solar wing.

The existing spacecraft platform is basically provided with a movable solar wing, the connection rigidity of the movable solar wing and the platform is low, and once the spacecraft carries out orbit transfer or attitude adjustment, micro-vibration can be generated, so that the attitude stability of the platform is reduced. More seriously, when the solar wing enters and exits the sun shadow, the external heat flow is changed violently, which may cause the solar wing to vibrate thermally, and the attitude stability of the spacecraft platform is seriously reduced. In addition, when the flexible solar wing performs orbital transfer and resource adjustment or internal parts perform mechanical motion, the problem that vibration is difficult to automatically attenuate is caused, the normal work of the whole spacecraft is influenced, and even the structural damage of the spacecraft is caused.

It can be seen that the vibration problem of the space rod structure is not negligible.

Disclosure of Invention

In view of the above problems, an object of the present invention is to provide a device and a method for damping vibration of a spatial rod structure, which can effectively improve the damping effect of the spatial rod structure.

In order to achieve the purpose, the technical scheme adopted by the invention is as follows:

the utility model provides a space member structure vibration damper, includes that a plurality of is used for installing the granule attenuator in space member structure, the granule attenuator including inside offer the casing of airtight die cavity and embed a plurality of damping granules that form particle medium contact stress network in the middle of the die cavity, the vibration frequency of space member structure is less than 200Hz, the coefficient of restitution of damping granule is 0.4 ~ 0.7, and coefficient of friction is 0.05 ~ 0.3, when the vibration frequency of space member structure is 200 ~ 1000Hz, the coefficient of restitution of damping granule is 0.1 ~ 0.4, and coefficient of friction is 0.3 ~ 0.55.

Furthermore, the exterior of the plurality of damping particles is covered with a packaging layer made of flexible material, and the flexible material is plastic or rubber or fiber.

Further, when the vibration frequency of the space rod structure is less than 200Hz, the filling rate of the damping particles is set to be between 85% and 90%; when the vibration frequency of the space rod piece structure is 200-1000 Hz, the filling rate of the damping particles is set between 90% and 98%.

Further, when the vibration frequency of the space rod structure is less than 200Hz, the inside of the cavity is additionally provided with a partition plate to divide the cavity into a plurality of cavities, and the length and the width of each cavity are 19-21 times of the diameter of the damping particles.

Further, when the vibration frequency of the space rod piece structure is 200-1000 Hz, the inner wall surface of the cavity is an arc surface.

Furthermore, the space rod structure is formed by connecting a plurality of parallel plane rod structures arranged at intervals, each plane rod structure comprises an upper chord, a lower chord arranged below the upper chord in parallel, a first vertical rod respectively fixedly connected with the upper chord and the lower chord to form a rectangular frame, a second vertical rod with one end fixedly connected to the center of the upper chord and the other end fixedly connected to the center of the lower chord, first inclined rods respectively arranged on two sides of the second vertical rod, one end of each first inclined rod fixedly connected with the upper chord and the other end fixedly connected with the lower chord, a cross web member with two end portions fixedly connected with the first inclined rods, and a plurality of second inclined rods, one end of each second inclined rod is fixedly connected with the first inclined rod, and the other end of each second inclined rod is fixedly connected with the second vertical rod; the bottom of the space rod structure is also provided with a base, and a plurality of vibration isolators are arranged between the space rod structure and the base.

Furthermore, the space rod piece structure is a solar wing.

The invention also discloses a vibration reduction method of the space rod piece structure, the particle damper is arranged on the space rod piece structure, and the installation method of the particle damper comprises the following steps:

A1. determining the vibration frequency of the space rod piece structure;

A2. adjusting relevant characteristics of the particle damper according to the vibration frequency of the space rod structure:

A21. coefficient of restitution of damping particles: when the vibration frequency of the space rod piece structure is less than 200Hz, damping particles with the coefficient of restitution of 0.4-0.7 are selected; when the vibration frequency of the space rod piece structure is 200-1000 Hz, damping particles with the coefficient of restitution of 0.1-0.4 are selected;

A22. coefficient of friction of damping particles: when the vibration frequency of the space rod piece structure is less than 200Hz, damping particles with the friction coefficient of 0.05-0.3 are selected; when the vibration frequency of the space rod piece structure is 200-1000 Hz, damping particles with the friction coefficient of 0.3-0.55 are selected.

A3. Establishing a finite element model of the space rod structure, adding constraints, carrying out modal analysis on the space rod structure, determining the maximum displacement position or the vibration energy intersection of each order of frequency modes of the space rod structure, and installing the particle damper obtained by adjusting in the step A2 at the maximum displacement position or the energy intersection.

Further, the adjustment of the relevant characteristics of the particle damper in a2 further includes:

A23. filling rate of damping particles: when the vibration frequency of the space rod piece structure is less than 200Hz, the filling rate of the damping particles is set to be between 85% and 90%; and when the vibration frequency of the space rod piece structure is 200-1000 Hz, setting the filling rate of the damping particles between 90% and 98%.

A24. A cavity structure: when the vibration frequency of the space rod piece structure is less than 200Hz, the interior of the cavity is additionally provided with a partition board to divide the cavity into a plurality of chambers, and the length and width of each chamber are 19-21 times of the diameter of damping particles; and when the vibration frequency of the space rod piece structure is 200-1000 Hz, setting the inner wall surface of the cavity as an arc surface. Wherein the ratio of the length and width of each chamber to the diameter of the damping particles is preferably close to 20: 1.

Further, the installation positions of the particle damper in a3 are as follows:

when the vibration frequency of the spatial rod structure is close to the Nth order modal frequency, the installation position of the particle damper is the Nth order modal maximum displacement position of the spatial rod structure, wherein N is 1 or 2 or 3; and when the vibration frequency of the space rod structure is close to the modal frequency of more than 3 orders, the installation position of the particle damper is the vibration energy intersection of the space rod structure.

The invention has the following beneficial effects: 1. the vibration damping device and the method provided by the invention can enable the structure of the space rod piece to be fast and stable, have obvious vibration damping effect in a full frequency band, especially a high frequency band, can effectively reduce the amplitude of vibration, reduce the transmission of vibration energy and achieve the peak eliminating effect; 2. according to the vibration frequency or the vibration wavelength of the space rod structure, the configurations of the recovery coefficient of the damping particles, the friction coefficient of the damping particles and the like are adjusted in a targeted manner, so that the vibration reduction effect is better; 3. the vibration damper has the advantages of simple structure, convenience for adjustment according to different vibration conditions, less limitation in use, suitability for various types of space rod piece structures and stronger universality. 4. The inner wall of the cavity is designed into an arc surface, so that the rotary contact area between the damping particles and the cavity can be increased to increase friction energy consumption.

Drawings

FIG. 1 is a schematic view of a particle damper without partition according to an embodiment of the present invention;

FIG. 2 is a schematic view of a particle damper with partition plates according to an embodiment of the present invention;

FIG. 3 is a schematic structural diagram according to a second embodiment of the present invention;

FIG. 4 is a schematic diagram of a third embodiment of the present invention;

FIG. 5 is a diagram illustrating a fourth embodiment of the present invention;

FIG. 6 is a sectional view of a four-particle damper without partition according to an embodiment of the present invention;

FIG. 7 is a sectional view of a four-particle damper with a partition plate according to an embodiment of the present invention.

Description of the main component symbols: 1. a particle damper; 11. a housing; 12. a cavity; 13. damping particles; 14. a partition plate; 15. a packaging layer; 2. a spatial bar structure; 21. a planar bar structure; 211. an upper chord; 212. a lower chord; 213. a first vertical bar; 214. a second vertical bar; 215. a first diagonal member; 216. a second diagonal member; 217. a cross web member; 3. a base; 4. and a vibration isolator.

Detailed Description

The invention is further described with reference to the following drawings and detailed description.

Example one

As shown in fig. 1-2, the invention discloses a vibration damper of a space rod structure, which comprises a plurality of particle dampers 1 arranged on the space rod structure 2, wherein each particle damper 1 comprises a shell 11 internally provided with a closed cavity 12 and a plurality of damping particles 13 arranged in the cavity 12 to form a particle medium contact stress network, when the vibration frequency of the space rod structure 2 is less than 200Hz, the coefficient of restitution of the damping particles 13 is 0.4-0.7, the coefficient of friction is 0.05-0.3, and when the vibration frequency of the space rod structure 2 is 200-1000 Hz, the coefficient of restitution of the damping particles 13 is 0.1-0.4, and the coefficient of friction is 0.3-0.55.

When the vibration frequency of the space rod structure 2 is less than 200Hz, the filling rate of the damping particles 13 is set between 85 percent and 90 percent; when the vibration frequency of the space rod structure 2 is 200-1000 Hz, the filling rate of the damping particles 13 is set between 90% and 98%.

When the vibration frequency of the space rod structure 2 is less than 200Hz, the inner part of the cavity 12 is additionally provided with the partition plates 14 to be divided into a plurality of cavities, and the length and the width of each cavity are set to be 19-21 times of the diameter of the damping particles 13.

When the vibration frequency of the space rod piece structure 2 is 200-1000 Hz, the inner wall surface of the cavity 12 is set to be a cambered surface.

The damping device can enable the space rod piece structure to be fast and stable, has an obvious damping effect in a full frequency band, particularly a high frequency band, is simple in structure and convenient to adjust according to different vibration conditions, and is less in limitation during use and strong in universality. The recovery coefficient and the friction coefficient of the damping particles 13 are adjusted in a targeted manner according to the vibration frequency of the spatial rod structure 2, so that the vibration damping effect of the particle damper 1 can be improved.

Acceleration frequency sweep experiments of 0-200 Hz and 200-1000 Hz are respectively carried out on the space rod piece structure 2, damping particles 13 with different recovery coefficients are selected, other parameters are kept unchanged, and vibration acceleration response peaks of the space rod piece structure 2 after the particle dampers 1 with different recovery coefficients are added are shown in the following table.

TABLE 1 Total effective value of vibration acceleration of spatial rod structure (0-200 Hz) corresponding to granular damping particles with different recovery coefficients

As shown in Table 1, when the spatial rod structure 2 is subjected to 0-200 Hz acceleration frequency sweep experiments, the minimum vibration acceleration effective value of the spatial rod structure 2 is 4.108m/s ^2 when damping particles 13 with the coefficient of restitution of 0.5 are added, and the vibration reduction effect is better than the coefficient of restitution of 0.2-0.4 when the coefficient of restitution of 0.5-0.7 is added.

TABLE 2 Total effective value of vibration acceleration of spatial rod structure (200 Hz-1000 Hz) corresponding to damping particles with different coefficients of restitution

As shown in Table 2, when the acceleration frequency sweep test of 200Hz to 1000Hz is performed on the spatial rod structure 2, the minimum effective value of the vibration acceleration of the spatial rod structure 2 is 7.433m/s ^2 when the damping particles 13 with the coefficient of restitution of 0.2 are added, and the vibration damping effect is better than that of the coefficient of restitution of 0.5 to 0.7 when the coefficient of restitution of 0.2 to 0.4 is added.

TABLE 3 Total effective value of vibration acceleration of spatial bar structure (0-200 Hz) corresponding to particle damping particles with different friction coefficients

As shown in Table 3, when the spatial rod structure 2 is subjected to 0-200 Hz acceleration frequency sweep experiments, the minimum vibration acceleration effective value of the spatial rod structure 2 is 4.108m/s ^2 when damping particles 13 with a friction coefficient of 0.2 are added, and the vibration damping effect is better than the friction coefficient of 0.4-0.5 when the friction coefficient is 0.1-0.3.

TABLE 4 damping particles with different friction coefficients corresponding to the vibration acceleration effective value of the spatial rod structure (200 Hz-1000 Hz)

As shown in Table 4, when the spatial rod structure 2 is subjected to an acceleration frequency sweep test of 200Hz to 1000Hz, the minimum effective value of the vibration acceleration of the spatial rod structure 2 is 7.754m/s ^2 when the damping particles 13 with the friction coefficient of 0.5 are added, and the vibration damping effect is better than the friction coefficient of 0.1 to 0.3 when the friction coefficient is 0.4 to 0.5.

Example two

In addition to the first embodiment, as shown in fig. 3, the spatial rod structure 2 is formed by connecting a plurality of parallel and spaced planar rod structures 21, each of the planar rod structures 21 includes an upper chord 211, a lower chord 212 disposed below the upper chord 211 in parallel, a first vertical rod 213 fixedly connected to the upper chord 211 and the lower chord 212 to form a rectangular frame, a second vertical rod 214 having one end fixedly connected to the center of the upper chord 211 and the other end fixedly connected to the center of the lower chord 212, first diagonal rods 215 respectively disposed on two sides of the second vertical rod 214 and having one end fixedly connected to the upper chord 211 and the other end fixedly connected to the lower chord 212, a cross web 217 having two ends fixedly connected to the first diagonal rods 215, and a plurality of second diagonal rods 216, one end of the second diagonal rods 216 fixedly connected to the first diagonal rods 215 and the other end fixedly connected to the second vertical rods 214.

The space rod structure 2 is a rigid connection structure, vibration is transmitted back and forth in the space rod structure 2 in a wave form, and the vibration is reduced every time the vibration passes through the particle damper 1; after the parameters of the particle damper 1 are adjusted according to the specific wavelength, the vibration reduction effect of 50% -60% can be achieved.

EXAMPLE III

On the basis of the second embodiment, as shown in fig. 4, a base 3 is disposed at the bottom of the space rod structure 2, and a plurality of vibration isolators 4 are disposed between the space rod structure 2 and the base 3.

The rubber vibration isolator is optimized to isolator 4, constitutes the vibration isolation buoyant raft with the combination of space rod structure 2, and when vibration takes place, the particle damper 1 that is located on space rod structure 2 can partly with structural vibration energy consumption in advance, reduces the transmission of vibration energy to isolator 4 direction, effectively improves the high frequency standing wave problem that isolator 4 exists, improves the vibration isolation efficiency of isolator 4, and holistic vibration isolation effect is better.

Example four

On the basis of the first embodiment, as shown in fig. 5 to 7, the exterior of the plurality of damping particles 13 is covered with a packaging layer 15 made of a flexible material, which is plastic or rubber or fiber. The space bar structure 2 is a solar wing. The sectional shape of the housing 11 is made T-shaped for mounting.

The solar wing is an important component of a spacecraft, is a typical large-flexibility space structure, and has dynamic characteristics of low frequency, small damping and the like. In order to improve the vibration suppression capability of the solar wing, the particle damper 1 is arranged on the solar wing structure, so that the vibration can be controlled on the premise of not influencing the original structure and function of the original solar wing. In order to avoid the influence of the difference of the particle dampers 1 on the solar wings on the two sides of the spacecraft on the attitude angle of the spacecraft, the consistency of the parameters and the structural distribution of the particle dampers 1 on the solar wings on the two sides of the spacecraft needs to be ensured during installation.

In addition, because the spacecraft is in a space microgravity environment, after the particle damper 1 is installed, the damping particles 13 are suspended in the cavity 12, in order to ensure that the damping particles 13 can collide and rub with the wall surface of the cavity 12 in the vibration process to achieve the purpose of consuming vibration energy, a plurality of cavities need to be divided by adding the partition plates 14 in the cavity 12, and the particle damper 1 with high filling rate of the damping particles 13 is selected.

EXAMPLE five

On the basis of the above embodiment, the present invention also discloses a vibration damping method for a spatial rod structure, wherein the particle damper 1 is installed on the spatial rod structure 2, and the installation method for the particle damper 1 is as follows:

A1. determining the vibration frequency of the spatial bar structure 2;

A2. the relevant characteristics of the particle damper 1 are adjusted according to the vibration frequency of the spatial rod structure 2:

A21. coefficient of restitution of the damping particles 13: when the vibration frequency of the space rod piece structure 2 is less than 200Hz, the damping particles 13 with the coefficient of restitution of 0.4-0.7 are selected; when the vibration frequency of the space rod piece structure 2 is 200-1000 Hz, the damping particles 13 with the coefficient of restitution of 0.1-0.4 are selected;

A22. coefficient of friction of the damping particles 13: when the vibration frequency of the space rod piece structure 2 is less than 200Hz, the damping particles 13 with the friction coefficient of 0.05-0.3 are selected; when the vibration frequency of the space rod structure 2 is 200-1000 Hz, the damping particles 13 with the friction coefficient of 0.3-0.55 are selected.

A3. Establishing a finite element model of the space rod piece structure 2, adding constraints, performing modal analysis on the space rod piece structure 2, determining the maximum displacement position or the energy intersection of each order of frequency modal of the space rod piece structure 2, and installing the particle damper 1 obtained by adjusting in the step A2 at the maximum displacement position or the energy intersection.

The adjustment of the relevant characteristics of the particle damper 1 in a2 further includes:

A23. filling rate of the damping particles 13: when the vibration frequency of the space rod structure 2 is less than 200Hz, the filling rate of the damping particles 13 is set between 85 percent and 90 percent; when the vibration frequency of the space rod structure 2 is 200-1000 Hz, the filling rate of the damping particles 13 is set between 90% and 98%.

A24. A cavity structure: when the vibration frequency of the space rod piece structure 2 is less than 200Hz, the interior of the cavity is additionally provided with a partition board to divide the cavity into a plurality of chambers, and the length and width of each chamber are 19-21 times of the diameter of the damping particles 13; when the vibration frequency of the space rod piece structure 2 is 200-1000 Hz, the inner wall surface of the cavity is set to be an arc surface.

The installation positions of the particle damper 1 in A3 are as follows:

when the vibration frequency of the spatial rod piece structure 2 is close to the nth order modal frequency, the installation position of the particle damper 1 is the nth order modal maximum displacement position of the spatial rod piece structure 2, wherein N is 1 or 2 or 3; when the vibration frequency of the space rod structure 2 is close to the modal frequency above 3 rd order, the installation position of the particle damper 1 is the vibration energy intersection of the space rod structure 2.

When the vibration frequency of the space rod piece structure 2 is in a low frequency band below 200Hz, the vibration of the space rod piece structure 2 system causes the vibration of the damping particle 13 system, micro collision and micro rotation motion are generated among the particles, wherein the micro collision energy consumption motion ratio is larger, and the damping particles 13 with higher coefficient of restitution and lower friction coefficient are selected, so that the vibration damping effect is better; meanwhile, because the micro-collision energy consumption is larger, in order to increase the collision frequency between the damping particles 13 and the inner wall of the cavity 12, the filling rate of the damping particles 13 is set to be lower, and the partition plates 14 are additionally arranged in the cavity 12 to divide the cavity into a plurality of cavities, so that sufficient collision spaces can be provided between the damping particles 13 and the inner wall of the cavity 12.

When the vibration frequency of the space rod piece structure 2 is in a high frequency band of 200-1000 Hz, micro-collision and micro-rotation movement are generated before particles, but the energy consumption ratio of the micro-rotation movement is larger, so that the damping particles 13 with lower coefficient of restitution and higher friction coefficient are selected, and the vibration reduction effect can be improved. And because the energy consumption of the micro-rotation movement is larger, the cavity 12 can be not divided into chambers, and the higher filling rate of the damping particles 13 is suitable to be set, and the cavity 12 or the inner wall surfaces of the divided chambers are designed into arc surfaces, so that the contact and friction between the damping particles 13 and the inner wall surfaces of the cavity 12 are increased, the friction energy consumption is increased, and the vibration damping effect is improved.

While the invention has been particularly shown and described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.