Vortex vibration suppression method and device based on cylindrical structure and medium

Abstract

The invention relates to the technical field of vortex-induced vibration, in particular to a vortex-induced vibration suppression method and device based on a cylindrical structure and a medium. The method comprises the steps that wind-induced torque parameters and friction torque parameters borne by the vortex-induced vibration suppression system under the action of target incoming wind are obtained; judging whether a wind-induced torque parameter is greater than the friction torque parameter, and if not, adjusting a pneumatic measure design parameter; whether the wind attack angle is smaller than a preset wind attack angle or not is judged, and if not, pneumatic measure design parameters are adjusted; acquiring a first vortex-induced vibration parameter after the vortex-induced vibration suppression system is applied and a second vortex-induced vibration parameter when the vortex-induced vibration suppression system is not applied; and if the first vortex-induced vibration parameter is greater than or equal to the second vortex-induced vibration parameter, adjusting the pneumatic measure design parameter. The vortex-induced vibration suppression system can rotate to the wake flow to reach a balance state under the action of the target incoming wind, so that the vortex-induced vibration effect of the cylindrical structure is effectively reduced or the vortex-induced vibration effect is directly suppressed.

Description

Background Art

[0002] In the field of structural wind engineering, wind turbine tower (circular column) structures are prone to vortex vibration effect under the action of wind load, which will seriously affect the safety of the tower structure. Although vortex vibration (vortex-induced vibration) will not directly cause structural dynamic instability and destruction, vortex vibration with a larger amplitude will reduce the assembly accuracy during construction, increase the difficulty of construction, endanger the safety of construction personnel, affect the safety of the structure during operation, reduce fatigue life, and thus affect the normal use of the structure. Therefore, the present application proposes a vortex vibration suppression method based on a circular column structure to suppress the occurrence of vortex vibration or reduce the impact of vortex vibration and improve the safety of the structure. Summary of the invention

[0003] The present application provides a vortex vibration suppression method, device and medium based on a circular column structure to solve one or more technical problems existing in the prior art and at least provide a beneficial choice or create conditions.

[0004] Other features and advantages of the present application will become apparent from the following detailed description, or may be learned in part by the practice of the present application.

[0005] According to one aspect of an embodiment of the present application, a vortex vibration suppression method based on a circular column structure is provided, which is applied to a vortex vibration suppression system. The vortex vibration suppression system can rotate around the circular column structure under the action of a target incoming wind. The method includes:

[0006] Acquiring wind-induced moment parameters to which the vortex-oscillation suppression system is subjected under the action of the target incoming wind, wherein the wind-induced moment parameters are used to cause the vortex-oscillation suppression system to rotate around the circular column structure;

[0007] Obtaining friction torque parameters to which the vortex vibration suppression system is subjected when rotating around the circular column structure;

[0008] determining whether the wind-induced torque parameter is greater than the friction torque parameter, and if not, adjusting aerodynamic measure design parameters of the vortex vibration suppression system until the wind-induced torque parameter is greater than the friction torque parameter;

[0009] In the case where the wind-induced torque parameter is greater than the friction torque parameter, determining whether a wind attack angle formed by the vortex vibration suppression system and the direction of the target incoming wind at the wake of the target incoming wind is less than a preset wind attack angle, and if not, adjusting aerodynamic measure design parameters of the vortex vibration suppression system until the wind attack angle is less than the preset wind attack angle;

[0010] When the wind attack angle is less than the preset wind attack angle, obtaining a first vortex-vibration parameter to which the circular column structure is subjected after the vortex-vibration suppression system is applied and a second vortex-vibration parameter to which the circular column structure is subjected when the vortex-vibration suppression system is not applied;

[0011] If the first vortex-oscillation parameter is greater than or equal to the second vortex-oscillation parameter, the aerodynamic measure design parameters of the vortex-oscillation suppression system are adjusted until the first vortex-oscillation parameter is less than the second vortex-oscillation parameter.

[0012] In one embodiment of the present application, based on the aforementioned scheme, the vortex vibration suppression system includes a partition plate device, a pulley device and an annular track device surrounding the circular column structure, the pulley device slides in the annular track device and is connected to the partition plate device; under the action of the target incoming wind, the pulley device drives the partition plate device to rotate around the circular column structure; the aerodynamic measure design parameters include the number of partition plates in the partition plate device, the angles between each of the partition plates, the overall size parameters of each of the partition plates, the opening parameters of each of the partition plates and the number of pulleys in the pulley device.

[0013] In one embodiment of the present application, based on the above-mentioned solution, the partition plate device includes a first partition plate and a second partition plate, and the step of obtaining the wind-induced moment parameter to which the vortex vibration suppression system is subjected under the action of the target incoming wind includes:

[0014] Obtaining the driving torque generated by the first partition plate under the action of the target incoming wind;

[0015] Obtaining the drag torque generated by the second partition plate under the action of the target incoming wind flow;

[0016] The wind-induced torque parameter is determined according to the propulsive torque and the resistive torque.

[0017] In one embodiment of the present application, based on the above solution, obtaining the driving torque generated by the first partition plate under the action of the target incoming wind includes:

[0018] Obtaining the incoming wind speed of the target incoming wind, the characteristic diameter of the vortex vibration suppression system, the air density of the environment in which the circular column structure is located, the first length of the first partition plate, and the drag coefficient of the vortex vibration suppression system under the action of the target incoming wind;

[0019] determining the thrust exerted on the first partition plate by the target incoming wind according to the incoming wind speed, the characteristic diameter, the air density, the first length and the drag coefficient;

[0020] Acquire the diameter of the circular column structure, the first distance between the first partition plate and the outer surface of the circular column structure, and the dynamic wind attack angle formed by the direction of the target incoming wind and the central axis of the vortex vibration suppression system;

[0021] Inputting the thrust, the diameter, the first distance, the first length, and the dynamic wind attack angle into a preset first calculation formula to obtain the propulsion torque;

[0022] Wherein, the preset first calculation formula is:

[0023]

[0024] In the formula, F D1 is the thrust, D is the diameter, L is the first length of the first partition plate, θ is the dynamic wind attack angle, l is the first distance, M D1 is the thrust torque.

[0025] In one embodiment of the present application, based on the above solution, obtaining the drag torque generated by the second partition plate under the action of the target incoming wind includes:

[0026] Obtaining a second length of the second partition plate and a second distance between the second partition plate and the outer surface of the circular column structure, and determining the resistance of the second partition plate under the action of the target incoming wind according to the incoming wind speed, the characteristic diameter, the air density, the second length and the drag coefficient;

[0027] Input the resistance, the diameter, the second distance, the second length, and the dynamic wind attack angle into a preset second calculation formula to obtain the resistance torque;

[0028] Wherein, the preset second calculation formula is:

[0029]

[0030] In the formula, F D2 is the resistance, D is the diameter, L is the second length of the second partition plate, θ is the dynamic wind attack angle, l is the second distance, M D2 is the resisting torque.

[0031] In one embodiment of the present application, based on the above solution, the wind-induced moment parameter is obtained by the following formula:

[0032] M D =M D1 -M D2

[0033] Where M Dis the wind-induced moment parameter, M D1 is the thrust torque, M D2 is the resisting torque.

[0034] In one embodiment of the present application, based on the above solution, the step of obtaining the friction torque parameter to which the vortex vibration suppression system is subjected when rotating around the circular column structure includes:

[0035] Obtaining the material density of the partition plate device, the number of the partition plates, the overall size parameters of the partition plates, the mass parameters of the pulley device, the dynamic friction coefficient of the pulley device, the diameter of the circular column structure, and the distance between the partition plate device and the outer surface of the circular column structure;

[0036] Inputting the material density, the quantity, the overall size parameter, the mass parameter, the dynamic friction coefficient, the distance, the diameter and the gravitational acceleration into a preset third calculation formula to obtain the friction torque parameter;

[0037] Wherein, the preset third calculation formula is:

[0038]

[0039] Where n1 is the number of partitions, A, B, δ are the overall size parameters, ρ 材 is the material density; m1 and m2 are the mass parameters, g is the gravitational acceleration, μ is the dynamic friction coefficient, D is the diameter, l is the distance, M f is the friction torque parameter.

[0040] In one embodiment of the present application, based on the above solution, the adjusting of the aerodynamic measure design parameters of the vortex vibration suppression system includes:

[0041] One or more adjustment methods are selected as target adjustment methods from the five adjustment methods of adjusting the number of the partition plates, adjusting the angles between the partition plates, adjusting the overall size parameters of the partition plates, adjusting the hole parameters of the partition plates, and adjusting the number of the pulleys;

[0042] The aerodynamic measure design parameters of the vortex vibration suppression system are adjusted according to the target adjustment method.

[0043] According to one aspect of an embodiment of the present application, a computer-readable storage medium is provided, on which a computer program is stored. The computer program includes executable instructions. When the executable instructions are executed by a processor, the method described in the above embodiment is implemented.

[0044] According to one aspect of an embodiment of the present application, an electronic device is provided, comprising: one or more processors; and a memory for storing executable instructions of the processors, wherein when the executable instructions are executed by the one or more processors, the one or more processors implement the methods described in the above embodiments.

[0045] The beneficial effect of the present application is that the present application applies a vortex vibration suppression system to the outer surface of a circular column structure, and the vortex vibration suppression system can rotate around the circular column structure under the action of a target incoming wind. By designing or adjusting the aerodynamic design parameters of the vortex vibration suppression system, the vortex vibration effect of the circular column structure caused by the target incoming wind can be reduced, thereby improving the safety of the circular column structure.

[0046] Furthermore, when the wind-induced torque parameter is greater than the friction torque parameter, it is determined whether the wind attack angle formed by the vortex-oscillation suppression system and the direction of the target incoming wind at the wake of the target incoming wind is less than a preset wind attack angle. If the wind attack angle is greater than or equal to the preset wind attack angle, it means that the aerodynamic measure design parameters at this time do not meet the requirements of the wind attack angle and cannot effectively reduce the vortex-oscillation effect caused by the target incoming wind. At this time, the aerodynamic measure design parameters can be adjusted to make the wind attack angle less than the preset wind attack angle to meet the requirements of the wind attack angle.

[0047] Furthermore, merely meeting the requirements for the wind attack angle is not sufficient to reduce the vortex-oscillation effect. Therefore, on the basis of meeting the requirements for the wind attack angle, it is necessary to obtain the first vortex-oscillation parameter to which the circular column structure is subjected after the vortex-oscillation suppression system is applied, and compare it with the second vortex-oscillation parameter to which the circular column structure is subjected when the vortex-oscillation suppression system is not applied, so as to determine whether the vortex-oscillation suppression system applied in the present application can effectively reduce the vortex-oscillation effect. If not, then readjust the aerodynamic measure design parameters of the vortex-oscillation suppression system until the first vortex-oscillation parameter after the vortex-oscillation suppression system is applied is significantly lower than the second vortex-oscillation parameter when the vortex-oscillation suppression system is not applied, thereby reducing the vortex-oscillation effect caused by the target incoming wind, or directly suppressing the occurrence of the vortex-oscillation effect.

[0048] Therefore, the present application verifies the design parameters of the aerodynamic measures, and when the set requirements are not met, continuously adjusts the design parameters of the aerodynamic measures to enable the vortex-oscillation suppression system to rotate to the wake of the target incoming wind under the action of the target incoming wind, thereby effectively reducing the vortex-oscillation effect of the circular column structure or directly suppressing the occurrence of the vortex-oscillation effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0049] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following is a brief description of the drawings required for use in the description of the embodiments. Obviously, the drawings described are only part of the embodiments of the present application, not all of the embodiments, and those skilled in the art can also obtain other design solutions and drawings based on these drawings without creative work.

[0050] Figure 1 It is a three-dimensional schematic diagram showing that a vortex vibration suppression system is equipped on the outer surface of a circular column structure according to an embodiment of the present application;

[0051] Figure 2 It is a front view of a vortex vibration suppression system according to an embodiment of the present application;

[0052] Figure 3 It is a left view of a vortex vibration suppression system according to an embodiment of the present application;

[0053] Figure 4 is a top view of a vortex vibration suppression system according to an embodiment of the present application;

[0054] Figure 5 It is a partial enlarged view of a vortex vibration suppression system according to an embodiment of the present application;

[0055] Figure 6 is a three-dimensional schematic diagram of an upper pulley block according to an embodiment of the present application;

[0056] Figure 7 It is a three-dimensional schematic diagram of a lower pulley assembly according to an embodiment of the present application;

[0057] Figure 8 It is a flow chart of a vortex vibration suppression method based on a circular column structure according to an embodiment of the present application;

[0058] Fig. 9 is a schematic diagram of a wind attack angle according to an embodiment of the present application;

[0059] Fig.10 is a specific flow chart of a vortex vibration suppression method based on a circular column structure according to an embodiment of the present application;

[0060] Fig.11 is a schematic diagram of a partition plate with a circular opening according to an embodiment of the present application;

[0061] Fig.12 is a schematic diagram of a partition plate with square openings according to an embodiment of the present application;

[0062] Fig.13 It is a schematic diagram showing that the partition plate rotates to the tail flow of the target incoming wind under the action of the target incoming wind and finally reaches a balanced state according to an embodiment of the present application;

[0063] Fig.14 is the relationship diagram between wind-induced moment parameters and friction moment parameters at different wind attack angles, different wind speeds when the characteristic diameter of the partition plate is D0 = 0.9 m;

[0064] Fig.15 is the relationship diagram between wind-induced moment parameters and friction moment parameters at different wind attack angles, different wind speeds when the characteristic diameter of the partition plate is D0 = 1.5 m;

[0065] Fig.16 It is a schematic diagram of the system structure of an electronic device according to an embodiment of the present application.

[0066] Reference numerals

[0067] The upper annular track 110 , the lower annular track 111 , the upper pulley block 120 , the main pulley 121 , the transverse auxiliary wheel 122 , the middle connecting block 130 , the lower pulley block 140 , the transverse partition 150 , the bolt connecting plate 151 , the vertical connecting shaft 160 , the porous plate type partition plate 210 , and the opening 211 . DETAILED DESCRIPTION

[0068] Example embodiments are now described more fully in conjunction with reference to the accompanying drawings. However, example embodiments can be implemented in a variety of forms and should not be construed as limited to the examples set forth herein; rather, these embodiments are provided so that this application will be more comprehensive and complete and fully convey the concept of the example embodiments to those skilled in the art.

[0069] In addition, described feature, structure or characteristic can be combined in one or more embodiments in any suitable manner. In the following description, many specific details are provided so as to provide a full understanding of the embodiments of the present application. However, it will be appreciated by those skilled in the art that the technical scheme of the present application can be put into practice without one or more of the specific details, or other methods, components, devices, steps, etc. can be adopted. In other cases, known methods, devices, realizations or operations are not shown or described in detail to avoid blurring the various aspects of the present application.

[0070] The block diagrams shown in the accompanying drawings are only functional entities and do not necessarily correspond to physically independent entities. These functional entities can be implemented in software form, or in one or more hardware modules or integrated circuits, or in different networks and / or processor devices and / or micro-control node devices.

[0071] The flowcharts shown in the accompanying drawings are only exemplary and do not necessarily include all the contents and operations / steps, nor must they be executed in the order described. For example, some operations / steps can be decomposed, and some operations / steps can be combined or partially combined, so the actual execution order may change according to actual conditions.

[0072] It should be noted that the "multiple" mentioned in this article refers to two or more. "And / or" describes the association relationship of the associated objects, indicating that there can be three relationships. For example, A and / or B can mean: A exists alone, A and B exist at the same time, and B exists alone. The character " / " generally indicates that the associated objects before and after are in an "or" relationship.

[0073] The vortex vibration suppression system proposed in the embodiment of the present application is described in detail below:

[0074] like Figure 1 As shown, Figure 1 The vortex vibration suppression system of the embodiment of the present application is equipped on the outer surface of the circular column (tower) structure. The vortex vibration suppression system includes a partition plate device, a pulley device and an annular track device surrounding the circular column structure. The partition plate device of the embodiment of the present application can specifically include two partition plates. Of course, the number of partition plates is two only an exemplary method of the embodiment of the present application. In other embodiments, the number of partition plates can also be set to 3, 4 or any other number. The number of partition plates is not limited here.

[0075] Similarly, the pulley device includes a plurality of pulleys, and the present application does not limit the number of pulleys. Figures 1 to 7 As shown, the annular track device of the embodiment of the present application includes: Figures 1 to 7 As shown in any of the figures, the upper annular track 110 and the lower annular track 111, the pulley device of the embodiment of the present application includes: Figures 1 to 7 The partition plate device of the present application embodiment includes two upper pulley blocks 120, four vertical main pulleys 121, four horizontal auxiliary wheels 122, and two lower pulley blocks 140 as shown in any of the figures. Figures 1 to 7 Two porous plate type separators 210 shown in any of the accompanying drawings.

[0076] Furthermore, the vortex vibration suppression system not only includes the partition plate device, the pulley device and the annular track device surrounding the circular column structure as described above, but also includes Figures 1 to 7 Any of the figures shown in the figure includes two middle connecting blocks 130, three transverse partitions 150, six bolt connecting plates 151, two vertical connecting shafts 160 and multiple openings 211 of the partition plates.

[0077] The following is an exemplary description of the installation method of the vortex vibration suppression system and the specific size parameters of each component (i.e., the design parameters of the aerodynamic measures described in the embodiment of the present application):

[0078] Specifically, the upper annular track 110 and the lower annular track 111 are respectively installed on the upper and lower sides of the outer surface of the tower structure (circular column structure), with a spacing of 6000mm between the upper and lower sides. The outer diameter of the annular track device is 3400m, the inner diameter is 3000mm, the edge height of the annular track device is 80mm, and the edge thickness is 10mm.

[0079] Furthermore, two upper pulley blocks 120 are installed on the upper annular track 110 , and the upper pulley block 120 and the lower pulley block 140 are each equipped with a vertical main pulley 121 and a horizontal auxiliary wheel 122 .

[0080] Further, the two upper pulley blocks 120, the two lower pulley blocks 140, the two middle connecting blocks 130 and the back side of each porous plate type partition plate 210 are connected with a bolt connection plate 151. The bolt connection plate 151 is connected to the porous plate type partition plate 210 by bolts.

[0081] Furthermore, the two upper pulley blocks 120 , the two lower pulley blocks 140 , the two middle connecting blocks 130 and the bolt connecting plates 151 at the back thereof are connected on the inner side through the three transverse partitions 150 .

[0082] The upper pulley block 120 of the present application is a rectangular shell structure equipped with pulleys, the length of the upper surface is 510mm, the width is 300mm, the length of the lower surface is 445mm, the width is 300mm, the overall height is 310mm, and the thickness is 10mm; the diameter of the vertical main pulley 121 is 150mm.

[0083] The lower pulley assembly 140 is a rectangular shell structure equipped with a pulley, the length of the upper surface of which is 510 mm, the width is 300 mm, the length of the lower surface is 460 mm, the width is 300 mm, the overall height is 310 mm, and the thickness is 10 mm.

[0084] The diameter of the transverse auxiliary wheel 122 is 80mm, the length of the bolt connecting plate 151 is 700mm, the height is 310mm, and the surface is provided with bolt holes with a diameter of 10mm; the porous plate partition plate 210 is a rectangular aluminum plate with a height of 7000mm, a width of 1500mm, and a thickness of 2mm, and has built-in ventilation holes (openings) 211 with a diameter of 100mm. The number of ventilation holes (openings) can be adjusted arbitrarily according to the porosity of 10% to 30%; the transverse partition plate 150 is an arc-shaped plate with an inner diameter of 3900mm, an outer diameter of 5200mm, and a thickness of 10mm; the vertical connecting shaft 160 is a cylinder with a height of 6400mm and a diameter of 100mm.

[0085] It should be noted that the above installation method of the vortex vibration suppression system and the specific values ​​of the size parameters of each component are only for illustrative purposes. In other embodiments, the installation method may be changed, and the number of components and the specific parameters of each component may also be adjusted. In other words, the design parameters of the aerodynamic measures described in the embodiments of the present application can be adjusted arbitrarily as needed and are not limited here.

[0086] The implementation details of the technical solution of the embodiment of the present application are described in detail below:

[0087] According to one aspect of an embodiment of the present application, a vortex vibration suppression method based on a circular column structure is provided, which is applied to a vortex vibration suppression system. The vortex vibration suppression system can rotate around the circular column structure under the action of a target incoming wind. Figure 8 This is a flow chart of a vortex vibration suppression method based on a circular column structure according to an embodiment of the present application. The method includes at least steps S1 to S6, which are described in detail as follows:

[0088] In step S1, wind-induced moment parameters to which the vortex-oscillation suppression system is subjected under the action of the target incoming wind are obtained, wherein the wind-induced moment parameters are used to make the vortex-oscillation suppression system rotate around the circular column structure.

[0089] Specifically, the wind speed of the target incoming wind can be set as needed. In the vortex vibration suppression method based on the circular column structure proposed in the present application, the incoming wind speed of the target incoming wind can be set to the minimum vortex vibration wind speed. The minimum vortex vibration wind speed is used to characterize the minimum wind speed corresponding to the vortex vibration effect of the circular column structure, that is, the vortex vibration effect can occur at the minimum vortex vibration wind speed. If the incoming wind speed of the target incoming wind is lower than the minimum vortex vibration wind speed, then the target incoming wind cannot cause the circular column structure to produce a vortex vibration effect. Of course, the incoming wind speed of the target incoming wind can also be set to other numerical wind speeds, not only limited to the minimum wind speed corresponding to the vortex vibration effect of the circular column structure, but also higher than the minimum vortex vibration wind speed. Then, the embodiment of the present application sets the incoming wind speed of the target incoming wind to the minimum vortex vibration wind speed first, so as to explore various situations that may occur in the circular column structure and the vortex vibration suppression system under the minimum vortex vibration wind speed.

[0090] In one embodiment of the present application, the vortex vibration suppression system includes a partition plate device, a pulley device and an annular track device surrounding the circular column structure, the pulley device slides in the annular track device and is connected to the partition plate device; under the action of the target incoming wind, the pulley device drives the partition plate device to rotate around the circular column structure; the aerodynamic measure design parameters include the number of partition plates in the partition plate device, the angles between each of the partition plates, the overall size parameters of each of the partition plates, the opening parameters of each of the partition plates and the number of pulleys in the pulley device.

[0091] Specifically, the specific component composition and installation method of the vortex vibration suppression system of the present application, and the size parameters of each component can be collectively referred to as aerodynamic measure design parameters; the specific aerodynamic measure design parameters have been combined in the above description. Figures 1 to 7 A detailed exemplary description has been given and will not be repeated here.

[0092] In one embodiment of the present application, the partition plate device includes a first partition plate and a second partition plate, and the step of obtaining the wind-induced moment parameter to which the vortex vibration suppression system is subjected under the action of the target incoming wind includes:

[0093] Obtaining the driving torque generated by the first partition plate under the action of the target incoming wind;

[0094] Obtaining the drag torque generated by the second partition plate under the action of the target incoming wind flow;

[0095] The wind-induced torque parameter is determined according to the propulsive torque and the resistive torque.

[0096] Specifically, the first partition plate and the second partition plate are not limited to Figures 1 to 7 Which partition plate is it? Here, the embodiment of the present application adopts functional definition of the first partition plate and the second partition plate. The first partition plate is used to characterize the partition plate that can generate thrust for the rotation of the vortex vibration suppression system under the action of the target incoming wind, and the second partition plate is used to characterize the partition plate that hinders the rotation of the vortex vibration suppression system and generates resistance under the action of the target incoming wind. Therefore, when the target incoming wind and the wind attack angle of the vortex vibration suppression system are different, the two partition plates of the present application may have the situation that the first partition plate and the second partition plate are interchangeable. For example, a certain partition plate at present can generate thrust for the rotation of the vortex vibration suppression system under the action of the target incoming wind, and at this time, the partition plate is the first partition plate; when the wind attack angle changes to a certain angle, the partition plate changes from generating thrust to generating resistance, and at this time, the partition plate changes from the first partition plate to the second partition plate.

[0097] Furthermore, the wind attack angle formed by the vortex vibration suppression system and the direction of the target incoming wind can be as follows: Fig. 9 As shown in the figure, the angle formed by the direction of the target incoming wind and the central axis of the vortex vibration suppression system, that is, the central axis of the two partitions, is called the wind attack angle. It should be noted that the wind attack angle can change during the rotation process, so a dynamic wind attack angle is defined in combination with the formula later. The concept of wind attack angle is consistent with that of dynamic wind attack angle.

[0098] In one embodiment of the present application, obtaining the driving torque generated by the first partition plate under the action of the target incoming wind includes:

[0099] Obtaining the incoming wind speed of the target incoming wind, the characteristic diameter of the vortex vibration suppression system, the air density of the environment in which the circular column structure is located, the first length of the first partition plate, and the drag coefficient of the vortex vibration suppression system under the action of the target incoming wind;

[0100] determining the thrust exerted on the first partition plate by the target incoming wind according to the incoming wind speed, the characteristic diameter, the air density, the first length and the drag coefficient;

[0101] Acquire the diameter of the circular column structure, the first distance between the first partition plate and the outer surface of the circular column structure, and the dynamic wind attack angle formed by the direction of the target incoming wind and the central axis of the vortex vibration suppression system;

[0102] Inputting the thrust, the diameter, the first distance, the first length, and the dynamic wind attack angle into a preset first calculation formula to obtain the propulsion torque;

[0103] Wherein, the preset first calculation formula is:

[0104]

[0105] In the formula, F D1 is the thrust, D is the diameter, L is the first length of the first partition plate, θ is the dynamic wind attack angle, l is the first distance, M D1 is the thrust torque.

[0106] Specifically, the thrust F D1 It can be obtained by the following formula:

[0107]

[0108] In the formula, C D is the drag coefficient, ρ is the air density. U is the incoming wind speed of the target incoming wind, D0 is the characteristic diameter of the mechanism system (vortex vibration suppression system), and L is the first length of the first partition plate. It should be noted that the dynamic wind attack angle may change as the vortex vibration suppression system rotates.

[0109] The step of obtaining the drag torque generated by the second partition plate under the action of the target incoming wind flow comprises:

[0110] Obtaining a second length of the second partition plate and a second distance between the second partition plate and the outer surface of the circular column structure, and determining the resistance of the second partition plate under the action of the target incoming wind according to the incoming wind speed, the characteristic diameter, the air density, the second length and the drag coefficient;

[0111] Input the resistance, the diameter, the second distance, the second length, and the dynamic wind attack angle into a preset second calculation formula to obtain the resistance torque;

[0112] Wherein, the preset second calculation formula is:

[0113]

[0114] In the formula, F D2 is the resistance, D is the diameter, L is the second length of the second partition plate, θ is the dynamic wind attack angle, l is the second distance, M D2 is the resisting torque.

[0115] Specifically, the resistance F D2 It can be obtained by the following formula:

[0116]

[0117] In the formula, C D is the drag coefficient, ρ is the air density. U is the incoming wind speed of the target incoming wind, D0 is the characteristic diameter of the mechanism system (vortex vibration suppression system), and L is the second length of the second partition plate. It should be noted that the dynamic wind attack angle may change as the vortex vibration suppression system rotates.

[0118] In one embodiment of the application, the wind-induced moment parameter is obtained by the following formula:

[0119] M D =M D1 -M D2

[0120] Where M D is the wind-induced moment parameter, M D1 is the thrust torque, M D2 is the resisting torque.

[0121] Specifically, the calculation of wind-induced moment parameters can be detailed by the following formula:

[0122]

[0123] In step S2, the friction torque parameters to which the vortex vibration suppression system is subjected when rotating around the circular column structure are obtained.

[0124] In one embodiment of the present application, the step of obtaining the friction torque parameter to which the vortex vibration suppression system is subjected when rotating around the circular column structure includes:

[0125] Obtaining the material density of the partition plate device, the number of the partition plates, the overall size parameters of the partition plates, the mass parameters of the pulley device, the dynamic friction coefficient of the pulley device, the diameter of the circular column structure, and the distance between the partition plate device and the outer surface of the circular column structure;

[0126] Inputting the material density, the quantity, the overall size parameter, the mass parameter, the dynamic friction coefficient, the distance, the diameter and the gravitational acceleration into a preset third calculation formula to obtain the friction torque parameter;

[0127] Wherein, the preset third calculation formula is:

[0128]

[0129] Where n1 is the number of partitions, A, B, δ are the overall size parameters, ρ 材 is the material density, m1 and m2 are the mass parameters, g is the gravitational acceleration, μ is the dynamic friction coefficient, D is the diameter, and l is the distance.

[0130] Specifically, ρ 材 is the material density of the partition plate. Since the material of the partition plate is aluminum as exemplarily mentioned above, then ρ 材 It can be specifically the material density of aluminum, expressed as ρ 铝 Then the third calculation formula can be expressed as ρ 铝 The changes are reflected as follows:

[0131]

[0132] In one embodiment of the present application, the adjusting of the aerodynamic measure design parameters of the vortex vibration suppression system includes:

[0133] Any one or more adjustment methods are selected as target adjustment methods from the five adjustment methods of adjusting the number of the partition plates, adjusting the angle between the partition plates, adjusting the overall size parameters of the partition plates, adjusting the opening parameters of the partition plates, and adjusting the number of the pulleys;

[0134] Adjust the design parameters of the aerodynamic measures of the vortex-induced vibration suppression system according to the described target adjustment method.

[0135] Specifically, there can be various adjustment methods. Although only five adjustment methods are reflected in the embodiments of the present application, including adjusting the number of the partition plates, adjusting the included angle between each of the partition plates, adjusting the overall dimension parameters of each of the partition plates, adjusting the opening parameters of each of the partition plates, and adjusting the number of the pulleys, these five adjustment methods are only for illustrative purposes. In other embodiments, there may be other adjustment methods, which are not limited herein.

[0136] In step S3, determine whether the wind-induced torque parameter is greater than the frictional torque parameter. If not, adjust the design parameters of the aerodynamic measures of the vortex-induced vibration suppression system until the wind-induced torque parameter is greater than the frictional torque parameter.

[0137] Specifically, it is necessary to ensure that the wind-induced torque parameter is greater than the frictional torque parameter so that the partition plates can rotate around the tower barrel (circular column structure) through the pulley device under the action of the target oncoming wind in the vortex-induced vibration suppression system.

[0138] In step S4, when the wind-induced torque parameter is greater than the frictional torque parameter, determine whether the wind attack angle formed by the vortex-induced vibration suppression system and the direction of the target oncoming wind at the wake of the target oncoming wind is less than the preset wind attack angle. If not, adjust the design parameters of the aerodynamic measures of the vortex-induced vibration suppression system until the wind attack angle is less than the preset wind attack angle.

[0139] Specifically, the wind attack angle needs to be less than the preset wind attack angle to reflect the suppression effect after applying the vortex-induced vibration suppression system.

[0140] In step S5, when the wind attack angle is less than the preset wind attack angle, obtain the first vortex-induced vibration parameter of the circular column structure after applying the vortex-induced vibration suppression system and the second vortex-induced vibration parameter of the circular column structure when the vortex-induced vibration suppression system is not applied.

[0141] Specifically, conduct a wind tunnel test on the above usage plan to verify whether vibration can be effectively suppressed. Measure the vortex-induced vibration interval I1 and the vortex-induced vibration amplitude A1 of the tower barrel (circular column structure) after applying the aerodynamic measures (that is, applying the vortex-induced vibration suppression system described in the present application) (i.e., the first vortex-induced vibration parameter described in the present application). And test the vortex-induced vibration interval I and the vortex-induced vibration amplitude A of the tower barrel when the aerodynamic measures are not applied (that is, applying the vortex-induced vibration suppression system described in the present application) (i.e., the second vortex-induced vibration parameter described in the present application). If both I1 < I and A1 < A are satisfied, the plan is applicable; otherwise, the plan needs to be adjusted. Adjust the control effect of the aerodynamic measures by changing the included angle between the partition plates and the shape of the partition plates.

[0142] In step S6, if the first vortex-oscillation parameter is greater than or equal to the second vortex-oscillation parameter, the aerodynamic measure design parameters of the vortex-oscillation suppression system are adjusted until the first vortex-oscillation parameter is less than the second vortex-oscillation parameter.

[0143] Specifically, the overall flow chart can be as follows: Fig.10 As shown in the figure, through continuous experiments, we finally found the appropriate aerodynamic design parameters to suppress the vortex vibration effect caused by the target incoming wind. Fig.10 The target wind attack angle shown is the preset wind attack angle mentioned in the present application. The specific value of the preset wind attack angle can be set as needed.

[0144] The following are some extensible example methods for adjusting the design parameters of the pneumatic measures in the embodiments of the present application:

[0145] Furthermore, the circular track of the present application has the functions of adjustable diameter, adjustable inclination angle and replaceable track, which can make the circular track suitable for tower structures (circular column structures) of different diameters and pulley devices of different specifications. The pulley device is used to bear the weight of the mechanical device part of the entire vortex vibration suppression system and the partition plate, and the size and bearing capacity specifications of the pulley device can be arbitrarily replaced.

[0146] Furthermore, the transverse partition is a fan-shaped structure with the same center as the circular column structure, connecting the pulley devices and bolt connection plates on the left and right sides. The transverse partition is retractable and can support the partition plate laterally and adjust the angle between the partition plates. The vertical connecting shaft can be used to connect the upper pulley block, the lower pulley block and the middle connecting block. The bolt connection plate can be used to connect the upper pulley block, the lower pulley block and the partition plate. The distance between the outer surface of the circular column structure and the partition plate can be adjusted by changing the connection position of the bolt connection plate and the partition plate.

[0147] The porous plate partition is made of light and high-strength material. The partition is replaceable and the opening parameters of the partition are adjustable, including the opening size, opening shape and opening distribution. Fig.11 and Fig.12 As shown, Fig.11 and Fig.12 There are two partition plates with different opening sizes, opening shapes and opening distribution methods. Due to the differences in opening sizes, opening shapes and opening distribution methods, the ventilation methods for the target incoming air flow are also different, and the vortex vibration suppression effects produced thereby are also different.

[0148] It should be noted that some specific parameters of the present application, such as the target incoming wind speed, the diameter of the circular column structure, the distance between the partition plate and the outer surface of the circular column structure, etc., can be detected by some specific sensors and will not be explained here.

[0149] The following is an exemplary description of the specific application implementation of the embodiments of the present application:

[0150] The wind force F on a single partition under the action of wind force D for:

[0151]

[0152] Among them, the wind-induced drag coefficient C of the entire vortex vibration suppression system under this condition is obtained by CFD modeling of the existing device. D is 2.3; ρ is the air density, ρ=1.29kg / m 3 ; U is the incoming wind speed. Since the wind speed at which the initial vortex vibration of the tower occurs is about 3m / s (which can be obtained from experimental analysis or empirical values), U=4m / s and U=5m / s are taken for calculation respectively; D0 is the characteristic width of the partition plate, and D0=1.5m is taken at this time; L is the length of the partition plate, and L=7m is taken at this time.

[0153] The vortex vibration suppression system is composed of two partitions, the angle between the two partitions is 90°. Under the action of the target wind flow, the partition will rotate to the tail of the target wind flow and finally reach a balanced state. Fig.13 This application introduces the definition of wind attack angle (dynamic wind attack angle) θ, that is, when the two partitions are symmetrically located at the wake of the target incoming wind, that is, the central axis of the two partitions is consistent with the direction of the target incoming wind at the wake, the wind attack angle θ = 0, and the vortex vibration suppression system is in a balanced state as a whole, and the wind-induced torque M it is subjected to D =0. It can be seen that within a certain range, the larger the wind attack angle θ is, the greater the wind-induced moment M D The larger the wind-induced moment parameter M of the vortex vibration suppression system as a whole D for:

[0154]

[0155] Among them, F D1 and F D2 are the force on the first partition plate that drives the entire vortex vibration suppression system to rotate under the action of the wind-induced moment parameter and the force on the second partition plate that prevents the vortex vibration suppression system from rotating; M D1 and M D2 In F D1 and F D2 Under the action of vortex vibration suppression system, the torque of wind turbine tower (circular column structure); D is the diameter of wind turbine tower (circular column structure), in this case, D=3m; L is the length of the first partition plate or the second partition plate (the length of the first partition plate and the second partition plate is the same in this embodiment), in this case, L=7m; θ is the wind attack angle. It is calculated that the change diagram of wind-induced moment parameters under different wind attack angles can be shown as follows: Fig.14 shown.

[0156] When the partition plate rotates to the incoming flow wake under the action of the wind-induced moment parameter, the friction resistance f of the entire vortex vibration suppression system is:

[0157] f=[n1×(1-P)×A×B×δ×ρ 铝 +m1+m2]×g×μ

[0158] Where n1 is the number of partition plates, in this case n1=2; A, B, δ are the length, width and thickness of the partition plates, A=7m, B=0.9m, δ=2mm; P is the porosity of the partition plates, P=20%; ρ 铝 is the density of aluminum, i.e. the material density of the partition plate, ρ 铝 =2700kg / m 3 ; m1+m2 is the total mass of the pulley device, m1=32kg, m2=68kg; g is the acceleration due to gravity, g=9.8m / s 2 ; μ is the dynamic friction coefficient of the pulley device, μ=0.02.

[0159] The friction torque parameter M of the entire vortex vibration suppression system around the center of the circular column structure is f for:

[0160]

[0161] Where D is the diameter of the circular column structure, in this case D = 3m; L is the length of the partition plate, in this case L = 7m; f is the resistance of the entire system on the circular track. The friction resistance parameters of the vibration suppression measures are calculated and shown in Fig.14 .

[0162] because Fig.14 It can be seen that when the wind speed is U = 4m / s and U = 5m / s, the wind-induced moment parameter M of the vortex vibration suppression system as a whole is D The value of the relative wind angle of attack (dynamic wind angle of attack) varies. Take the wind-induced moment parameter M D Greater than the friction torque parameter M f Working conditions: It can be seen that when the wind speed U=4m / s, the wind attack angle θ needs to be greater than 10°; when the wind speed U=5m / s, the wind attack angle θ needs to be greater than 5°. If the wind attack angle meets the requirements, the solution is used, otherwise it needs to be redesigned, that is, the aerodynamic design parameters of the vortex vibration suppression system are adjusted.

[0163] Next, after obtaining the above-mentioned usage plan through calculation, fabricate a model of the vortex-induced vibration suppression system in this plan and conduct a wind tunnel test for re-verification. If the model cannot rotate effectively, the plan can be adjusted (i.e., adjust the design parameters of the aerodynamic measures of the vortex-induced vibration suppression system). The plan adjustment is mainly achieved by changing the size of the partition plate or the specifications of the sliding device. It should be noted that Fig.14 and Fig.15 the moment represented by the ordinate of is the wind force moment parameter.

[0164] Changing the size of the partition plate can increase the wind force moment parameter M received by the overall vortex-induced vibration suppression system D . For example, increase the width of the partition plate from D0 = 0.9m to D0 = 1.5m. As calculated in Fig.15 . It can be clearly found that when the wind speed U = 4m / s, the wind attack angle θ needs to be greater than 5°; when the wind speed U = 5m / s, the wind attack angle θ needs to be greater than 3°. Thus, it can be seen that the required wind attack angle decreases significantly after adjusting the design parameters of the aerodynamic measures.

[0165] Next, test the control effect of the aerodynamic measures. Conduct a wind tunnel test on the above-mentioned usage plan to verify whether vibration can be effectively suppressed. Measure the vortex-induced vibration interval I1 and the vortex-induced vibration amplitude A1 (i.e., the first vortex-induced vibration parameter described in this application) of the tower barrel (circular column structure) after applying the aerodynamic measures (that is, applying the vortex-induced vibration suppression system described in this application). And test the vortex-induced vibration interval I and the vortex-induced vibration amplitude A (i.e., the second vortex-induced vibration parameter described in this application) of the tower barrel when no aerodynamic measures are applied (that is, applying the vortex-induced vibration suppression system described in this application). If both I1 < I and A1 < A are satisfied, this plan is applicable; otherwise, the plan needs to be adjusted. Adjust the control effect of the aerodynamic measures by changing the angle between the partition plates and the shape of the partition plates.

[0166] As another aspect, this application also provides a computer-readable storage medium, on which a program product capable of implementing the method provided above in this specification is stored. In some possible implementation manners, each aspect of this application can also be implemented in the form of a program product, which includes program code. When the program product runs on a terminal device, the program code is used to cause the terminal device to execute the steps according to various exemplary implementation manners of this application described in the "Embodiment Method" part above in this specification.

[0167] The program product for implementing the above method according to the embodiments of this application can adopt a portable compact disc read-only memory (CD-ROM) and include program code, and can run on a terminal device, such as a personal computer. However, the program product of this application is not limited to this. In this document, the readable storage medium can be any tangible medium that contains or stores a program, and this program can be used by or in combination with an instruction execution system, device, or device.

[0168] The program product may employ any combination of one or more readable media. The readable medium may be a readable signal medium or a readable storage medium. The readable storage medium may be, for example, but not limited to, an electrical, magnetic, optical, electromagnetic, infrared or semiconductor system, device or device, or any combination of the above. More specific examples of readable storage media (a non-exhaustive list) include: an electrical connection with one or more wires, a portable disk, a hard disk, a random access memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disk read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the above.

[0169] Computer readable signal media may include a data signal propagated in baseband as part of a carrier wave, wherein readable program code is carried. Such propagated data signals may take a variety of forms, including but not limited to electromagnetic signals, optical signals, or any suitable combination of the above. Readable signal media may also be any readable medium other than a readable storage medium, which may send, propagate, or transmit a program for use by or in conjunction with an instruction execution system, apparatus, or device.

[0170] The program code embodied on the readable medium may be transmitted using any appropriate medium, including but not limited to wireless, wired, optical cable, RF, etc., or any suitable combination of the foregoing.

[0171] Program code for performing the operations of the present application may be written in any combination of one or more programming languages, including object-oriented programming languages ​​such as Java, C++, etc., and conventional procedural programming languages ​​such as "C" or similar programming languages. The program code may be executed entirely on the user computing device, partially on the user device, as a separate software package, partially on the user computing device and partially on a remote computing device, or entirely on a remote computing device or server. In the case of a remote computing device, the remote computing device may be connected to the user computing device through any type of network, including a local area network (LAN) or a wide area network (WAN), or may be connected to an external computing device (e.g., using an Internet service provider to connect through the Internet).

[0172] As another aspect, the present application also provides an electronic device capable of implementing the above method.

[0173] Those skilled in the art will appreciate that various aspects of the present application may be implemented as a system, method or program product. Therefore, various aspects of the present application may be specifically implemented in the following forms, that is, a complete hardware implementation, a complete software implementation (including firmware, microcode, etc.), or a combination of hardware and software, which may be collectively referred to as "circuit", "module" or "system" herein.

[0174] Refer to the following Fig.16 The electronic device 400 according to this embodiment of the present application is described. Fig.16 The electronic device 400 shown is merely an example and should not bring any limitation to the functions and scope of use of the embodiments of the present application.

[0175] like Fig.16 As shown, the electronic device 400 is in the form of a general computing device. The components of the electronic device 400 may include but are not limited to: at least one processing unit 410, at least one storage unit 420, and a bus 430 connecting different system components (including the storage unit 420 and the processing unit 410).

[0176] The storage unit stores program codes, which can be executed by the processing unit 410, so that the processing unit 410 executes the steps described in the above “Example Method” section of this specification according to various exemplary implementations of the present application.

[0177] The storage unit 420 may include a readable medium in the form of a volatile storage unit, such as a random access memory unit (RAM) 421 and / or a cache memory unit 422 , and may further include a read-only memory unit (ROM) 423 .

[0178] The storage unit 420 may also include a program / utility 424 having a set (at least one) of program modules 425, such program modules 425 including but not limited to: an operating system, one or more application programs, other program modules, and program data, each of which or some combination may include an implementation of a network environment.

[0179] Bus 430 may represent one or more of several types of bus structures, including a memory unit bus or memory unit controller node, a peripheral bus, an accelerated graphics port, a processing unit, or a local bus using any of a variety of bus architectures.

[0180] The electronic device 400 may also communicate with one or more external devices 1200 (e.g., keyboards, pointing devices, Bluetooth devices, etc.), may also communicate with one or more devices that enable a user to interact with the electronic device 400, and / or communicate with any device that enables the electronic device 400 to communicate with one or more other computing devices (e.g., routers, modems, etc.). Such communication may be performed via an input / output (I / O) interface 450. In addition, the electronic device 400 may also communicate with one or more networks (e.g., local area networks (LANs), wide area networks (WANs), and / or public networks, such as the Internet) via a network adapter 460. As shown, the network adapter 460 communicates with other modules of the electronic device 400 via a bus 430. It should be understood that, although not shown in the figure, other hardware and / or software modules may be used in conjunction with the electronic device 400, including but not limited to: microcode, device drivers, redundant processing units, external disk drive arrays, RAID systems, tape drives, and data backup storage systems.

[0181] Through the description of the above implementation methods, it is easy for those skilled in the art to understand that the example implementation methods described here can be implemented by software or by combining software with necessary hardware. Therefore, the technical solution according to the implementation methods of the present application can be embodied in the form of a software product, which can be stored in a non-volatile storage medium (which can be a CD-ROM, a USB flash drive, a mobile hard disk, etc.) or on a network, and includes several instructions to enable a computing device (which can be a personal computer, a server, a terminal device or a network device, etc.) to execute the method according to the implementation methods of the present application.

[0182] In addition, the above-mentioned figures are only schematic illustrations of the processes included in the method according to the exemplary embodiment of the present application, and are not intended to be limiting. It is easy to understand that the processes shown in the above-mentioned figures do not indicate or limit the time sequence of these processes. In addition, it is also easy to understand that these processes can be performed synchronously or asynchronously in multiple modules.

[0183] It should be understood that the present application is not limited to the precise structures that have been described above and shown in the drawings, and that various modifications and changes may be performed without departing from the scope thereof. The scope of the present application is limited only by the appended claims.

Claims

1. A vortex vibration suppression method based on a circular column structure, characterized in that: Applied to a vortex vibration suppression system, the vortex vibration suppression system can rotate around a circular column structure under the action of a target incoming wind, and the method includes: Acquiring wind-induced moment parameters to which the vortex-oscillation suppression system is subjected under the action of the target incoming wind, wherein the wind-induced moment parameters are used to cause the vortex-oscillation suppression system to rotate around the circular column structure; Obtaining friction torque parameters to which the vortex vibration suppression system is subjected when rotating around the circular column structure; determining whether the wind-induced torque parameter is greater than the friction torque parameter, and if not, adjusting aerodynamic measure design parameters of the vortex vibration suppression system until the wind-induced torque parameter is greater than the friction torque parameter; In the case where the wind-induced torque parameter is greater than the friction torque parameter, determining whether a wind attack angle formed by the vortex vibration suppression system and the direction of the target incoming wind at the wake of the target incoming wind is less than a preset wind attack angle, and if not, adjusting aerodynamic measure design parameters of the vortex vibration suppression system until the wind attack angle is less than the preset wind attack angle; When the wind attack angle is less than the preset wind attack angle, obtaining a first vortex-vibration parameter to which the circular column structure is subjected after the vortex-vibration suppression system is applied and a second vortex-vibration parameter to which the circular column structure is subjected when the vortex-vibration suppression system is not applied; If the first vortex-oscillation parameter is greater than or equal to the second vortex-oscillation parameter, the aerodynamic measure design parameters of the vortex-oscillation suppression system are adjusted until the first vortex-oscillation parameter is less than the second vortex-oscillation parameter.

2. The vortex vibration suppression method based on the circular column structure according to claim 1 is characterized in that: The vortex vibration suppression system includes a partition plate device, a pulley device and an annular track device surrounding the circular column structure, the pulley device slides in the annular track device and is connected to the partition plate device; under the action of the target incoming wind, the pulley device drives the partition plate device to rotate around the circular column structure; the aerodynamic measure design parameters include the number of partition plates in the partition plate device, the angles between each of the partition plates, the overall size parameters of each of the partition plates, the opening parameters of each of the partition plates and the number of pulleys in the pulley device.

3. The vortex vibration suppression method based on the circular column structure according to claim 2 is characterized in that: The partition plate device includes a first partition plate and a second partition plate, and the step of obtaining the wind-induced moment parameter to which the vortex vibration suppression system is subjected under the action of the target incoming wind includes: Obtaining the driving torque generated by the first partition plate under the action of the target incoming wind; Obtaining the drag torque generated by the second partition plate under the action of the target incoming wind flow; The wind-induced torque parameter is determined according to the propulsive torque and the resistive torque.

4. The vortex vibration suppression method based on the circular column structure according to claim 3 is characterized in that: The step of obtaining the driving torque generated by the first partition plate under the action of the target incoming wind includes: Obtaining the incoming wind speed of the target incoming wind, the characteristic diameter of the vortex vibration suppression system, the air density of the environment in which the circular column structure is located, the first length of the first partition plate, and the drag coefficient of the vortex vibration suppression system under the action of the target incoming wind; determining the thrust exerted on the first partition plate by the target incoming wind according to the incoming wind speed, the characteristic diameter, the air density, the first length and the drag coefficient; Acquire the diameter of the circular column structure, the first distance between the first partition plate and the outer surface of the circular column structure, and the dynamic wind attack angle formed by the direction of the target incoming wind and the central axis of the vortex vibration suppression system; Inputting the thrust, the diameter, the first distance, the first length, and the dynamic wind attack angle into a preset first calculation formula to obtain the propulsion torque; Wherein, the preset first calculation formula is: In the formula, F D1 is the thrust, D is the diameter, L is the first length of the first partition plate, θ is the dynamic wind attack angle, l is the first distance, M D1 is the driving torque.

5. The vortex vibration suppression method based on the circular column structure according to claim 4 is characterized in that: The step of obtaining the drag torque generated by the second partition plate under the action of the target incoming wind flow comprises: Obtaining a second length of the second partition plate and a second distance between the second partition plate and the outer surface of the circular column structure, and determining the resistance of the second partition plate under the action of the target incoming wind according to the incoming wind speed, the characteristic diameter, the air density, the second length and the drag coefficient; Input the resistance, the diameter, the second distance, the second length, and the dynamic wind attack angle into a preset second calculation formula to obtain the resistance torque; Wherein, the preset second calculation formula is: In the formula, F D2 is the resistance, D is the diameter, L is the second length of the second partition plate, θ is the dynamic wind attack angle, l is the second distance, M D2 is the drag torque.

6. The vortex vibration suppression method based on a circular column structure according to claim 5 is characterized in that: The wind-induced moment parameter is obtained by the following formula: M D =M D1 -M D2 Where M D is the wind-induced moment parameter, M D1 is the thrust torque, M D2 is the resisting torque.

7. The vortex vibration suppression method based on a circular column structure according to claim 6 is characterized in that: The obtaining of the friction torque parameter to which the vortex vibration suppression system is subjected when rotating around the circular column structure comprises: Obtaining the material density of the partition plate device, the number of the partition plates, the overall size parameters of the partition plates, the mass parameters of the pulley device, the dynamic friction coefficient of the pulley device, the diameter of the circular column structure, and the distance between the partition plate device and the outer surface of the circular column structure; Inputting the material density, the quantity, the overall size parameter, the mass parameter, the dynamic friction coefficient, the distance, the diameter and the gravitational acceleration into a preset third calculation formula to obtain the friction torque parameter; Wherein, the preset third calculation formula is: Where n1 is the number of partitions, A, B, δ are the overall size parameters, ρ 材 is the material density; m1 and m2 are the mass parameters, g is the gravitational acceleration, μ is the dynamic friction coefficient, D is the diameter, l is the distance, M f is the friction torque parameter.

8. The vortex vibration suppression method based on a circular column structure according to claim 7 is characterized in that: The aerodynamic measure design parameters of the vortex vibration suppression system are adjusted, including: Any one or more adjustment methods are selected as target adjustment methods from the five adjustment methods of adjusting the number of the partition plates, adjusting the angle between the partition plates, adjusting the overall size parameters of the partition plates, adjusting the opening parameters of the partition plates, and adjusting the number of the pulleys; The aerodynamic measure design parameters of the vortex vibration suppression system are adjusted according to the target adjustment method.

9. A computer-readable storage medium, characterized in that: The computer-readable storage medium stores at least one program code, and the at least one program code is loaded and executed by a processor to implement the operations performed by the method according to any one of claims 1 to 8.

10. An electronic device, characterized in that: The electronic device includes one or more processors and one or more memories, wherein the one or more memories store at least one program code, and the at least one program code is loaded and executed by the one or more processors to implement the operations performed by the method according to any one of claims 1 to 8.

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