阅读说明：本技术 一种动惯性导向控制装置 (Moving inertia guiding control device ) 是由 杨艺 陈龙 刘昌宁 杨晓峰 沈钰杰 于 2020-04-26 设计创作，主要内容包括：本发明提供了一种动惯性导向控制装置,包括缸体、活塞和主螺旋管,所述活塞将缸体的内腔分为上腔和下腔,所述上腔与下腔之间连接主螺旋管；所述活塞包括活塞主体、质量块和螺旋槽；所述活塞主体内部设有内腔,所述内腔分别与上腔和下腔连通；所述质量块两端分别通过弹性装置安装在内腔内；所述活塞主体内部设有沿所述内腔均布的若干螺旋槽,一部分所述螺旋槽连通上腔与内腔,另一部分所述螺旋槽连通下腔与内腔；所述质量块根据加速度的变化选择性使若干所述螺旋槽与内腔连通或阻断。本发明实现了与两端点加速度方向的辨识和随动控制,使得基于加速度的半主动控制方法得以被动实现,无需依赖外端能量的输入,且装置一体化程度高,易于布置。(The invention provides a dynamic inertia guiding control device which comprises a cylinder body, a piston and a main spiral pipe, wherein the piston divides an inner cavity of the cylinder body into an upper cavity and a lower cavity, and the main spiral pipe is connected between the upper cavity and the lower cavity; the piston comprises a piston main body, a mass block and a spiral groove; an inner cavity is formed in the piston main body and is respectively communicated with the upper cavity and the lower cavity; two ends of the mass block are respectively installed in the inner cavity through elastic devices; a plurality of spiral grooves are uniformly distributed along the inner cavity in the piston main body, one part of the spiral grooves are communicated with the upper cavity and the inner cavity, and the other part of the spiral grooves are communicated with the lower cavity and the inner cavity; the mass block selectively enables the spiral grooves to be communicated with or blocked from the inner cavity according to the change of the acceleration. The invention realizes the identification and the follow-up control of the acceleration directions of two end points, so that the semi-active control method based on the acceleration can be realized passively without depending on the input of the energy of the outer end, and the device has high integration degree and is easy to arrange.)

1. The moving inertia guide control device is characterized by comprising a cylinder body (7), a piston (6) and a main spiral pipe (5), wherein the piston (6) divides an inner cavity of the cylinder body (7) into an upper cavity and a lower cavity, and the main spiral pipe (5) used for generating a first inertia force is connected between the upper cavity and the lower cavity; the piston (6) comprises a piston body, a mass block (20) and a spiral groove; an inner cavity is formed in the piston main body and is respectively communicated with the upper cavity and the lower cavity; two ends of the mass block (20) are respectively installed in the inner cavity through elastic devices, and the mass block (20) can move in the inner cavity along the acceleration direction; a plurality of spiral grooves are uniformly distributed along the inner cavity in the piston main body, one part of the spiral grooves are communicated with the upper cavity and the inner cavity, and the other part of the spiral grooves are communicated with the lower cavity and the inner cavity and are used for generating an inertia force different from or equal to the first inertia force; the mass block (20) selectively enables the spiral grooves to be communicated with or blocked from the inner cavity according to the change of the acceleration.

2. The dynamic inertia guiding control device according to claim 1, wherein a plurality of upper spiral grooves and a plurality of lower spiral grooves are uniformly distributed in the piston main body, the upper spiral grooves are communicated with the upper cavity and the inner cavity, and the lower spiral grooves are communicated with the lower cavity and the inner cavity; the upper spiral groove comprises a first upper spiral groove (14) and a second upper spiral groove (15), and a liquid outlet of the first upper spiral groove (14) and a liquid outlet of the second upper spiral groove (15) are respectively close to two ends of the mass block (20) in a balanced state; the lower spiral groove comprises a first lower spiral groove (24) and a second lower spiral groove (16), and a liquid inlet of the first lower spiral groove (24) and a liquid inlet of the second lower spiral groove (16) are respectively close to two ends of the mass block (20) in a balanced state; the mass block (20) moves in the inner cavity through the change of the acceleration and is used for selectively enabling the first upper spiral groove (14) and the first lower spiral groove (24) to be communicated with or blocked from the inner cavity or selectively enabling the second upper spiral groove (15) and the second lower spiral groove (16) to be communicated with or blocked from the inner cavity.

3. The dynamic inertia guiding control device according to claim 2, wherein the liquid outlet of the first upper spiral groove (14) and the liquid inlet of the first lower spiral groove (24) are located at the same horizontal position, and the first upper spiral groove (14) and the first lower spiral groove (24) are simultaneously communicated or blocked with the inner cavity under the action of acceleration through the mass block (20); the liquid outlet of the second upper spiral groove (15) and the liquid inlet of the second lower spiral groove (16) are positioned at the same horizontal position; the second upper spiral groove (15) and the second lower spiral groove (16) are simultaneously communicated or blocked with the inner cavity under the action of acceleration through the mass block (20).

4. The dynamic inertial guidance control device according to claim 3, characterized in that the distance between the liquid outlet of the first upper spiral groove (14) and the liquid outlet of the second upper spiral groove (15) or the distance between the liquid inlet of the first lower spiral groove (24) and the liquid inlet of the second lower spiral groove (16) is smaller than the length of the mass (20).

5. The dynamic inertia steering control device according to claim 4, wherein, in a balanced state, two ends of the mass block (20) block the liquid outlet of the first upper spiral groove (14), the liquid outlet of the second upper spiral groove (15), the liquid inlet of the first lower spiral groove (24) and the liquid inlet of the second lower spiral groove (16), respectively; when the mass block (20) moves downwards, the first upper spiral groove (14) and the first lower spiral groove (24) are simultaneously communicated with the inner cavity; when the mass block (20) moves upwards, the second upper spiral groove (15) and the second lower spiral groove (16) are simultaneously communicated with the inner cavity.

6. The dynamic inertial guidance control device according to claim 3, characterized in that the distance between the liquid outlet of the first upper spiral groove (14) and the liquid outlet of the second upper spiral groove (15) or the distance between the liquid inlet of the first lower spiral groove (24) and the liquid inlet of the second lower spiral groove (16) is greater than or equal to the length of the mass block (20).

7. The dynamic inertia guiding control device according to claim 6, wherein, in a balanced state, the liquid outlet of the first upper spiral groove (14), the liquid outlet of the second upper spiral groove (15), the liquid inlet of the first lower spiral groove (24) and the liquid inlet of the second lower spiral groove (16) are respectively communicated with the inner cavity; when the mass block (20) moves upwards, the first upper spiral groove (14) and the first lower spiral groove (24) are simultaneously blocked from the inner cavity; when the mass (20) moves downwards, the second upper spiral groove (15) and the second lower spiral groove (16) are simultaneously blocked from the inner cavity.

8. A dynamic inertial guidance control device according to any one of claims 1-7, characterized in that the main spiral tube (5) differs from at least one of the number of turns, diameter, pitch and radius of the spiral grooves for generating different inertial forces.

Technical Field

The invention relates to the field of motor vehicle shock absorbers, in particular to a dynamic inertia guiding control device.

Background

With the development of the transportation industry in China, the domestic passenger cars are developed towards intellectualization, high-speed, light weight and cleanness, and the requirement on vehicle energy conservation is higher and higher. With the consolidation of the vehicle suspension structure, the improvement of the comprehensive performance of the common passive suspension approaches the limit increasingly, and researchers turn the attention to the semi-active control suspension and the active control suspension gradually. However, both semi-active and active control suspensions require energy input beyond the suspension to achieve control, and active suspensions are more slowly developed due to high energy consumption.

In the development of intelligent vehicles, semi-active control suspension gradually becomes the mainstream of the current suspension development, and an energy recovery system is also used in the semi-active control suspension. However, the energy recovery system has limited recovery efficiency, is insufficient to provide sufficient energy for the suspension, and still depends on the input of external energy. This has the effect of increasing the cost of the vehicle, increasing the load on the suspension, and even negatively affecting the vibration isolation performance of the suspension.

In addition, current semi-active suspension control is mainly used for realizing regulation and control of element parameters, some semi-active control is realized by changing the characteristics of element materials, and some semi-active control realizes multi-stage regulation and control of the parameters by using electromagnetic valves, even on-off switch control. Although the control algorithm is simple, the corresponding controller and actuator are still required to be equipped, which not only makes the suspension structure become complicated and the production cost increase, but also makes the suspension structure reduce the stability of the suspension system due to the dependence on the electric system. If the input of the energy of the outer end is not needed, the control method of realizing the semi-active control by the electromagnetic valve switch is realized passively through mechanical elements, so that the performance of the suspension can be improved, the stability of the suspension can be further improved, the production cost is reduced, and the energy is saved.

Due to the attention on the inertia characteristics of the suspension, more and more moving inertia elements are designed, and the structural design and the control method of the suspension are further developed. Unlike dampers, which have two end-point forces related to the relative motion velocity of two end-points, and two end-point forces related to the relative acceleration of two end-points, the direction of acceleration is difficult to be directly identified by the motion direction of an object, so some methods using "on-off" as control are difficult to be applied to the moving inertia element by using passive methods.

Disclosure of Invention

Aiming at the defects in the prior art, the invention provides a dynamic inertia guiding control device, which realizes the identification and follow-up control of the acceleration directions of two end points after the dynamic inertia guiding piston and a liquid flow direction structure are designed, so that a semi-active control method based on the acceleration can be realized passively without depending on the input of external end energy, and the device has high integration degree and is easy to arrange.

The present invention achieves the above-described object by the following technical means.

A moving inertia guide control device comprises a cylinder body, a piston and a main spiral pipe, wherein the piston divides an inner cavity of the cylinder body into an upper cavity and a lower cavity, and the main spiral pipe used for generating first inertia force is connected between the upper cavity and the lower cavity; the piston comprises a piston main body, a mass block and a spiral groove; an inner cavity is formed in the piston main body and is respectively communicated with the upper cavity and the lower cavity; two ends of the mass block are respectively installed in the inner cavity through elastic devices, and the mass block can move in the inner cavity along the acceleration direction; a plurality of spiral grooves are uniformly distributed along the inner cavity in the piston main body, one part of the spiral grooves are communicated with the upper cavity and the inner cavity, and the other part of the spiral grooves are communicated with the lower cavity and the inner cavity and are used for generating an inertia force different from or equal to the first inertia force; the mass block selectively enables the spiral grooves to be communicated with or blocked from the inner cavity according to the change of the acceleration.

Furthermore, a plurality of upper spiral grooves and a plurality of lower spiral grooves are uniformly distributed in the piston main body, the upper spiral grooves are communicated with the upper cavity and the inner cavity, and the lower spiral grooves are communicated with the lower cavity and the inner cavity; the upper spiral groove comprises a first upper spiral groove and a second upper spiral groove, and a liquid outlet of the first upper spiral groove and a liquid outlet of the second upper spiral groove are respectively close to two ends of the mass block in a balanced state; the lower spiral groove comprises a first lower spiral groove and a second lower spiral groove, and a liquid inlet of the first lower spiral groove and a liquid inlet of the second lower spiral groove are respectively close to two ends of the mass block in a balanced state; the mass block moves in the inner cavity through the change of the acceleration and is used for selectively enabling the first upper spiral groove and the first lower spiral groove to be communicated with or blocked from the inner cavity or selectively enabling the second upper spiral groove and the second lower spiral groove to be communicated with or blocked from the inner cavity.

Furthermore, a liquid outlet of the first upper spiral groove and a liquid inlet of the first lower spiral groove are positioned at the same horizontal position, and the first upper spiral groove and the first lower spiral groove are simultaneously communicated or blocked with the inner cavity under the action of acceleration through the mass block; the liquid outlet of the second upper spiral groove and the liquid inlet of the second lower spiral groove are positioned at the same horizontal position; the second upper spiral groove and the second lower spiral groove are communicated or blocked with the inner cavity at the same time under the action of acceleration through the mass block.

Further, the distance between the liquid outlet of the first upper spiral groove and the liquid outlet of the second upper spiral groove or the distance between the liquid inlet of the first lower spiral groove and the liquid inlet of the second lower spiral groove is smaller than the length of the mass block.

Further, in a balanced state, two ends of the mass block respectively block a liquid outlet of the first upper spiral groove, a liquid outlet of the second upper spiral groove, a liquid inlet of the first lower spiral groove and a liquid inlet of the second lower spiral groove; when the mass block moves downwards, the first upper spiral groove and the first lower spiral groove are communicated with the inner cavity at the same time; when the mass block moves upwards, the second upper spiral groove and the second lower spiral groove are communicated with the inner cavity at the same time.

Further, the distance between the liquid outlet of the first upper spiral groove and the liquid outlet of the second upper spiral groove or the distance between the liquid inlet of the first lower spiral groove and the liquid inlet of the second lower spiral groove is greater than the length of the mass block.

Further, in a balanced state, a liquid outlet of the first upper spiral groove, a liquid outlet of the second upper spiral groove, a liquid inlet of the first lower spiral groove and a liquid inlet of the second lower spiral groove are respectively communicated with the inner cavity; when the mass block moves upwards, the first upper spiral groove and the first lower spiral groove are simultaneously blocked with the inner cavity; when the mass block moves downwards, the second upper spiral groove and the second lower spiral groove are simultaneously blocked from the inner cavity.

Furthermore, at least one of the spiral turns, the pipe diameter, the spiral pipe distance and the spiral radius parameters of the main spiral pipe and the spiral grooves is different, and the main spiral pipe and the spiral grooves are used for generating different inertia forces.

The invention has the beneficial effects that:

1. the dynamic inertia guiding control device provided by the invention has the advantages that the target of the direction and the magnitude of the acceleration parameter of the dynamic inertia element is expressed by the mechanical element, the passive realization of semi-active control is realized, the structural integration degree of the device is high, the device is easy to install, the element parameter of the dynamic inertia element can be rapidly switched along with the magnitude of the vibration input force, and the device is a parameter three-level adjustable device.

2. According to the dynamic inertia guiding control device, the dynamic inertia coefficient of the dynamic inertia guiding control device can be designed according to actual requirements, such as the number of the upper spiral groove, the lower spiral groove and the spiral pipe, the number of spiral turns, the size of the groove diameter, the thread pitch and the spiral radius, so as to realize the setting of the dynamic inertia coefficient.

3. The dynamic inertia guiding control device passively realizes different control methods by designing the position relations among the upper spiral groove, the lower spiral groove and the mass block, and can also realize reasonable state switching conditions by setting different upper spring stiffness, lower spring stiffness and mass block.

Drawings

Fig. 1 is a schematic structural diagram of a dynamic inertia guiding control device according to the present invention.

Fig. 2 is a schematic diagram of the arrangement of the spiral groove in the piston according to the invention.

Fig. 3 is a set of sectional views of the inside of the piston according to embodiment 1 of the present invention.

Fig. 4 is another set of sectional views of the interior of the piston according to embodiment 1 of the present invention.

Fig. 5 is a schematic diagram illustrating a positional relationship between the upper and lower spiral grooves and the mass in embodiment 1.

Fig. 6 is a set of cross-sectional views of the interior of the piston according to embodiment 2 of the present invention.

Fig. 7 is another set of sectional views of the interior of the piston according to embodiment 2 of the present invention.

Fig. 8 is a schematic diagram illustrating a positional relationship between the upper and lower spiral grooves and the mass in embodiment 2.

In the figure:

1-upper lifting lug; 2-a piston rod; 3-sealing ring; 4-a through hole; 5-a main spiral pipe; 6-a piston; 7-cylinder body; 8-an anti-collision block; 9-a lower lifting lug; 10-upper sealing cover; 11-flow-through holes; 12-upper fluid chamber; 13-a gasket; 14-a first upper helical groove; 15-a second upper helical groove; 16-a second lower helical flute; 17-lower sealing cap; 18-lower fluid chamber; 19-a lower spring; 20-a mass block; 21-upper spring; 22-a lower connecting rod; 23-an upper connecting rod; 24-first lower helical groove.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.

In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "axial," "radial," "vertical," "horizontal," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the present invention and for simplicity in description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting. Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.

In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

As shown in fig. 1, the moving inertia guiding control device according to the present invention includes a cylinder body 7, an upper lifting lug 1, a lower lifting lug 9, a piston 6 and a main spiral tube 5, wherein the upper lifting lug 1 is connected to the piston 6 through a piston rod 2, the piston 6 is disposed in the cylinder body 7, the piston 6 divides an inner cavity of the cylinder body 7 into an upper cavity and a lower cavity, the piston rod 2 and the cylinder body 7 are sealed by a sealing ring 3, the upper cavity and the lower cavity are both provided with through holes 4, the through holes 4 of the upper cavity and the lower cavity are connected by the main spiral tube 5, such that liquid in the upper cavity and the lower cavity can flow through the main spiral tube 5 to generate a first inertia. The bottom of the inner wall of the cylinder body 7 is provided with an anti-collision block 8, so that the piston rod 2 is prevented from colliding with the inner wall of the cylinder body 7.

The piston 6 is a core component of the moving inertia guiding control device, as shown in fig. 3 and 4, the piston 6 includes an upper sealing cover 10, a lower sealing cover 17, a mass block 20, a spiral groove and a piston main body, the upper sealing cover 10 and the lower sealing cover 17 are both provided with a circulation hole 11, an upper liquid cavity 12 and a lower liquid cavity 18 are respectively reserved between the upper sealing cover 10 and the lower sealing cover 17 as well as between the piston main body and the upper sealing cover 10, the circulation hole 11 of the upper sealing cover 10 is communicated with the upper liquid cavity 12 and the upper cavity, and the circulation hole 11 of the lower sealing cover 17 is communicated with the lower liquid cavity 18 and the lower. The piston body is installed between the upper sealing cover 10 and the lower sealing cover 17, and a sealing gasket 13 is installed between the outside of the piston body and the inner wall of the cylinder 7. The piston main body is of a hollow structure and comprises an inner cavity coaxial with the piston 6, a mass block 20 is coaxially arranged in the inner cavity, the outer wall of the mass block 20 is attached to the inner cavity, the mass block 20 can move along the inner wall of the inner cavity without friction, the mass block 20 is located in the middle of the piston main body when the piston main body is static, the mass block 20 is a symmetrical element, therefore, the mass block 20 is guaranteed to move vertically all the time when moving, and the phenomenon that the movement deviates from a central line is avoided. The upper and lower surfaces of the mass block 20 are coaxially connected with an upper spring 21 and a lower spring 19 respectively through an upper connecting rod 23 and a lower connecting rod 22, and the other ends of the upper spring 21 and the lower spring 19 are fixed on the upper and lower inner walls of the inner cavity respectively. The upper inner wall and the lower inner wall of the inner cavity of the moving inertia guide piston 6 are also provided with liquid flow holes with the diameter far smaller than that of the flow holes 11 so as to ensure that the mass block 20 can move up and down in the inner cavity. In fact, the upper seal cap 10 and the lower seal cap 17 may be absent from the piston 6, only an inner chamber is required in the center of the interior of the piston body, said inner chamber communicating with the upper chamber and the lower chamber, respectively. A plurality of spiral grooves are uniformly distributed along the inner cavity in the piston main body, one part of the spiral grooves are communicated with the upper cavity and the inner cavity, and the other part of the spiral grooves are communicated with the lower cavity and the inner cavity and are used for generating an inertia force different from or equal to the first inertia force; the mass block 20 selectively connects or disconnects the plurality of spiral grooves with the inner cavity according to the change of the acceleration, so as to change the inertia force of the whole structure.

As shown in fig. 3 and 4, a plurality of upper spiral grooves and a plurality of lower spiral grooves are uniformly distributed in the piston main body, the upper spiral grooves are communicated with the upper cavity and the inner cavity, and the lower spiral grooves are communicated with the lower cavity and the inner cavity; the upper spiral groove comprises a first upper spiral groove 14 and a second upper spiral groove 15, and a liquid outlet of the first upper spiral groove 14 and a liquid outlet of the second upper spiral groove 15 are respectively close to two ends of the mass block 20 in a balanced state; the lower spiral grooves comprise a first lower spiral groove 24 and a second lower spiral groove 16, and a liquid inlet of the first lower spiral groove 24 and a liquid inlet of the second lower spiral groove 16 are respectively close to two ends of the mass block 20 in a balanced state; the mass block 20 moves in the inner cavity through the change of the acceleration, and is used for selectively enabling the first upper spiral groove 14 and the first lower spiral groove 24 to be communicated with or blocked from the inner cavity, or selectively enabling the second upper spiral groove 15 and the second lower spiral groove 16 to be communicated with or blocked from the inner cavity. As shown in fig. 3, the position of the liquid outlet of the first upper spiral groove 14 and the position of the liquid inlet of the first lower spiral groove 24 are in a symmetrical relationship around the central axis of the movable piston 6. The liquid inlet of the second lower spiral groove 16 is positioned below the liquid inlet of the first lower spiral groove 24. The position relation between the liquid outlet of the second upper spiral groove 15 and the liquid inlet of the second lower spiral groove 16 is a symmetrical relation around the central axis of the movable piston 6. The first upper helical groove 14, the second upper helical groove 15, the second lower helical groove 16 and the first lower helical groove 24 are evenly distributed around the central axis of the piston 6 without any cross therebetween. At least one parameter of the number of spiral turns, the size of the groove diameter, the spiral tube pitch and the spiral radius of the first upper spiral groove 14, the second upper spiral groove 15, the second lower spiral groove 16 and the first lower spiral groove 24 is different, so that different inertia forces can be generated.

The invention can be used in the places needing vibration isolation such as vehicle suspension, airplane landing gear, propeller and the like, and supposing that the upper lifting lug 1 of the moving inertia guiding control device is connected with the object to be subjected to vibration isolation, and the lower lifting lug 9 is connected with the vibration input end, the device corresponds to three states along with the difference of the acceleration magnitude and the direction of the vibration input end in the working environment. And non-linear factors such as friction, parasitic damping and the like in the dynamic inertia steering control device are ignored. When the device is assembled, the upper spring 21 and the lower spring 19 respectively have certain pretightening force, so that the mass block 20 is in a balanced state. The cylinder body 7, the inner cavity of the piston main body, the upper liquid cavity 11, the lower liquid cavity 18, the first upper spiral groove 14, the second upper spiral groove 15, the second lower spiral groove 16, the first lower spiral groove 24 and the main spiral pipe 5 are filled with liquid, when the piston 6 moves up and down along with the piston rod 2, the piston 6 pushes the liquid to move in the first upper spiral groove 14, the second upper spiral groove 15, the second lower spiral groove 16, the first lower spiral groove 24 and the main spiral pipe 5 to form inertia force, and the ratio of the inertia force to the relative acceleration at two ends of the dynamic inertia guiding control device is constant and is called dynamic inertia coefficient.

The dynamic inertia coefficient can also be calculated by the following formula:

wherein m is_hDenotes the mass of liquid in the main spiral pipe 5 or the first upper spiral groove 14 or the second upper spiral groove 15 or the second lower spiral groove 16 or the first lower spiral groove 24, h denotes the spiral pitch, r, of the spiral pipe 5 or the first upper spiral groove 14 or the second upper spiral groove 15 or the second lower spiral groove 16 or the first lower spiral groove 24₄Denotes the radius of the helix, A, of the helix tube 5 or of the first upper helical groove 14 or of the second upper helical groove 15 or of the second lower helical groove 16 or of the first lower helical groove 24₁Represents the effective working area, A, of the piston 6₂Showing the cross-sectional area of the pipe of the spiral pipe 5 or the first upper spiral groove 14 or the second upper spiral groove 15 or the second lower spiral groove 16 or the first lower spiral groove 24.

Assuming that the spring rate of the upper spring 21 is k_pThe spring rate of the lower spring 19 is k_dThe pretension tension displacement of the upper spring 21 is x_pThe pretension tension displacement of the lower spring 19 is x_dWhen the mass of the mass block 20 is m and the gravity acceleration is g, the following relationship should be satisfied:

mg+k_d·x_d＝k_p·x_p。

when the mass 20 is at rest, x₁Is the vertical length, x, of the mass 20₂Indicates the distance, x, from the upper end of the liquid outlet of the first upper spiral groove 14 to the upper inner wall of the piston body₃The distance from the liquid outlet of the first upper spiral groove 14 to the lower surface of the mass block 20 is shown, the total vertical length of the piston body is L, and the pipe diameter of the first upper spiral groove 14 and the first lower spiral groove 24 is d₁The thicknesses of the upper spring 21 and the lower spring 19 when they are completely compressed are ignored, and the distance between the lower end of the liquid outlet of the first upper spiral groove 14 and the upper end of the liquid outlet of the second upper spiral groove 15 is z. The position relationship between the second upper spiral groove 15 and the mass 20 is the same as the position relationship between the first upper spiral groove 14 and the mass 20. I.e. y₂Indicates the distance, y, from the lower end of the liquid outlet of the second upper spiral groove 15 to the lower inner wall of the piston body₃Denotes the second upper screwThe distance from the upper end of the liquid outlet of the spiral groove 15 to the upper surface of the mass block 20, the pipe diameter of the second upper spiral groove 15 and the second lower spiral groove 16 is d₂The liquid outlet of the first upper spiral groove 14 and the liquid inlet of the first lower spiral groove 24 are located at the same horizontal position, and the first upper spiral groove 14 and the first lower spiral groove 24 are simultaneously communicated or blocked with the inner cavity under the action of acceleration through the mass block 20; the liquid outlet of the second upper spiral groove 15 and the liquid inlet of the second lower spiral groove 16 are positioned at the same horizontal position; the second upper spiral groove 15 and the second lower spiral groove 16 are simultaneously communicated or blocked with the inner cavity under the action of the acceleration through the mass 20.

In fig. 3, 4 and 5, in embodiment 1 of the present invention, a distance between a liquid outlet of the first upper spiral groove 14 and a liquid outlet of the second upper spiral groove 15 or a distance between a liquid inlet of the first lower spiral groove 24 and a liquid inlet of the second lower spiral groove 16 is smaller than a length of the mass 20, i.e. z<x₁In a balanced state, two ends of the mass block 20 respectively block a liquid outlet of the first upper spiral groove 14, a liquid outlet of the second upper spiral groove 15, a liquid inlet of the first lower spiral groove 24 and a liquid inlet of the second lower spiral groove 16; when the mass block 20 moves downwards, the first upper spiral groove 14 and the first lower spiral groove 24 are simultaneously communicated with the inner cavity; when the mass 20 moves upwards, the second upper helical groove 15 and the second lower helical groove 16 are simultaneously communicated with the inner cavity.

When z < x₁In this case, the preferred positional relationship among the first upper spiral groove 14, the second upper spiral groove 15 and the mass 20 is as shown in fig. 5, and they satisfy the following relationship:

x₂+d₁≤x₁，x₃+d₁≤x₁，z+d₁+d₂＜x₁＜x₂+d₁+z＜L；

y₂+d₂≤x₁，y₃+d₂≤x₁，z+d₁+d₂＜x₁＜y₂+d₁+z＜L；

by limiting the positions of the first upper spiral groove 14 and the second upper spiral groove 15, it is ensured that the second upper spiral groove 15 and the second lower spiral groove 16 cannot be communicated with each other when the first upper spiral groove 14 and the first lower spiral groove 24 are communicated with each other, and the first upper spiral groove 14 and the first lower spiral groove 24 cannot be communicated with each other when the second upper spiral groove 15 and the second lower spiral groove 16 are communicated with each other.

In a stable working state, when the vibration input by the vibration input end is uniform, the two ends of the dynamic inertia guiding control device, namely the upper lifting lug 1 and the lower lifting lug 9 are not stressed, and the mass block 20 is in a balanced state at the moment. The first upper spiral groove 14 and the first lower spiral groove 24 are not communicated with each other, and no dynamic inertia coefficient is generated, the second upper spiral groove 15 and the second lower spiral groove 16 are not communicated with each other, no inertia force is generated, the inertia force is generated by the main spiral pipe 5, and the dynamic inertia coefficient generated at the moment is recorded as b₁。

When the vibration input end input signal generates upward acceleration in a stable working state, the two ends of the moving inertia guiding control device are subjected to an upward resultant force F_pGenerating an upward acceleration a_p. At this time, the mass 20 moves downward relative to the cylinder 7 due to inertia, the lower spring 19 is compressed, the first upper spiral groove 14 and the first lower spiral groove 24 are communicated with each other, and the liquid flows in the first upper spiral groove 14 and the first lower spiral groove 24 to generate inertia force. As the mass 20 moves downwards, the volume of the inner cavity changes, and the mass 20 presses the liquid in the inner cavity of the piston body to flow out of the piston body, pass through the lower liquid cavity 18 and flow back to the lower cavity through the circulating hole 11. At this time, the inertia force is generated by the first upper spiral groove 14, the first lower spiral groove 24 and the main spiral pipe 5, and the kinetic inertia coefficient generated at this time is recorded as b₂。

When the vibration input end input signal generates downward acceleration in a stable working state, the two ends of the moving inertia guiding control device are subjected to a downward resultant force F_dGenerating a downward acceleration a_d. At this time, the mass 20 moves upward relative to the cylinder 7 due to inertia, the upper spring 21 is compressed, the second upper spiral groove 15 and the second lower spiral groove 16 are communicated with each other, and the liquid flows in the second upper spiral groove 15 and the second lower spiral groove 16 to generate inertia force. Due to the mass block20 moves upwards, the volume of the inner cavity changes, and the mass block 20 extrudes liquid in the inner cavity of the piston body to flow out of the piston body and flow back to the upper cavity through the upper liquid cavity 12 and the through hole 11. At this time, the inertia force is generated by the second upper spiral groove 15, the second lower spiral groove 16 and the main spiral pipe 5, and the kinetic inertia coefficient generated at this time is recorded as b₃。

The dynamic inertia coefficient b under three states is that the spiral turns, the groove diameter, the thread pitch and the spiral radius of the main spiral pipe 5, the first upper spiral groove 14, the second upper spiral groove 15, the second lower spiral groove 16 and the first lower spiral groove 24 are not determined₂、b₁、b₃The dynamic inertia coefficient b can not be determined, and in the actual use process, the dynamic inertia coefficient b can be set by adjusting the spring stiffness and the pretightening force of the upper spring 21 and the lower spring 19 according to the actual conditions₂、b₁、b₃When the three states are switched, the acceleration threshold value of the signal input by the vibration input end can be set, and the dynamic inertia coefficient b in the three states can be realized by setting parameters such as the number of spiral turns, the size of the groove diameter, the spiral pipe pitch, the spiral radius, the liquid density and the like₂、b₁、b₃The size of (2) meets the control requirement.

The positive direction of the acceleration is set to the upward direction, and the downward direction is set to the negative direction.

Then in z < x₁The control rule of the dynamic inertia guiding control device is as follows:

wherein b represents the kinetic inertia coefficient of the kinetic inertia guiding control device, and a represents the acceleration value of the input signal of the vibration input end.

FIG. 6, FIG. 7 and FIG. 8 show an embodiment 2 of the present invention, in which the distance between the liquid outlet of the first upper spiral groove 14 and the liquid outlet of the second upper spiral groove 15 or the distance between the liquid inlet of the first lower spiral groove 24 and the liquid inlet of the second lower spiral groove 16 is greater than or equal to the length of the mass block 20, i.e. z ≧ x₁In the equilibrium state, the outlet of the first upper spiral groove 14 and the second upper spiral grooveThe liquid outlets of the two upper spiral grooves 15, the liquid inlet of the first lower spiral groove 24 and the liquid inlet of the second lower spiral groove 16 are respectively communicated with the inner cavity; when the mass block 20 moves upwards, the first upper spiral groove 14 and the first lower spiral groove 24 are simultaneously blocked from the inner cavity; when the mass 20 moves downwards, the second upper spiral groove 15 and the second lower spiral groove 16 are simultaneously blocked from the inner cavity.

When z is larger than or equal to x₁In this case, it is preferable that the first upper spiral groove 14, the second upper spiral groove 15, and the mass 20 are arranged in the following relationship as shown in fig. 8:

x₂≥x₁，x₃≥x₁，x₁＜L,x₂＜L,x₃＜L

by performing the above position limitation on the first upper spiral groove 14, the first lower spiral groove 24, the second upper spiral groove 15 and the second lower spiral groove 16, when the first upper spiral groove 14 and the first lower spiral groove 24 are communicated with each other, the second upper spiral groove 15 and the second lower spiral groove 16 are also communicated with each other, and only when the mass block 20 moves to a specific position, the first upper spiral groove 14 and the first lower spiral groove 24 or the second upper spiral groove 15 and the second lower spiral groove 16 are not communicated with each other.

In a stable working state, when the vibration input by the vibration input end is uniform, the two ends of the dynamic inertia guiding control device, namely the upper lifting lug 1 and the lower lifting lug 9 are not stressed, and the mass block 20 is in a balanced state at the moment. The first upper spiral groove 14 and the first lower spiral groove 24 are communicated with each other, the second upper spiral groove 15 and the second lower spiral groove 16 are communicated with each other, the inertia force is generated by the first upper spiral groove 14, the first lower spiral groove 24, the second upper spiral groove 15, the second lower spiral groove 16 and the main spiral pipe 5 together, and the generated dynamic inertia coefficient is recorded as b₁₁。

In a stable working state, when the vibration input end input signal continuously generates upward acceleration, the range of upward resultant force applied to two ends of the moving inertia guiding control device is [ F ]_p1,F_p2[, producing an upward acceleration in the range of [ a ]_p1,a_p2]. The mass 20 is then moved downwards with respect to the cylinder 7 by inertia, compressing itAnd the lower spring 19 changes the volume of the inner cavity due to the downward movement of the mass block 20, and the mass block 20 presses the liquid in the inner cavity of the piston body to flow out of the piston body, pass through the lower liquid cavity 18 and flow back to the lower cavity through the circulating hole 11. When the mass 20 moves below the first upper spiral groove 14, but the lower surface of the mass 20 is located below the second upper spiral groove 15, and the upper surface of the mass 20 is located above the second upper spiral groove 15, the mass 20 blocks the liquid flow between the second upper spiral groove 15 and the second lower spiral groove 16, at this time, the inertia force is generated by the first upper spiral groove 14, the first lower spiral groove 24 and the main spiral pipe 5, and the dynamic inertia coefficient generated at this time is recorded as b₂₂. When the upward acceleration generated by the input signal of the vibration input end continues to increase, the upward resultant force received by the two ends of the moving inertia guiding control device is more than F_p2The resulting upward acceleration is greater than a_p2At this time, the mass 20 continues to move downwards relative to the cylinder 7 due to inertia, when the upper surface of the mass 20 is located below the second upper spiral groove 15, the second upper spiral groove 15 and the second lower spiral groove 16 are communicated with each other again, at this time, the inertia force is generated by the first upper spiral groove 14, the first lower spiral groove 24, the second upper spiral groove 15, the second lower spiral groove 16 and the spiral pipe 5, and the kinetic inertia coefficient generated at this time is b₁₁。

In a stable working state, when the input signal of the vibration input end continuously generates downward acceleration, the range of the downward resultant force applied to the two ends of the moving inertia guiding control device is [ F ]_d1,F_d2]Producing a downward acceleration in the range of [ a ]_d1,a_d2]. At this time, the mass 20 moves upward relative to the cylinder 7 due to inertia, the upper spring 21 is compressed, when the mass 20 moves above the second upper spiral groove 15, but the upper surface of the mass 20 is located above the first upper spiral groove 14, and the lower surface of the mass 20 is located below the first upper spiral groove 14, the mass 20 blocks the liquid flow between the first upper spiral groove 14 and the first lower spiral groove 24, at this time, the inertia force is generated by the second upper spiral groove 15, the second lower spiral groove 16 and the main spiral pipe 5, and the dynamic inertia coefficient generated at this time is recorded as b₃₃. As the mass 20 moves upward, the volume of the cavity changes and the mass 20 presses against the piston bodyThe liquid in the inner cavity flows out of the piston main body and flows back to the upper cavity through the upper liquid cavity 12 and the circulating hole 11. When the downward acceleration generated by the input signal of the vibration input end continues to increase, the downward resultant force received by the two ends of the moving inertia guiding control device is more than F_d2The generated downward acceleration is greater than a_d2At this time, the mass 20 continues to move upwards relative to the cylinder 7 due to inertia, when the lower surface of the mass 20 is located above the first upper spiral groove 14, the first upper spiral groove 14 and the first lower spiral groove 24 are communicated with each other again, at this time, the inertia force is generated by the first upper spiral groove 14, the first lower spiral groove 24, the second upper spiral groove 15, the second lower spiral groove 16 and the spiral pipe 5, and the kinetic inertia coefficient generated at this time is b₁₁。

At z ≧ x₁The control rule of the dynamic inertia guiding control device is as follows:

it should be understood that although the present description has been described in terms of various embodiments, not every embodiment includes only a single embodiment, and such description is for clarity purposes only, and those skilled in the art will recognize that the embodiments described herein may be combined as suitable to form other embodiments, as will be appreciated by those skilled in the art.

The above-listed detailed description is only a specific description of a possible embodiment of the present invention, and they are not intended to limit the scope of the present invention, and equivalent embodiments or modifications made without departing from the technical spirit of the present invention should be included in the scope of the present invention.