Floating ring with constant inner diameter
By designing a floating ring with a constant inner diameter, radial floating is achieved by utilizing the deformation of the annular matrix and the elastic acceptor. This solves the problems of complex structure and poor universal adaptability of existing floating components, achieving high-precision alignment and stability, and improving the reliability and service life of the equipment.
Patent Information
- Application Number
- CN202520557331.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-27
- Publication Date
- 2025-12-26
- Estimated Expiration
- 2035-03-27
AI Technical Summary
Existing floating components or kits have complex structures, are inconvenient to maintain and disassemble, have poor universal adaptability, are difficult to control costs, and are difficult to meet the needs of different mechanical parts.
Design a floating ring with a constant inner diameter, comprising an annular base and an elastic receptor. Radial floating is achieved through the deformation of the elastic receptor. Multiple arc-shaped wing plates are used to evenly distribute the load, ensuring high-precision alignment and stability.
The simplified structure facilitates maintenance and disassembly, improves universal adaptability, enhances the stability and accuracy of radial floating, extends equipment lifespan, and ensures the effectiveness of power transmission.
Smart Images

Figure CN223725281U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to mechanical parts connection technical field, concretely relates to a floating ring of constant inner diameter. BACKGROUND
[0002] In some occasions requiring high-precision centering and allowing radial floating, floating assemblies or sets are usually installed between the mechanical parts connected to each other, which functions to compensate or eliminate the machining errors and assembly deviations of the mechanical parts, realize flexible connection, protect the relevant parts and equipment to run smoothly, and prolong the service life of the equipment.
[0003] At present, to realize the radial floating of multiple angles in the circumference, the traditional floating assemblies or sets have multiple elastic members, the structure is relatively complex, which is not conducive to maintenance and disassembly and replacement, and different mechanical parts often need to be equipped with floating assemblies or sets of multiple structures, which has poor universal adaptability, is not conducive to cost control and spare parts management. UTILITY MODEL CONTENT
[0004] In view of the deficiencies of the prior art, the utility model provides a floating ring with constant inner diameter to solve the problems that the existing floating assemblies or sets have multiple elastic members, the structure is relatively complex, which is not conducive to maintenance and disassembly and replacement, and different mechanical parts often need to be equipped with floating assemblies or sets of multiple structures, which has poor universal adaptability, is not conducive to cost control and spare parts management.
[0005] To achieve the above object, the utility model provides the following technical scheme:
[0006] A floating ring with constant inner diameter comprises:
[0007] An annular base body is sleeved on the outer part of a first component with constant inner diameter; and
[0008] An elastic receptor is connected to the outer part of the annular base body and embedded in a second component.
[0009] Wherein, the elastic receptor can be deformed to store stress under the action of radial force, and release the stress through radial floating at any angle in the circumference to quickly center the first component and the second component and realize self-centering adjustment between them after the radial force disappears.
[0010] In one embodiment of the present application, the elastic receptor comprises multiple arc-shaped wings distributed uniformly around the outer circumference of the annular base body and connected with the inner sidewall of the second component.
[0011] One end of each of the arc-shaped wings is connected with a protruding part provided on the outer circumferential surface of the annular base body.
[0012] Another end of each of the arc-shaped wing plates gradually extends away from the center of the annular base from the protruding part to form a floating gap between the concave surface of the arc-shaped wing plate and the outer surface of the annular base.
[0013] In one embodiment of the present disclosure, the protruding part has a first arc-shaped surface, and the arc-shaped wing plates have a second arc-shaped surface and a third arc-shaped surface, which are sequentially connected.
[0014] The concave surface of the arc-shaped wing plate is a fourth arc-shaped surface, which is connected to the third arc-shaped surface through a rounded corner.
[0015] The gap between the fourth arc-shaped surface of one arc-shaped wing plate, the first arc-shaped surface of an adjacent protruding part, and the second arc-shaped surface of an adjacent arc-shaped wing plate is the floating gap.
[0016] In one embodiment of the present disclosure, the projection of the rounded corner of one arc-shaped wing plate along the radial direction of the annular base falls on the second arc-shaped surface of an adjacent arc-shaped wing plate from 1 / 3 of the second arc-shaped surface away from the third arc-shaped surface.
[0017] In one embodiment of the present disclosure, a plurality of the arc-shaped wing plates are integrally formed with the annular base.
[0018] In one embodiment of the present disclosure, the first arc-shaped surface is tangent to and concentric with the second arc-shaped surface.
[0019] The circle on which the first arc-shaped surface and the second arc-shaped surface are located is eccentric to the inner surface of the annular base.
[0020] The third arc-shaped surface is concentric with the inner surface of the annular base.
[0021] The fourth arc-shaped surface is eccentric to the inner surface of the annular base.
[0022] In one embodiment of the present disclosure, the thickness of each of the arc-shaped wing plates changes in the manner of first increasing and then decreasing along the extension direction thereof.
[0023] In one embodiment of the present disclosure, the thickness of each of the arc-shaped wing plates is the largest at the connection between the second arc-shaped surface and the third arc-shaped surface.
[0024] In one embodiment of the present disclosure, the arc-shaped wing plates are evenly distributed around the outer circumference of the annular base.
[0025] In one embodiment of the present disclosure, the arc-shaped wing plates are evenly distributed around the outer circumference of the annular base.
[0026] In one embodiment of the present disclosure, the first component is a shaft component.
[0027] The second component is a hole-type component.
[0028] Compared with the prior art, the beneficial effects of this utility model are:
[0029] 1. By deforming the elastic receptor connected to the annular matrix, the radial floating of the first or second component at any angle around its circumference is achieved, which greatly simplifies the structure and makes maintenance and disassembly convenient. Moreover, the annular matrix and the elastic receptor are set internally and externally, which can be used for different mechanical parts, with strong versatility and adaptability, and can effectively control the cost of accessories.
[0030] 2. By using multiple circumferentially distributed arc-shaped wing plates, the load on this floating ring can be evenly distributed to the annular base, ensuring uniform deformation of each arc-shaped wing plate, maintaining the reliability of the rebound (elastic function of the elastic receptor) of each arc-shaped wing plate, enhancing the stability of radial floating, thereby ensuring high-precision fit between this floating ring and the first and second components.
[0031] 3. The floating gap is designed with controllable radial elastic deformation, allowing the elastic receptor (arc-shaped wing plate) to produce small displacements in the radial direction, thereby absorbing stress caused by vibration, thermal expansion, or dynamic loads and avoiding wear or failure caused by rigid contact. In addition, through the synergistic effect of elastic deformation and the precision dimensions of the components themselves, this floating ring can ensure the positioning accuracy between the first and second components, significantly improving the reliability and service life of the system containing the first and second components. Furthermore, the third arc-shaped surface, which is concentric with the inner circular surface of the annular base, abuts against the inner wall of the second component in a surface contact manner, ensuring the effective transmission of power between the first and second components. Attached Figure Description
[0032] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.
[0033] Fig. 1 This is a three-dimensional structural diagram of the present invention;
[0034] Fig. 2 This is a schematic diagram of the main structure of this utility model;
[0035] Fig. 3 This is a cross-sectional view of the present invention after it is installed between the first component and the second component. Detailed Implementation
[0036] In the following, certain example embodiments are simply described. As those skilled in the art will realize, the described embodiments can be modified in various different ways without departing from the spirit or scope of the present application. The drawings and description are therefore to be regarded as illustrative in nature rather than restrictive.
[0037] In the description of the present application, it is to be understood that the orientations or positional relationships indicated by the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like are based on the orientations or positional relationships shown in the drawings, and are merely for the convenience of describing the present application and simplifying the description, and therefore cannot be understood as indicating or implying that the devices or elements indicated must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the present application.
[0038] In addition, the terms "first", "second", "third", etc. are used only for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the technical features indicated. Therefore, the features defined with "first", "second", etc. can explicitly or implicitly include one or more of the features. In the description of the present application, the meaning of "a plurality of" is two or more, unless otherwise explicitly specified and limited.
[0039] In the present application, unless otherwise explicitly specified and limited, the terms "mounting", "connecting", "connecting", "fixing" and the like should be understood broadly, for example, it can be fixed connection, or detachable connection, or integrated; it can be directly connected, or indirectly connected through an intermediate medium; it can be the internal communication of two elements or the interaction relationship of two elements. For those skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.
[0040] In the present application, unless otherwise explicitly specified and limited, the "upper" or "lower" of the first feature to the second feature can include the direct contact of the first and second features, or can include the contact of the first and second features through another feature between them. Moreover, the "upper", "upper" and "upper" of the first feature to the second feature include the vertical height of the first feature above and oblique to the second feature, or only indicate that the horizontal height of the first feature is higher than that of the second feature. The "below", "below" and "below" of the first feature to the second feature include the vertical height of the first feature below and oblique to the second feature, or only indicate that the horizontal height of the first feature is less than that of the second feature.
[0041] The following disclosure provides many different embodiments or examples for implementing different structures of the present application. For simplicity of the disclosure, the description below refers to the drawings to illustrate specific embodiments in which the present application can be practiced. In a normal manner, the drawings are not necessarily to scale and the specific measurements are not necessarily provided. The same or similar characters refer to the same or similar parts throughout the several views of the drawings.
[0042] The embodiments of the present application will be described in detail below with reference to the drawings.
[0043] Referring to Figs. 1-3 The present application provides a floating ring 300 with constant inner diameter, comprising:
[0044] a ring-shaped base 310, which is sleeved on the first component 100 with constant inner diameter; and
[0045] a resilient receptor 320, which is connected to the outside of the ring-shaped base 310 and embedded in the second component 200;
[0046] Wherein, the resilient receptor 320 can be deformed to store stress under the action of radial force, and release the stress through radial floating at any angle of circumference after the radial force disappears to quickly center the first component 100 and the second component 200 to realize self-centering adjustment between them.
[0047] Specifically, the elastic receptor 320 includes a plurality of arc-shaped wings 321 distributed around the outer circumference of the annular base 310 and connected with the inner side wall of the second component 200, each arc-shaped wing 321 is connected with a protrusion 311 arranged on the outer circumferential surface of the annular base 310 at one end, and extends away from the center of the annular base 310 at the other end to form a floating gap between the inner concave surface of the arc-shaped wing 321 and the outer circumferential surface of the annular base 310. Under the action of the radial force, each arc-shaped wing 321 is extruded and deformed towards the floating gap, and the stress is stored through the elastic receptor 320; after the radial force disappears, the stress is released through the elastic recovery of each arc-shaped wing 321, thereby driving the first component 100 or the second component 200 to produce radial floating at any angle around the circumference, so that the first component 100 and the second component 200 are quickly re-centered to realize self-centering adjustment between them. That is, the radial floating of the first component 100 or the second component 200 at any angle around the circumference is realized by the deformation of the elastic receptor 320 connected to the outside of the annular base 310, the structure is greatly simplified, and maintenance and disassembly are convenient. Moreover, the annular base 310 and the elastic receptor 320 are arranged inside and outside, which can be used for different mechanical parts, has strong universal adaptability, and can effectively control the cost of accessories; at the same time, through the plurality of circumferentially distributed arc-shaped wings 321, the load received by the floating ring 300 can be uniformly dispersed to the annular base 310, ensuring uniform deformation of each arc-shaped wing 321, maintaining the reliability of the elastic recovery (elastic function of the elastic receptor 320) of each arc-shaped wing 321, enhancing the stability of the radial floating, and thereby ensuring the high-precision cooperation between the floating ring 300 and the first component 100 and the second component 200.
[0048] The protrusion 311 has a first arc-shaped surface 311a protruding outward, the arc-shaped wing 321 has a second arc-shaped surface 321a and a third arc-shaped surface 321b protruding outward, and the first arc-shaped surface 311a, the second arc-shaped surface 321a and the third arc-shaped surface 321b are sequentially connected; the inner concave surface of the arc-shaped wing 321 is a fourth arc-shaped surface 321c, and the fourth arc-shaped surface 321c is connected with the third arc-shaped surface 321b through a round corner 321d; the gap between the fourth arc-shaped surface 321c of one arc-shaped wing 321 and the first arc-shaped surface 311a of the adjacent protrusion 311 and the second arc-shaped surface 321a of the adjacent arc-shaped wing 321 is the floating gap. Under the action of the radial force, each arc-shaped wing 321 can be extruded and uniformly and symmetrically deformed towards the floating gap, thereby eliminating the eccentricity problem caused by machining errors and assembly deviations, and automatically adjusting the position of the first component 100 or the second component 200 during elastic recovery, thereby ensuring that the center axes of the two components are aligned (i.e., self-centering).
[0049] The projection of the fillet 321d of an arc-shaped wing plate 321 radially inward along the annular base 310 falls on the second arc-shaped surface 321a of the adjacent arc-shaped wing plate 321 from 1 / 3 of the second arc-shaped surface 321a away from the third arc-shaped surface 321b. In this way, one arc-shaped wing plate 321 can cover 2 / 3 of the second arc-shaped surface 321a of the adjacent arc-shaped wing plate 321, so that each arc-shaped wing plate 321 can form an overlapping state when pressed against each other, thereby ensuring that the deformation of each arc-shaped wing plate 321 to the floating gap is uniform and symmetrical.
[0050] In order to reduce the manufacturing cost of the floating ring 300 and ensure the connection strength of the arc-shaped wing plate 321 and the convex part 311 to prolong the service life of the floating ring 300, a plurality of arc-shaped wing plates 321 are integrally processed with the annular base 310. Specifically, to facilitate the processing of the floating gap between each arc-shaped wing plate 321 and the annular base 310, the first arc-shaped surface 311a is tangent to and concentric with the second arc-shaped surface 321a (i.e., they share a common circle), the circle on which the first arc-shaped surface 311a and the second arc-shaped surface 321a are located is eccentric to the inner circular surface of the annular base 310, the third arc-shaped surface 321b is concentric with the inner circular surface of the annular base 310, and the fourth arc-shaped surface 321c is eccentric to the inner circular surface of the annular base 310. The floating gap designed and processed in this way has a controllable radial elastic deformation amount, can allow the elastic receptor 320 (arc-shaped wing plate 321) to produce a slight displacement in the radial direction, thereby absorbing stress caused by vibration, thermal expansion or dynamic load, avoiding wear or failure caused by rigid contact; in addition, through the synergistic effect of elastic deformation and the precise dimensions of the parts themselves, the floating ring 300 can ensure the positioning accuracy between the first part 100 and the second part 200, significantly improving the reliability and service life of the system containing the first part 100 and the second part 200; furthermore, the third arc-shaped surface 321b concentrically arranged with the inner circular surface of the annular base 310 is in surface contact with the inner side wall of the second part 200, which can ensure effective transmission of power between the first part 100 and the second part 200.
[0051] The thickness of each arc-shaped wing plate 321 changes in the manner of first increasing and then decreasing along its extension direction (i.e., the direction gradually away from the center of the annular base 310 from the convex part 311). The thickness of each arc-shaped wing plate 321 is the largest (i.e., the thickest) at the connection between the second arc-shaped surface 321a and the third arc-shaped surface 321b. In this way, when one arc-shaped wing plate 321 is pressed against the adjacent arc-shaped wing plate 321, the fillet 321d on the arc-shaped wing plate 321 can be completely accommodated in the corresponding floating gap after deformation, further ensuring that each arc-shaped wing plate 321 can produce uniform and symmetrical deformation.
[0052] The arc-shaped wing plates 321 are evenly distributed around the outer circumference of the annular base 310.
[0053] In the embodiment, the arc-shaped wing plates 321 are evenly distributed around the outer circumference of the annular base 310.
[0054] The first component 100 is a shaft component (such as a shaft core), and the second component 200 is a hole component (such as a sleeve).
[0055] In summary, the floating ring 300 is applicable to the connection of shaft and hole components in a precision transmission system, and is also applicable to a floating joint for compensating dynamic deviation in an automatic device, a damping and buffering element in a high-vibration environment, and other occasions requiring high-precision centering and allowing radial floating.
[0056] The above embodiments are only preferred embodiments of the present application, and are not a limitation on the technical solutions of the present application. Any technical solution that can be realized on the basis of the above embodiments without creative labor should be considered to fall within the protection scope of the patent of the present application.
Claims
1. A constant internal diameter floating ring, characterised in that, Comprise: a ring-shaped base body, which is sleeved on the first component with a constant inner diameter; and a resilient receiver, which is connected to the outside of the ring-shaped base body and is embedded in the second component; wherein the resilient receiver can be deformed to store stress under the action of a radial force and release the stress through radial floating of an arbitrary angle of the circumference after the radial force disappears to quickly center the first component and the second component to achieve self-centering adjustment between the two.
2. The floating ring with constant inner diameter according to claim 1, wherein: the resilient receiver comprises a plurality of arc-shaped wings, which are evenly distributed around the outer circumference of the ring-shaped base body and are connected to the inner side wall of the second component; one end of each of the arc-shaped wings is connected to a protrusion provided on the outer circumferential surface of the ring-shaped base body; the other end of each of the arc-shaped wings gradually extends away from the center of the ring-shaped base body to form a floating gap between the inner concave surface of the arc-shaped wing and the outer circumferential surface of the ring-shaped base body.
3. The floating ring with constant inner diameter according to claim 2, wherein: the protrusion has a first arc-shaped outer convex surface, the arc-shaped wing has a second arc-shaped outer convex surface and a third arc-shaped outer convex surface, and the first arc-shaped surface, the second arc-shaped surface and the third arc-shaped surface are sequentially connected; the inner concave surface of the arc-shaped wing is a fourth arc-shaped surface, and the fourth arc-shaped surface is connected to the third arc-shaped surface through a round corner; the gap between the fourth arc-shaped surface of one arc-shaped wing, the first arc-shaped surface of the adjacent protrusion and the second arc-shaped surface of the adjacent arc-shaped wing is the floating gap.
4. The constant internal diameter floating ring of claim 3, wherein, The projection of the round corner of one arc-shaped wing along the radial direction of the ring-shaped base body falls on the second arc-shaped surface of the adjacent arc-shaped wing at a position 1 / 3 away from the third arc-shaped surface.
5. An inner constant diameter floating ring according to claim 3 or 4, characterized in that The plurality of arc-shaped wings are integrally formed with the ring-shaped base body.
6. The floating ring with constant inner diameter according to claim 5, wherein: the first arc-shaped surface is tangent to and concentric with the second arc-shaped surface; the circle on which the first arc-shaped surface and the second arc-shaped surface are located is eccentric to the inner circumferential surface of the ring-shaped base body; the third arc-shaped surface is concentric with the inner circumferential surface of the ring-shaped base body; the fourth arc-shaped surface is eccentric to the inner circumferential surface of the ring-shaped base body.
7. The floating ring with constant inner diameter according to claim 3 or 6, wherein: the thickness of each arc-shaped wing changes in a manner of first increasing and then decreasing along the extension direction of the arc-shaped wing; wherein the thickness of each arc-shaped wing is the largest at the connection between the second arc-shaped surface and the third arc-shaped surface.
8. The constant internal diameter floating ring of claim 7, wherein, There are at least 3 arc-shaped wings evenly distributed around the outer circumference of the ring-shaped base body.
9. The constant internal diameter floating ring of claim 8, wherein, There are 6 arc-shaped wings evenly distributed around the outer circumference of the ring-shaped base body.
10. The floating ring with constant inner diameter according to claim 1 or 2, wherein: the first component is a shaft component; the second component is a hole component.