Anti-vibration electronic compass structure
By installing shock-absorbing components at the four corners of the electronic compass body and using lateral and longitudinal elastic elements to absorb equipment vibration, the problem of electronic compass damage caused by equipment vibration in the prior art is solved, and the service life of the electronic compass is improved.
Patent Information
- Application Number
- CN202520412086.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-11
- Publication Date
- 2026-01-06
- Estimated Expiration
- 2035-03-11
AI Technical Summary
Existing electronic compasses are easily damaged by equipment vibration, resulting in a shortened service life.
Four sets of vibration damping components are installed at the four corners of the electronic compass body. Each set of vibration damping components consists of an outer sleeve and a mounting sleeve. The vibration of the equipment is absorbed by the lateral and longitudinal elastic elements, including lateral elastic elements and longitudinal elastic elements. Vibration reduction is achieved by using a detachable connection structure.
It effectively absorbs lateral and longitudinal vibrations of the equipment, reduces damage to components, and extends the service life of the electronic compass.
Smart Images

Figure CN223769529U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to electronic compass technical field especially is related to a kind of anti-vibration electronic compass structure. BACKGROUND
[0002] Electronic compass, also known as digital compass, is a kind of navigation instrument or attitude sensor using geomagnetic field to determine north pole. It determines direction by measuring earth's magnetic field, with low energy consumption, small size, light weight, high precision and miniaturization. Electronic compass is mainly composed of magnetometer module, accelerometer module, gyroscope module, MCU module and serial conversion module, which can calculate heading angle and attitude parameters by processing the signals of these modules. The existing electronic compass is usually fixed on the equipment by bolts, lacks anti-vibration function, and is easily damaged by the vibration of the equipment during work, thus reducing its service life. SUMMARY
[0003] The utility model aims at overcoming the above technical deficiencies, and provides an anti-vibration electronic compass structure to solve the technical problem that the existing electronic compass is usually fixed on the equipment by bolts, lacks anti-vibration function, and is easily damaged by the vibration of the equipment during work, thus reducing its service life.
[0004] To achieve the above technical purpose, the technical scheme of the utility model provides an anti-vibration electronic compass structure, which comprises an electronic compass main body and four groups of shock-absorbing components installed at four corners of the electronic compass main body. Each corner of the electronic compass main body is provided with a mounting hole. Each group of shock-absorbing components comprises an outer sleeve arranged inside the corresponding mounting hole. A mounting sleeve is coaxially arranged inside the outer sleeve. A plurality of transverse elastic members are connected between the outer wall of the mounting sleeve and the inner wall of the outer sleeve. The two ends of the mounting sleeve are connected to the electronic compass main body through longitudinal elastic members.
[0005] Further, the transverse elastic member is a first spring.
[0006] Further, the inner wall of the outer sleeve is provided with a first fixing column, and the outer wall of the mounting sleeve is provided with a second fixing column. One end of the first spring is sleeved on the first fixing column and in contact with the inner wall of the outer sleeve but not fixedly connected. The other end of the first spring is sleeved on the second fixing column and in contact with the outer wall of the mounting sleeve but not fixedly connected.
[0007] Further, the longitudinal elastic member comprises two second springs sleeved on the two ends of the mounting sleeve respectively.
[0008] Further, the mounting sleeve is provided with a stop ring at each end, one end of one of the second springs is in contact with one of the stop rings but not fixedly connected, the other end of the second spring is in contact with one side of the electronic compass body but not fixedly connected, one end of the other second spring is in contact with the other stop ring but not fixedly connected, and the other end of the other second spring is in contact with the other side of the electronic compass body but not fixedly connected.
[0009] Further, the at least one stop ring is detachably connected with the mounting sleeve through a detachable connection structure.
[0010] Further, the detachable connection structure comprises a clamping groove arranged on the outer wall of the mounting sleeve and a clamping block arranged on the inner wall of the stop ring and matched with the clamping groove.
[0011] Further, the clamping groove is in L-shaped structure.
[0012] The beneficial effects of the present application include: the anti-vibration electronic compass structure provided by the present application can absorb the transverse vibration and longitudinal vibration of the equipment during work through the transverse elastic member and the longitudinal elastic member, has good damping effect, avoids damage of the parts on the electronic compass body due to vibration, and improves the service life. BRIEF DESCRIPTION OF DRAWINGS
[0013] Figure 1 is a schematic structural view of the anti-vibration electronic compass structure of the embodiment of the present application;
[0014] Figure 2 is Figure 1 the enlarged view of A of figure
[0015] Figure 3 is Figure 1 the sectional view of A of figure
[0016] Figure 4 is Figure 1 the exploded view of A of figure
[0017] Figure 5 is a schematic structural view of the mounting sleeve of the embodiment of the present application;
[0018] In the figure: 1, electronic compass body; 11, mounting hole; 2, damping assembly; 21, outer sleeve; 211, first fixed column; 22, mounting sleeve; 221, second fixed column; 222, stop ring; 2221, clamping block; 223, clamping groove; 23, transverse elastic member; 24, longitudinal elastic member. DETAILED DESCRIPTION
[0019] In order to make the purpose, technical scheme and advantages of the present application more clear, the present application will be further described in detail below in combination with the drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application and do not limit the present application.
[0020] This utility model embodiment provides a vibration-resistant electronic compass structure, such as Figures 1-5 As shown, the device includes an electronic compass body 1 and four sets of vibration damping components 2 installed at the four corners of the electronic compass body 1. Each of the four corners of the electronic compass body 1 has a mounting hole 11. Each set of vibration damping components 2 includes an outer sleeve 21 located inside the corresponding mounting hole 11. The outer sleeve 21 is a hollow cylindrical body with openings at both ends. A mounting sleeve 22 is coaxially mounted inside the outer sleeve 21. The mounting sleeve 22 is also a hollow cylindrical body with openings at both ends. The outer wall of the mounting sleeve 22 is connected to the inner wall of the outer sleeve 21 by several transverse elastic members 23. The two ends of the mounting sleeve 22 are connected to the electronic compass body 1 by longitudinal elastic members 24. During installation, the mounting sleeves 22 on the four sets of vibration damping components 2 are bolted to the device. The transverse elastic members 23 and longitudinal elastic members 24 absorb the transverse and longitudinal vibrations of the device during operation, resulting in good vibration damping and preventing damage to the components of the electronic compass body 1 due to vibration, thus extending its service life.
[0021] In this embodiment, the transverse elastic element 23 is a first spring. When the transverse elastic element 23 is the first spring, the inner wall of the outer sleeve 21 is provided with a first fixing post 211, which is integrally formed with the outer sleeve 21. The outer wall of the mounting sleeve 22 is provided with a second fixing post 221, which is integrally formed with the mounting sleeve 22. One end of the first spring is sleeved on the first fixing post 211 and contacts the inner wall of the outer sleeve 21 but is not fixedly connected. The other end of the first spring is sleeved on the second fixing post 221 and contacts the outer wall of the mounting sleeve 22 but is not fixedly connected. This allows for easy disassembly and reassembly between the outer sleeve 211 and the mounting sleeve 22 and the first transverse elastic element 23.
[0022] The transverse elastic element 23 in this invention is not limited to using a first spring. In other embodiments, the transverse elastic element 23 may be a metal sheet, a silicone block, or other elastic objects.
[0023] In this embodiment, the longitudinal elastic element 24 includes two second springs sleeved at both ends of the mounting sleeve 22. When the longitudinal elastic element 24 is a second spring, both ends of the mounting sleeve 22 are provided with retaining rings 222. One end of one of the second springs is in contact with one of the retaining rings 222 but not fixedly connected, and the other end of one of the second springs is in contact with one side of the electronic compass body 1 but not fixedly connected. One end of the other second spring is in contact with the other retaining ring 222 but not fixedly connected, and the other end of the other second spring is in contact with the other side of the electronic compass body 1 but not fixedly connected. At the same time, at least one retaining ring 222 and the mounting sleeve 22 can be detached and disassembled through a detachable connection structure, which facilitates the disassembly and assembly of the anti-vibration electronic compass structure of this utility model.
[0024] The longitudinal elastic element 24 in this invention is not limited to using a first spring. In other embodiments, the longitudinal elastic element 24 may be a metal sheet, a silicone block, or other elastic objects.
[0025] It should be noted that when only one retaining ring 222 is detachably connected to the mounting sleeve 22 via a detachable connection structure, the other retaining ring 222 is integrally formed with the mounting sleeve 22. The detachable connection structure includes a slot 223 on the outer wall of the mounting sleeve 22 and a block 2221 on the inner wall of the retaining ring 222 that cooperates with the slot 223. The slot 223 has an L-shaped structure. The slot 223 and the block 2221 cooperate to facilitate the connection and disconnection between the retaining ring 222 and the mounting sleeve 22. At the same time, one end of the block 2221 is chamfered, which makes it easy to insert the block 2221 into the slot 223.
[0026] The vibration-resistant electronic compass structure of this utility model can absorb the lateral and longitudinal vibrations of the equipment during operation through the lateral elastic element 23 and the longitudinal elastic element 24. It has a good vibration reduction effect, avoids damage to the components on the electronic compass body 1 due to vibration, and improves its service life.
[0027] The specific embodiments of this utility model described above do not constitute a limitation on the scope of protection of this utility model. Any other corresponding changes and modifications made based on the technical concept of this utility model should be included within the scope of protection of the claims of this utility model.
Claims
1. A vibration resistant electronic compass structure, characterized by, The application relates to an electronic compass body (1) and four groups of damping components (2) respectively arranged at four corners of the electronic compass body (1), wherein each corner of the electronic compass body (1) is provided with a mounting hole (11), each group of the damping components (2) comprises an outer sleeve (21) arranged in the corresponding mounting hole (11), a mounting sleeve (22) is coaxially arranged in the outer sleeve (21), a plurality of transverse elastic elements (23) are arranged between the outer wall of the mounting sleeve (22) and the inner wall of the outer sleeve (21), and the two ends of the mounting sleeve (22) are connected with the electronic compass body (1) through longitudinal elastic elements (24).
2. The vibration-resistant electronic compass structure of claim 1, wherein, The transverse elastic element (23) is a first spring.
3. The vibration-resistant electronic compass structure of claim 2, wherein, The inner wall of the outer sleeve (21) is provided with a first fixing column (211), the outer wall of the mounting sleeve (22) is provided with a second fixing column (221), one end of the first spring is sleeved on the first fixing column (211) and is in contact with the inner wall of the outer sleeve (21) but is not fixedly connected, and the other end of the first spring is sleeved on the second fixing column (221) and is in contact with the outer wall of the mounting sleeve (22) but is not fixedly connected.
4. The vibration-resistant electronic compass structure of claim 1, wherein, The longitudinal elastic element (24) comprises two second springs which are respectively sleeved on the two ends of the mounting sleeve (22).
5. The vibration-resistant electronic compass structure of claim 4, wherein, The two ends of the mounting sleeve (22) are provided with two stop rings (222), one end of one of the second springs is in contact with one of the stop rings (222) but is not fixedly connected, one end of the other second spring is in contact with the other stop ring (222) but is not fixedly connected, one end of the other second spring is in contact with one side of the electronic compass body (1) but is not fixedly connected, and the other end of the other second spring is in contact with the other side of the electronic compass body (1) but is not fixedly connected.
6. The vibration-resistant electronic compass structure of claim 5, wherein, At least one of the stop rings (222) and the mounting sleeve (22) are detachably connected through a detachable connecting structure.
7. The vibration-resistant electronic compass structure of claim 6, wherein, The detachable connecting structure comprises a clamping groove (223) arranged on the outer wall of the mounting sleeve (22) and a clamping block (2221) arranged on the inner wall of the stop ring (222) and matched with the clamping groove (223).
8. The vibration-resistant electronic compass structure of claim 7, wherein, The clamping groove (223) is in L-shaped structure.