CN212587703U - Anti-vibration's marine satellite antenna base - Google Patents
Anti-vibration's marine satellite antenna base Download PDFInfo
- Publication number
- CN212587703U CN212587703U CN201922433866.2U CN201922433866U CN212587703U CN 212587703 U CN212587703 U CN 212587703U CN 201922433866 U CN201922433866 U CN 201922433866U CN 212587703 U CN212587703 U CN 212587703U
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- Prior art keywords
- satellite antenna
- mounting panel
- plate
- vibration
- marine satellite
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- Expired - Fee Related
Links
- 230000035939 shock Effects 0.000 claims description 12
- 238000013016 damping Methods 0.000 claims description 7
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims description 5
- 235000017491 Bambusa tulda Nutrition 0.000 claims description 5
- 241001330002 Bambuseae Species 0.000 claims description 5
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims description 5
- 239000011425 bamboo Substances 0.000 claims description 5
- 238000009434 installation Methods 0.000 description 9
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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- Vibration Prevention Devices (AREA)
Abstract
The utility model provides a marine satellite antenna base of anti-vibration, including the base main part, crisscross a plurality of damper on the infrabasal plate of base main part, it is a plurality of damper all includes mounting panel and last mounting panel down, and is a plurality of both sides all are equipped with the fixed plate, and are a plurality of down the mounting panel all be equipped with the movable plate directly over the lower mounting panel, and are a plurality of the bottom of going up the mounting panel is all crisscross a plurality of second elasticity posts, and is a plurality of the second spring has all been cup jointed on the outer wall of second elasticity post, the backup pad is installed on the top of rubber slab, hollow post is installed to the top center department of backup pad, install first elasticity post perpendicularly in the cavity of hollow post, cup jointed first spring on the outer wall of first elasticity post. The utility model discloses a damper assembly, first elasticity post and first spring, the effectual vibrations that have alleviated satellite antenna and received have alleviateed the influence of vibrations to satellite antenna.
Description
Technical Field
The utility model mainly relates to a marine satellite antenna base technical field specifically is an anti-vibration's marine satellite antenna base.
Background
When the ship sails, the ship-used satellite antenna is extremely easy to shake due to swinging of the ship, and a base of the ship-used satellite antenna mostly does not have a shockproof structure, so that the ship-used satellite antenna can interfere with receiving and sending of signals when shaking is caused, the ship-used satellite antenna is in a shaking environment for a long time, parts inside the ship-used satellite antenna can be damaged, the ship-used satellite antenna can receive and send signals, and the ship-used satellite antenna is scrapped even when being serious. Therefore, there is a need to develop a vibration-proof base of a marine satellite antenna to reduce the influence of vibration on the marine satellite antenna.
SUMMERY OF THE UTILITY MODEL
The utility model mainly provides a marine satellite antenna base of anti-vibration for solve the technical problem who proposes among the above-mentioned background art.
The utility model provides a technical scheme that above-mentioned technical problem adopted does:
an anti-vibration marine satellite antenna base comprises a base body, wherein a plurality of shock absorption components are horizontally and fixedly installed on an inner bottom plate of the base body in a staggered mode, each shock absorption component comprises a lower installation plate and an upper installation plate, fixed plates are vertically installed on the front side and the rear side of each lower installation plate, the tops of the fixed plates are fixedly connected with the bottoms of the upper installation plates, sliding grooves are horizontally and symmetrically formed in the inner sides of the fixed plates, a movable plate is installed right above the lower installation plates, sliding blocks are horizontally and symmetrically installed on the front side and the rear side of each movable plate, each sliding block is slidably connected with each sliding groove, a plurality of second elastic columns are horizontally and symmetrically installed at the bottoms of the upper installation plates, second springs are sleeved on the outer walls of the second elastic columns, and the tops of the second springs are embedded in the bottoms of the upper installation plates, a plurality of damping springs are horizontally and alternately arranged between the tops of the lower mounting plates and the bottoms of the moving plates;
it is a plurality of fixed mounting has the rubber slab directly over the lower mounting panel, the backup pad is installed through the bolt in the top of rubber slab, the hollow post is installed perpendicularly to the top center department of backup pad, install first elasticity post perpendicularly in the cavity of hollow post, cup jointed first spring on the outer wall of first elasticity post, just spacing section of thick bamboo is installed on the top of first elasticity post.
Furthermore, the connecting plate is installed on the top of spacing section of thick bamboo, the top of connecting plate is connected with the shock pad through sticky bonding.
Furthermore, the top of connecting plate passes through bolt fixed mounting has the antenna mount pad, just the top center department of antenna mount pad is equipped with the mounting groove perpendicularly.
Furthermore, a plurality of rubber pads are horizontally and alternately bonded to the tops of the upper mounting plates.
Furthermore, the bottom of the first elastic column is fixedly connected with the top of the supporting plate through a bolt, and the bottom of the first spring is embedded in the top of the supporting plate.
Further, the bottom of base main part is close to outer edgewise and rotates through the pivot equidistance and is connected with a plurality of folding bracing pieces, and is a plurality of folding bracing piece is kept away from the one end bottom of base main part all installs the supporting legs perpendicularly through the pivot.
Compared with the prior art, the beneficial effects of the utility model are that:
one of the two main bodies is provided with a damping spring, the damping spring is used for buffering and absorbing partial impact force, the sliding connection between the sliding block and the sliding groove drives the movable plate to move upwards, the second spring and the second elastic column are extruded when the movable plate moves upwards, partial impact force is absorbed through the second spring and the second elastic column, partial impact force is absorbed through the rubber plate, the impact force is continuously transmitted, the vibration is reduced through the first elastic column and the first spring in sequence, the vibration received by the satellite antenna is relieved, and when the vibration disappears, the movable plate is rebounded to the original position through the second spring and the second elastic column, so that the vibration received by the satellite antenna is effectively relieved;
and secondly, the utility model discloses a base main part is supported to a plurality of folding bracing pieces and supporting legs, and firm base main part prevents that base main part from removing because vibrations, and then influences satellite antenna receiving and transmitting signal.
The present invention will be explained in detail with reference to the drawings and specific embodiments.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the hollow column structure of the present invention;
FIG. 3 is a schematic structural view of the shock absorbing assembly of the present invention;
fig. 4 is an enlarged view of a region a in fig. 3.
Reference numerals: 1. a base body; 11. folding the support rod; 12. supporting legs; 13. a support plate; 14. a rubber plate; 2. a hollow column; 21. a limiting cylinder; 22. a first elastic column; 23. a first spring; 24. a connecting plate; 241. a shock pad; 3. an antenna mounting base; 31. mounting grooves; 4. a shock absorbing assembly; 41. a lower mounting plate; 42. a fixing plate; 421. a chute; 43. a damping spring; 44. moving the plate; 441. a slider; 45. a second spring; 46. a second elastic column; 47. an upper mounting plate; 471. and (7) a rubber pad.
Detailed Description
In order to facilitate understanding of the present invention, the present invention will be described more fully with reference to the accompanying drawings, in which several embodiments of the present invention are shown, but the present invention can be implemented in different forms, and is not limited to the embodiments described in the text, but rather, these embodiments are provided to make the disclosure of the present invention more thorough and comprehensive.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may be present, and when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present, as the terms "vertical", "horizontal", "left", "right" and the like are used herein for descriptive purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs, and the use of the term knowledge in the specification of the present invention is for the purpose of describing particular embodiments and is not intended to limit the present invention, and the term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.
Please refer to fig. 1-4, which illustrate an anti-vibration marine satellite antenna base, including a base main body 1, a plurality of shock absorbing assemblies 4 are horizontally and fixedly installed on an inner bottom plate of the base main body 1 in a staggered manner, each of the plurality of shock absorbing assemblies 4 includes a lower mounting plate 41 and an upper mounting plate 47, fixing plates 42 are vertically installed on front and rear sides of the plurality of lower mounting plates 41, tops of the plurality of fixing plates 42 are fixedly connected with bottoms of the plurality of upper mounting plates 47, sliding grooves 421 are horizontally and symmetrically installed on inner sides of the plurality of fixing plates 42, moving plates 44 are installed right above the plurality of lower mounting plates 41, sliding blocks 441 are horizontally and symmetrically installed on front and rear sides of the plurality of moving plates 44, each sliding block 441 is slidably connected with each sliding groove 421, and a plurality of second elastic columns 46 are horizontally and staggeredly installed on bottoms of the plurality of upper mounting plates 47, it is a plurality of all cup jointed second spring 45 on the outer wall of second elasticity post 46, it is a plurality of the top of second spring 45 is all embedded in a plurality of go up the bottom of mounting panel 47, and it is a plurality of the top of mounting panel 41 is with a plurality of down equal level is crisscross installs a plurality of damping spring 43 between the bottom of movable plate 44, and is a plurality of fixed mounting has rubber slab 14 directly over lower mounting panel 41, backup pad 13 is installed through the bolt in the top of rubber slab 14, hollow post 2 is installed perpendicularly to the top center department of backup pad 13, install first elasticity post 22 perpendicularly in the cavity of hollow post 2, cup jointed first spring 23 on the outer wall of first elasticity post 22, just spacing section of thick bamboo 21 is installed on the top of first elasticity post 22.
Please refer to fig. 1 again, the antenna mounting base 3 is fixedly mounted at the top end of the connecting plate 24 through a bolt, and a mounting groove 31 is vertically arranged at the center of the top end of the antenna mounting base 3. In the present embodiment, the satellite antenna is mounted through the mounting groove 31 of the antenna mounting base 3.
Please refer to fig. 1 again, the bottom end of the base main body 1 is connected to a plurality of folding support rods 11 through rotating shafts at equal intervals near the outer edge, and the bottoms of the ends of the folding support rods 11 far away from the base main body 1 are vertically provided with support legs 12 through rotating shafts. In this embodiment, the base body 1 is supported by the plurality of folding support rods 11 and the support legs 12, so as to stabilize the base body 1, thereby preventing the base body 1 from moving due to vibration and further affecting the satellite antenna transmission and reception.
Please refer to fig. 2-3 again, the bottom of the first elastic column 22 is fixedly connected to the top of the supporting plate 13 through a bolt, the bottom of the first spring 23 is embedded in the top of the supporting plate 13, a connecting plate 24 is installed at the top end of the limiting cylinder 21, and the top end of the connecting plate 24 is connected to a shock pad 241 through adhesive bonding. In this embodiment, the shock absorbing effect of the device is improved by the shock absorbing pad 241 and the rubber pad 471.
The utility model discloses a concrete operation as follows:
firstly, a satellite antenna is installed through an installation groove 31 of an antenna installation seat 3, then a base main body 1 is supported through a plurality of folding support rods 11 and support legs 12, the base main body 1 is stabilized, when the device is vibrated, the bottom of the base main body 1 is impacted, partial impact force is absorbed through a damping spring 43, then the sliding connection between a sliding block 441 and a sliding groove 421 is realized, a moving plate 44 is driven to move upwards, the moving plate 44 extrudes a second spring 45 and a second elastic column 46 when moving upwards, partial impact force is absorbed through the second spring 45 and the second elastic column 46, partial impact force is absorbed through a rubber plate 14, the impact force is continuously transmitted, the vibration is reduced through a first elastic column 22 and a first spring 23 in sequence, the vibration borne by the satellite antenna is relieved, when the vibration disappears, the moving plate 44 rebounds to the original position through the second spring 45 and the second elastic column 46, the vibration suffered by the satellite antenna is effectively relieved.
The present invention has been described above with reference to the accompanying drawings, and it is obvious that the present invention is not limited by the above-mentioned manner, if the method and the technical solution of the present invention are adopted, the present invention can be directly applied to other occasions without substantial improvement, and the present invention is within the protection scope of the present invention.
Claims (6)
1. The utility model provides a marine satellite antenna base of vibrations, includes base main part (1), its characterized in that: the interior bottom plate of base main part (1) is gone up the crisscross fixed mounting of level and is had a plurality of damper (4), and is a plurality of damper (4) all include lower mounting panel (41) and last mounting panel (47), and is a plurality of fixed plate (42) are all installed perpendicularly to both sides around lower mounting panel (41), and are a plurality of the top of fixed plate (42) all with a plurality of go up the bottom fixed connection of mounting panel (47), it is a plurality of the equal horizontal symmetry in inboard of fixed plate (42) is equipped with spout (421), and is a plurality of all install movable plate (44) directly over lower mounting panel (41), and is a plurality of slider (441) are installed to the equal horizontal symmetry in both sides around movable plate (44), every slider (441) all with every spout (421) sliding connection, and a plurality of the equal horizontal crisscross in bottom of going up mounting panel (47) installs a plurality of second elastic columns (46), second springs (45) are sleeved on the outer walls of the second elastic columns (46), the top ends of the second springs (45) are embedded into the bottoms of the upper mounting plates (47), and a plurality of damping springs (43) are horizontally installed between the tops of the lower mounting plates (41) and the bottoms of the moving plates (44) in a staggered mode;
it is a plurality of fixed mounting has rubber slab (14) under mounting panel (41), backup pad (13) are installed through the bolt in the top of rubber slab (14), the top center department of backup pad (13) installs hollow post (2) perpendicularly, install first elasticity post (22) perpendicularly in the cavity of hollow post (2), first spring (23) have been cup jointed on the outer wall of first elasticity post (22), just spacing section of thick bamboo (21) are installed on the top of first elasticity post (22).
2. The anti-vibration marine satellite antenna mount as claimed in claim 1, wherein: connecting plate (24) are installed on the top of spacing section of thick bamboo (21), the top of connecting plate (24) is connected with shock pad (241) through sticky bonding.
3. The anti-vibration marine satellite antenna mount as claimed in claim 2, wherein: the top of connecting plate (24) passes through bolt fixed mounting has antenna mount pad (3), just the top center department of antenna mount pad (3) is equipped with mounting groove (31) perpendicularly.
4. The anti-vibration marine satellite antenna mount as claimed in claim 1, wherein: the tops of the upper mounting plates (47) are horizontally and alternately bonded with a plurality of rubber pads (471).
5. The anti-vibration marine satellite antenna mount as claimed in claim 1, wherein: the bottom of the first elastic column (22) is fixedly connected with the top of the support plate (13) through a bolt, and the bottom of the first spring (23) is embedded in the top of the support plate (13).
6. The anti-vibration marine satellite antenna mount as claimed in claim 1, wherein: the bottom of base main part (1) is close to outer edgewise and rotates through pivot equidistance and is connected with a plurality of folding bracing pieces (11), and is a plurality of folding bracing piece (11) are kept away from the supporting legs (12) are all installed perpendicularly through the pivot in the one end bottom of base main part (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922433866.2U CN212587703U (en) | 2019-12-30 | 2019-12-30 | Anti-vibration's marine satellite antenna base |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922433866.2U CN212587703U (en) | 2019-12-30 | 2019-12-30 | Anti-vibration's marine satellite antenna base |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212587703U true CN212587703U (en) | 2021-02-23 |
Family
ID=74655104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922433866.2U Expired - Fee Related CN212587703U (en) | 2019-12-30 | 2019-12-30 | Anti-vibration's marine satellite antenna base |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212587703U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116030674A (en) * | 2022-11-23 | 2023-04-28 | 浙江大学 | Six degrees of freedom anti-seasickness simulation trainer |
-
2019
- 2019-12-30 CN CN201922433866.2U patent/CN212587703U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116030674A (en) * | 2022-11-23 | 2023-04-28 | 浙江大学 | Six degrees of freedom anti-seasickness simulation trainer |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210223 Termination date: 20211230 |