CN112928422A - Mounting bracket for satellite communication - Google Patents
Mounting bracket for satellite communication Download PDFInfo
- Publication number
- CN112928422A CN112928422A CN202110094602.8A CN202110094602A CN112928422A CN 112928422 A CN112928422 A CN 112928422A CN 202110094602 A CN202110094602 A CN 202110094602A CN 112928422 A CN112928422 A CN 112928422A
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- China
- Prior art keywords
- plate
- shaped base
- satellite communication
- mounting bracket
- rubber
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/005—Damping of vibrations; Means for reducing wind-induced forces
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/20—Resilient mountings
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- Vibration Prevention Devices (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
Abstract
The invention discloses a mounting bracket for satellite communication, which relates to the technical field of satellite communication equipment, and adopts the technical scheme that the mounting bracket comprises a ground layer, a bottom plate is arranged on the ground layer, a drum sheet is arranged at the top of the bottom plate, a top plate is arranged at the top end of the drum sheet, the drum sheet is arranged between the bottom plate and the top plate in an arc shape, the bottom plate, the drum sheet and the top plate form a wind collecting structure, a balancing weight is arranged in the middle of the wind collecting structure, a gap is left between the balancing weight and the wind collecting structure, a fixing ring is arranged on one side of the fixing ring in a hinged mode, a damping rod A is arranged on the fixing ring and is positioned on the side opposite to the electric pushing rod, pull rods are arranged on the sides of the electric pushing rod opposite to the damping rod A, and the other ends of the pull rods are arranged on the balancing weight, the swing degree of the satellite receiving antenna is reduced.
Description
Technical Field
The invention relates to the technical field of satellite communication equipment, in particular to a mounting bracket for satellite communication.
Background
A satellite is a natural celestial body that periodically orbits in a closed orbit around a planet, and a satellite is also commonly referred to as a satellite.
Satellite communication is simply communication between radio communication stations on earth using a satellite as a relay. The satellite communication system is composed of a satellite and an earth station, a receiving antenna for receiving satellite signals, which is a pan commonly called as a metal paraboloid, collects weak signals transmitted by the satellite and removes noise as much as possible, the satellite signals are reflected by the parabolic antenna and then are concentrated to a focus of the satellite signals, and generally, the larger the aperture of the antenna is, the stronger the signals of programs are, and the higher the receiving quality is.
Nowadays, with the technical development of satellite communication, the field of satellite application is wider and wider, for example, vehicle-mounted navigation or marine vessels, and the like are closely related to the transmission of satellite signals, and with the construction and popularization of satellite base stations, people enjoy more and more convenience brought by satellites and bring new problems.
Disclosure of Invention
In order to solve the problems in the prior art, the invention aims to provide an installation support for satellite communication, which has the advantages of reducing the side wind resistance, reducing the influence of wind pressure on a satellite receiving antenna, slowing down the vibration sense, improving the anti-seismic effect and reducing the swing degree of the satellite receiving antenna.
In order to achieve the purpose, the invention provides the following technical scheme: a mounting bracket for satellite communication comprises a ground layer, wherein a bottom plate is mounted on the ground layer, a drum sheet is mounted at the top of the bottom plate, a top plate is mounted at the top end of the drum sheet, the drum sheet is installed between the bottom plate and the top plate in an arc shape, the bottom plate, the drum sheet and the top plate form a wind collecting structure, a balancing weight is mounted in the middle of the wind collecting structure, a gap is reserved between the balancing weight and the wind collecting structure, a fixing ring is mounted on one side of the fixing ring in a hinged mode, a damping rod A is mounted on the fixing ring and located on the side opposite to the electric push rod, a pull rod is arranged on one side of the electric push rod opposite to the damping rod A, the other end of the pull rod is mounted on the balancing weight, a damping rod B is mounted at the top of the balancing weight and along the front-back direction, and, and the electric push rod is hinged with the top of the damping rod A and is provided with a connecting ring, and the connecting ring is fixedly connected with the satellite receiving antenna.
As a further scheme of the invention: the top of bottom plate and the bottom of roof correspond installs the bearing, the both ends of drum piece are installed on the bearing and with bearing rotation connection.
As a still further scheme of the invention: the bottom of balancing weight is provided with the U-shaped base, the U-shaped base is half enclosed, and the balancing weight is installed in the inside of U-shaped base, gu fixed ring installs at the top of U-shaped base to be located between U-shaped base and the balancing weight, the lateral wall annular array of U-shaped base is provided with the curb plate, the curb plate slope is installed on the lateral wall of U-shaped base.
As a still further scheme of the invention: the bottom of U-shaped base is provided with the slide, and the bottom of U-shaped base corresponds with the top of slide and has seted up the spout, the spout sets up to the ring form, is provided with a plurality of balls on the spout, and U-shaped base passes through ball sliding connection with the slide, U-shaped base and slide all are located the inside of receipts wind structure.
As a still further scheme of the invention: the bottom fixed mounting of bottom plate has the bedplate, the rubber slab protective layer is installed to the bottom of bedplate, the bedplate is down installed to the other end of rubber slab protective layer, the surface mounting of rubber slab protective layer has the pneumatic valve, go up the bedplate and articulate between the bedplate down and install a plurality of damping rod C, it is a plurality of damping rod C installs the both sides at the rubber slab protective layer, damping rod C's outside is provided with spring, and damping rod C is located spring's inside, and spring's both ends are fixed mounting respectively on last bedplate and bedplate down.
As a still further scheme of the invention: the utility model discloses a shock insulation rubber, including rubber slab protective layer, top layer, air chamber, air flue, lead core, rubber slab protective layer's inside is provided with to be filled has shock insulation rubber, shock insulation rubber's inside is provided with a plurality of metal sheets, top layer along vertical direction be provided with a plurality of air chambers between the metal sheet, and is a plurality of be provided with between the air chamber and connect the air flue, shock insulation rubber's internally mounted has a plurality of lead cores, and is a.
As a still further scheme of the invention: and a wind sensor is arranged in the center of the top of the balancing weight.
Compared with the prior art, the invention has the beneficial effects that:
1. according to the scheme, the bottom plate, the drum pieces and the top plate arranged on the ground layer form a wind collecting structure, when the wind speed is increased, the drum pieces collect wind, the drum pieces are installed between the bottom plate and the top plate in an arc shape, a small gap is left between the drum pieces, when the wind passes through the wind collecting structure, a narrow pipe effect is formed, the wind blows into the wind collecting structure to push the U-shaped base to rotate, when the wind laterally enters the wind, the U-shaped base is pushed to rotate through the wind, the arc surface or the back surface of the satellite receiving antenna faces the incoming direction of the wind, so that the lateral wind resistance is reduced, then the satellite receiving antenna is adjusted to be at a lower height through adjusting the electric push rod, and then the satellite receiving antenna is placed horizontally, so that the influence of the wind pressure on the satellite receiving antenna is effectively reduced.
2. According to the invention, the upper base plate is fixedly arranged at the bottom of the bottom plate, when an earthquake occurs, the shock insulation rubber in the rubber plate protective layer absorbs the energy of the shock, because the earthquake can generate horizontal inertia, the metal plates in the shock insulation rubber play a role of positioning a center line, the satellite receiving antenna is guided to a neutral position, the horizontal acting force is effectively absorbed, the damage is reduced, a plurality of lead cores are arranged in the shock insulation rubber, the metal plates are reinforced and stabilized, and a plurality of air chambers are arranged between the metal plates at the top layer, so that the shock buffering and resisting functions are further achieved, the shock feeling is relieved, the shock resisting effect is improved, and the swing degree of the satellite receiving antenna is reduced.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of an exploded structure of a wind collecting structure and a counterweight block according to the present invention;
FIG. 3 is a schematic cross-sectional view of the wind collecting structure and the counterweight block of the present invention;
FIG. 4 is an exploded view of the upper seat plate, the shock-insulation rubber and the lower seat plate of the present invention;
fig. 5 is an enlarged detail view of a portion a in fig. 3 according to the present invention.
In the figure: 1. a ground layer; 2. a base plate; 3. a drum sheet; 4. a top plate; 5. a balancing weight; 501. a U-shaped base; 502. a side plate; 503. a slide plate; 504. a chute; 505. a ball bearing; 6. a fixing ring; 7. an electric push rod; 701. a damping rod A; 8. a pull rod; 9. a damping rod B; 10. a connecting ring; 11. an upper seat plate; 12. A rubber sheet protective layer; 121. shock insulation rubber; 122. a metal plate; 123. an air chamber; 124. connecting an air passage; 125. a lead core; 13. a lower seat plate; 14. an air valve; 15. a damping lever C; 16. an elastic spring; 17. A wind sensor.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
Referring to fig. 1 to 5, in an embodiment of the present invention, an installation bracket for satellite communication includes a ground layer 1, a bottom plate 2 is installed on the ground layer 1, a drum 3 is installed on the top of the bottom plate 2, a top plate 4 is installed on the top end of the drum 3, the drum 3 is installed between the bottom plate 2 and the top plate 4 in an arc shape, the bottom plate 2, the drum 3 and the top plate 4 form a wind collecting structure, a balancing weight 5 is installed in the middle of the wind collecting structure, a gap is left between the balancing weight 5 and the wind collecting structure and a fixing ring 6 is installed, an electric push rod 7 is installed on one side of the fixing ring 6 in a hinged manner, a damping rod a701 is installed on one side of the fixing ring 6 opposite to the electric push rod 7, pull rods 8 are installed on both sides of the electric push rod 7 opposite to the damping rod a701, the other end of the pull rod 8 is installed on the balancing weight 5, a damping rod B9, the other end of the damping rod B9 is fixedly connected with the side edge of the satellite receiving antenna, the electric push rod 7 is hinged with the top of the damping rod A701 and is provided with a connecting ring 10, and the connecting ring 10 is fixedly connected with the satellite receiving antenna.
In fig. 3, bearings are mounted on the top of the bottom plate 2 and the bottom of the top plate 4, and two ends of the drum 3 are mounted on the bearings and rotatably connected with the bearings.
In fig. 3, the bottom of balancing weight 5 is provided with U-shaped base 501, U-shaped base 501 is half enclosed, and balancing weight 5 is installed in the inside of U-shaped base 501, gu fixed ring 6 installs at the top of U-shaped base 501 to be located between U-shaped base 501 and balancing weight 5, the annular array of lateral wall of U-shaped base 501 is provided with curb plate 502, curb plate 502 slope is installed on the lateral wall of U-shaped base 501.
In fig. 3, a sliding plate 503 is arranged at the bottom of a U-shaped base 501, a sliding groove 504 is arranged at the bottom of the U-shaped base 501 corresponding to the top of the sliding plate 503, the sliding groove 504 is annular, a plurality of balls 505 are arranged on the sliding groove 504, the U-shaped base 501 and the sliding plate 503 are slidably connected through the balls 505, the U-shaped base 501 and the sliding plate 503 are both located inside a wind-receiving structure, the wind-receiving structure is formed by a bottom plate 2, a drum 3 and a top plate 4 which are arranged on a ground layer 1, when the wind speed is high, the drum 3 receives wind, because the drum 3 is arc-shaped and arranged between the bottom plate 2 and the top plate 4, a small gap is left between the drum 3 and the drum 3, when the wind passes through, a narrow pipe effect is formed, the wind blows into the wind-receiving structure to push the U-shaped base 501 to rotate, when the wind comes from side, the U-shaped base 501 is pushed to rotate by wind force, so that the, the side wind resistance is reduced, then the satellite receiving antenna is adjusted to be at a lower height by adjusting the electric push rod 7, and then the satellite receiving antenna is put flat, so that the influence of wind pressure on the satellite receiving antenna is effectively reduced.
In fig. 3, the bottom fixed mounting of bottom plate 2 has upper seat plate 11, rubber slab protective layer 12 is installed to upper seat plate 11's bottom, bedplate 13 down is installed to the other end of rubber slab protective layer 12, the surface mounting of rubber slab protective layer 12 has pneumatic valve 14, it installs a plurality of damping rods C15, a plurality of to go up articulated between bedplate 11 and the bedplate 13 down damping rods C15 and install the both sides at rubber slab protective layer 12, damping rods C15's outside is provided with spring 16, and damping rods C15 is located spring 16's inside, and spring 16's both ends are fixed mounting respectively on upper seat plate 11 and bedplate 13 down, and bottom plate 2 extends to the below of ground floor 1, passes through pre-buried muscle fixed connection with upper seat plate 11.
In fig. 4, the rubber sheet protection layer 12 is internally filled with vibration isolation rubber 121, the vibration isolation rubber 121 is internally provided with a plurality of metal sheets 122 along the vertical direction, a plurality of air chambers 123 are arranged between the metal sheets 122 at the top layer, a plurality of connecting air passages 124 are arranged between the air chambers 123, a plurality of lead cores 125 are arranged inside the vibration isolation rubber 121, the lead cores 125 penetrate through the metal sheets 122 and are fixedly arranged between the upper seat plate 11 and the lower seat plate 13, the upper seat plate 11 is fixedly arranged at the bottom of the bottom plate 2, when an earthquake occurs, the vibration isolation rubber 121 inside the rubber sheet protection layer 12 absorbs the energy of the vibration, because the earthquake can generate horizontal inertia, the metal sheets 122 inside the vibration isolation rubber 121 play a role of positioning a central line, guide the satellite receiving antenna to a neutral position, effectively absorb horizontal acting force to reduce damage, and the plurality of lead cores 125 are arranged inside the vibration isolation rubber 121, the metal sheet 122 is stabilized in the reinforcement to set up a plurality of air chambers 123 between the metal sheet 122 at the top layer, further reach the antidetonation function of buffering, slow down the sense of earthquake, promote the antidetonation effect, reduce satellite receiving antenna's the degree of swaying.
In fig. 2, a wind sensor 17 is installed at the center of the top of the counterweight 5, the wind sensor 17 is electrically connected with the electric push rod 7, and when the wind force sensed by the wind sensor 17 reaches a certain level, the wind sensor 17 gives an instruction to automatically lower the electric push rod 7 and level the satellite receiving antenna.
The working principle of the invention is as follows: the bottom plate 2, the drum piece 3 and the top plate 4 arranged on the ground layer 1 form a wind collecting structure, when the wind speed is increased, the drum piece 3 collects wind, as the drum piece 3 is installed between the bottom plate 2 and the top plate 4 in an arc shape, a small gap is left between the drum piece 3 and the drum piece 3, when the wind passes through, a narrow tube effect is formed, the wind blows into the interior of the wind collecting structure to push the U-shaped base 501 to rotate, when the wind laterally moves towards, the U-shaped base 501 is pushed to rotate by the wind, the arc surface or the back surface of the satellite receiving antenna faces the incoming direction of the wind so as to reduce the lateral wind resistance, then the satellite receiving antenna is adjusted to be in a lower height by adjusting the electric push rod 7 and then is flatly placed, the influence of the wind pressure on the satellite receiving antenna is effectively reduced, the upper seat plate 11 is fixedly installed at the bottom of the bottom plate 2, and when an earthquake occurs, the shock insulation rubber 121 in the interior of the rubber, absorb the energy of vibrations, because the earthquake can produce horizontally inertia, the metal sheet 122 of the inside of shock insulation rubber 121, play the effect of location central line, guide satellite receiving antenna to neutral position, the horizontal effort of effective absorption reduces and damages, at a plurality of lead cores 125 of the internally mounted of shock insulation rubber 121, metal sheet 122 is stabilized in the reinforcement, and set up a plurality of air chambers 123 between the metal sheet 122 at the top layer, further reach the shock-resistant function of buffering, slow down the sense of earthquake, promote the antidetonation effect, reduce satellite receiving antenna's the degree of swaying.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention are equivalent to or changed within the technical scope of the present invention.
Claims (7)
1. The utility model provides a satellite communication is with installing support, includes ground layer (1), its characterized in that: the floor is characterized in that a bottom plate (2) is installed on a ground layer (1), a drum piece (3) is installed at the top of the bottom plate (2), a top plate (4) is installed at the top end of the drum piece (3), the drum piece (3) is installed between the bottom plate (2) and the top plate (4) in an arc shape, the bottom plate (2), the drum piece (3) and the top plate (4) form a wind collecting structure, a balancing weight (5) is installed in the middle of the wind collecting structure, a gap is left between the balancing weight (5) and the wind collecting structure, a fixing ring (6) is installed, an electric push rod (7) is installed on one side of the fixing ring (6) opposite to the electric push rod (7) in a hinged mode, a damping rod A (701) is installed on the fixing ring (6) and located on one side of the electric push rod (7) opposite to the damping rod A (701), pull rods (8) are arranged on one side, the top of balancing weight (5) and install damping rod B (9) along the fore-and-aft direction, the other end of damping rod B (9) and satellite receiving antenna's side fixed connection, electric putter (7) are articulated with the top of damping rod A (701) and are installed go-between (10), go-between (10) and satellite receiving antenna fixed connection.
2. The mounting bracket for satellite communication according to claim 1, wherein the top of the bottom plate (2) and the bottom of the top plate (4) are correspondingly provided with bearings, and two ends of the drum sheet (3) are arranged on the bearings and are rotatably connected with the bearings.
3. The mounting bracket for satellite communication according to claim 1, wherein the bottom of the weight block (5) is provided with a U-shaped base (501), the U-shaped base (501) is in a semi-enclosed type, the weight block (5) is mounted inside the U-shaped base (501), the fixing ring (6) is mounted on the top of the U-shaped base (501) and located between the U-shaped base (501) and the weight block (5), the side wall annular array of the U-shaped base (501) is provided with side plates (502), and the side plates (502) are obliquely mounted on the side walls of the U-shaped base (501).
4. The mounting bracket for satellite communication according to claim 4, wherein a sliding plate (503) is arranged at the bottom of the U-shaped base (501), a sliding groove (504) is formed in the bottom of the U-shaped base (501) and the top of the sliding plate (503) correspondingly, the sliding groove (504) is annular, a plurality of balls (505) are arranged on the sliding groove (504), the U-shaped base (501) and the sliding plate (503) are connected in a sliding mode through the balls (505), and the U-shaped base (501) and the sliding plate (503) are located inside the wind collecting structure.
5. The mounting bracket for satellite communication according to claim 1, wherein the bottom of the bottom plate (2) is fixedly provided with an upper seat plate (11), a rubber plate protective layer (12) is arranged at the bottom of the upper seat plate (11), a lower seat plate (13) is arranged at the other end of the rubber plate protective layer (12), an air valve (14) is arranged on the surface of the rubber plate protective layer (12), a plurality of damping rods C (15) are hinged between the upper seat plate (11) and the lower seat plate (13), the damping rods C (15) are arranged on two sides of the rubber plate protective layer (12), an elastic spring (16) is arranged outside the damping rod C (15), the damping rod C (15) is located inside the elastic spring (16), and two ends of the elastic spring (16) are fixedly mounted on the upper seat plate (11) and the lower seat plate (13) respectively.
6. The mounting bracket for satellite communication according to claim 6, wherein the rubber sheet protection layer (12) is filled with vibration isolation rubber (121), the vibration isolation rubber (121) is internally provided with a plurality of metal sheets (122) along a vertical direction, a plurality of air chambers (123) are arranged between the metal sheets (122) at the top layer, a connecting air passage (124) is arranged between the plurality of air chambers (123), a plurality of lead cores (125) are arranged inside the vibration isolation rubber (121), and the plurality of lead cores (125) penetrate through the metal sheets (122) and are fixedly arranged between the upper seat plate (11) and the lower seat plate (13).
7. The mounting bracket for satellite communication according to claim 1, wherein the top center of the counterweight block (5) is provided with a wind sensor (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110094602.8A CN112928422B (en) | 2021-01-25 | 2021-01-25 | Mounting bracket for satellite communication |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110094602.8A CN112928422B (en) | 2021-01-25 | 2021-01-25 | Mounting bracket for satellite communication |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112928422A true CN112928422A (en) | 2021-06-08 |
| CN112928422B CN112928422B (en) | 2023-07-07 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110094602.8A Active CN112928422B (en) | 2021-01-25 | 2021-01-25 | Mounting bracket for satellite communication |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112928422B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3546704A (en) * | 1966-07-29 | 1970-12-08 | Plessey Co Ltd | Satellite tracking dish antenna with course and fine driving mechanism |
| CN2126936Y (en) * | 1992-06-10 | 1993-02-10 | 烟台开发区意埃伊股份有限公司 | Horizontal antenna |
| CN2854837Y (en) * | 2005-08-04 | 2007-01-03 | 孟光盈 | Disk electric slide satellite antenna |
| CN206758632U (en) * | 2017-05-24 | 2017-12-15 | 张智博 | satellite antenna fixed structure |
| CN110683007A (en) * | 2019-10-21 | 2020-01-14 | 江苏憬知梦蓝科技有限公司 | Multi-redundancy offshore floating type laser radar wind measuring device |
| CN210838102U (en) * | 2019-12-25 | 2020-06-23 | 陈蕙 | Weather interference prevention broadcast television satellite equipment |
-
2021
- 2021-01-25 CN CN202110094602.8A patent/CN112928422B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3546704A (en) * | 1966-07-29 | 1970-12-08 | Plessey Co Ltd | Satellite tracking dish antenna with course and fine driving mechanism |
| CN2126936Y (en) * | 1992-06-10 | 1993-02-10 | 烟台开发区意埃伊股份有限公司 | Horizontal antenna |
| CN2854837Y (en) * | 2005-08-04 | 2007-01-03 | 孟光盈 | Disk electric slide satellite antenna |
| CN206758632U (en) * | 2017-05-24 | 2017-12-15 | 张智博 | satellite antenna fixed structure |
| CN110683007A (en) * | 2019-10-21 | 2020-01-14 | 江苏憬知梦蓝科技有限公司 | Multi-redundancy offshore floating type laser radar wind measuring device |
| CN210838102U (en) * | 2019-12-25 | 2020-06-23 | 陈蕙 | Weather interference prevention broadcast television satellite equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112928422B (en) | 2023-07-07 |
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| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information |
Inventor after: Chu Guimei Inventor after: Meng Qingkun Inventor before: Chu Guimei |
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| CB03 | Change of inventor or designer information | ||
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Effective date of registration: 20230612 Address after: 528200 room 1504, building 1, Jiabang Guojin center, No. 1 Shilong South Road, Guicheng Street, Nanhai District, Foshan City, Guangdong Province Applicant after: ZHONGYUETONG CONSTRUCTION TECHNOLOGY Co.,Ltd. Address before: 56 Nanfang Jiazhuang, Fengtai District, Beijing Applicant before: Chu Guimei |
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