CN220545008U - Communication transmission module experimental facility based on space satellite - Google Patents
Communication transmission module experimental facility based on space satellite Download PDFInfo
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- CN220545008U CN220545008U CN202322287391.7U CN202322287391U CN220545008U CN 220545008 U CN220545008 U CN 220545008U CN 202322287391 U CN202322287391 U CN 202322287391U CN 220545008 U CN220545008 U CN 220545008U
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- signal receiver
- satellite
- protective shell
- transmission module
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- 238000004891 communication Methods 0.000 title claims abstract description 40
- 230000005540 biological transmission Effects 0.000 title claims abstract description 18
- 230000001681 protective effect Effects 0.000 claims abstract description 31
- 230000017525 heat dissipation Effects 0.000 claims description 7
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 6
- 230000008054 signal transmission Effects 0.000 abstract description 6
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 6
- 235000017491 Bambusa tulda Nutrition 0.000 description 6
- 241001330002 Bambuseae Species 0.000 description 6
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 6
- 239000011425 bamboo Substances 0.000 description 6
- 238000010295 mobile communication Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 2
- 230000009975 flexible effect Effects 0.000 description 2
- 238000012806 monitoring device Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
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- Radio Relay Systems (AREA)
Abstract
The utility model relates to the technical field of satellite communication, in particular to communication transmission module experimental equipment based on a space-through satellite, which comprises a protective shell and a signal receiver, wherein an efficient amplifier is arranged in the protective shell, a signal converter is arranged in the protective shell, a satellite pan is arranged on the surface of the signal receiver, a plurality of groups of holes are formed in the surface of the satellite pan and close to one end of the signal receiver, a telescopic rod is arranged under the signal receiver, a limiting cylinder is arranged above the telescopic rod, a rotating roller is arranged above the telescopic rod, signals are transmitted to the signal converter through the arrangement of the signal receiver, a plurality of groups of holes are formed in the surface of the satellite pan and close to one end of the signal receiver, rainwater is prevented from accumulating in the satellite pan, and the effect of improving the signal transmission efficiency is achieved while damage caused by the signal receiver is prevented.
Description
Technical Field
The utility model belongs to the technical field of satellite communication, and particularly relates to communication transmission module experimental equipment based on a space satellite.
Background
Satellite communication technology is a communication between two or more earth stations that uses satellites as relay stations to forward radio waves.
Through searching, in the prior art, chinese patent application number: CN202221775340.8, filing date: 2022-07-11 discloses a satellite communication system, which comprises a plurality of satellite communication devices, a plurality of mobile communication base stations, a rainfall monitoring device and a satellite communication control console, wherein the satellite communication devices acquire data to be communicated in a preset satellite communication area, the mobile communication base stations realize communication data transmission between any two satellite communication devices, the rainfall monitoring device monitors rainfall information of the preset satellite communication area, and the satellite communication control console sends mobile communication control instructions to the satellite communication devices according to the rainfall information so that the satellite communication devices send the data to be communicated to target satellite communication devices based on the mobile communication base stations. According to the method and the device, rainfall information in the range of the preset satellite communication area is monitored, the data to be communicated are sent to other satellite communication equipment through the mobile communication base station for satellite communication transmission in the area with large rain attenuation, and the overall communication reliability in the range of the area is guaranteed.
The device still has the following drawbacks: although the device transmits satellite communication to other satellite communication devices through the mobile communication base station to ensure the overall communication reliability in the area, the data transmission efficiency of the device needs to be improved, and the device reduces the stability of communication.
Disclosure of Invention
Aiming at the problems, the utility model provides communication transmission module experimental equipment based on a space-time satellite, which comprises a protective shell and a signal receiver, wherein an efficient amplifier is arranged in the protective shell, a signal converter is arranged in the protective shell, and a satellite pot is arranged on the surface of the signal receiver;
the satellite dish is characterized in that a plurality of groups of holes are formed in the surface of the satellite dish and are close to one end of the signal receiver, a telescopic rod is arranged under the signal receiver, a mounting bottom plate is arranged at the bottom of the telescopic rod, a connecting block is arranged at the top of the telescopic rod, a limiting cylinder is arranged above the telescopic rod and is located at the top of the connecting block, and a rotating roller is arranged above the telescopic rod.
Further, the bottom of the protective shell is provided with a plurality of groups of fixed supporting legs, and the fixed supporting legs are arranged in a rectangular array with the central axis of the protective shell as the center.
Further, a plurality of groups of wiring through holes are connected to the two opposite side walls of the protective shell in a penetrating way, and the plurality of groups of wiring through holes are symmetrically arranged with the central axis of the protective shell as the center.
Further, a heat dissipation window is formed in the top of the protective shell, and the central axis of the heat dissipation window coincides with the central axis of the protective shell.
Further, the plurality of groups of holes are arranged in an annular array with the central axis of the signal receiver as the center, and the bottom of the signal receiver is provided with a fixed block.
Furthermore, two groups of fixed mounting holes are formed in the surface of the mounting bottom plate, and the two groups of fixed mounting holes are symmetrically arranged with the central axis of the mounting bottom plate as the center.
Further, the rotating roller is movably sleeved in the limiting cylinder, and the rotating roller is rotatably arranged by taking the central axis of the limiting cylinder as the center.
Further, the bottom of signal receiver is equipped with spacing joint piece, the surface of rotatory roller is equipped with spacing joint groove, spacing joint groove and spacing joint piece joint setting.
The beneficial effects of the utility model are as follows:
1. through signal receiver's setting, give signal transmission to signal converter, rethread high-efficient amplifier's setting can reach the purpose that improves satellite signal transmission efficiency, and a plurality of groups trompils have been seted up to the one end that just is close to signal receiver on the surface of rethread satellite pot, prevent that the rainwater from accumulating in the inside of satellite pot, have reached the effect that improves signal transmission efficiency again when preventing that signal receiver causes the damage.
2. The inside at spacing section of thick bamboo is cup jointed in the activity of rotatory roller, and the rethread rotatory roller rotates the setting as the center with the axis of spacing section of thick bamboo, and the staff of being convenient for adjusts signal receiver's angle, and the telescopic action of rethread telescopic link is convenient for the staff to signal receiver's height-adjusting, has reached the effect that improves equipment communication stability again when being convenient for adjust signal receiver.
Additional features and advantages of the utility model will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the utility model. The objectives and other advantages of the utility model may be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions of the prior art, the following description will briefly explain the drawings used in the embodiments or the description of the prior art, and it is obvious that the drawings in the following description are some embodiments of the present utility model, and other drawings can be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 shows a schematic diagram of a structure according to an embodiment of the present utility model;
FIG. 2 illustrates a cross-sectional view of a guard casing structure according to an embodiment of the present utility model;
FIG. 3 shows a schematic view of a telescopic rod structure according to an embodiment of the present utility model;
fig. 4 shows a schematic diagram of a signal receiver structure according to an embodiment of the utility model.
In the figure: 1. a protective housing; 2. a fixed support leg; 3. a wiring through hole; 4. a heat dissipation window; 5. an efficient amplifier; 6. a signal converter; 7. a mounting base plate; 8. fixing the mounting hole; 9. a telescopic rod; 10. a connecting block; 11. a limiting cylinder; 12. a rotating roller; 13. a limit clamping groove; 14. a satellite pan; 15. opening holes; 16. a signal receiver; 17. a fixed block; 18. and the limiting clamping block.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
The embodiment of the utility model provides communication transmission module experimental equipment based on a space-time satellite, which comprises a protective shell 1 and a signal receiver 16; as illustrated in fig. 1-4.
The bottom of the protective shell 1 is provided with a plurality of groups of fixed supporting legs 2, the plurality of groups of fixed supporting legs 2 are arranged in a rectangular array by taking the central axis of the protective shell 1 as the center, a plurality of groups of wiring through holes 3 are connected to the two opposite side walls of the protective shell 1 in a penetrating way, the plurality of groups of wiring through holes 3 are symmetrically arranged by taking the central axis of the protective shell 1 as the center, the top of the protective shell 1 is provided with a heat dissipation window 4, and the central axis of the heat dissipation window 4 coincides with the central axis of the protective shell 1;
the inside of protective housing 1 is equipped with high-efficient amplifier 5, the inside of protective housing 1 is equipped with signal converter 6, signal receiver 16's surface is equipped with satellite pot 14, a plurality of groups trompil 15 have been seted up to the surface of satellite pot 14 and the one end that is close to signal receiver 16, a plurality of groups trompil 15 are the annular array setting as the center with signal receiver 16's axis, signal receiver 16's bottom is equipped with fixed block 17, signal receiver 16's bottom is equipped with spacing joint piece 18.
Specifically, through the setting of the signal receiver 16, signals are transmitted to the signal converter 6, and then through the setting of the high-efficiency amplifier 5, the purpose of improving satellite signal transmission efficiency can be achieved, and a plurality of groups of holes 15 are formed in the surface of the satellite pan 14 and at one end close to the signal receiver 16, so that rainwater is prevented from accumulating in the satellite pan 14, and damage to the signal receiver 16 is prevented.
The limiting clamping block 18 is connected with the fixed block 17, a telescopic rod 9 is arranged right below the signal receiver 16, a connecting block 10 is arranged at the top of the telescopic rod 9, a limiting cylinder 11 is arranged above the telescopic rod 9, the limiting cylinder 11 is positioned at the top of the connecting block 10, a rotating roller 12 is arranged above the telescopic rod 9, the rotating roller 12 is movably sleeved in the limiting cylinder 11, and the rotating roller 12 is rotatably arranged by taking the central axis of the limiting cylinder 11 as the center;
the surface of the rotary roller 12 is provided with a limit clamping groove 13, the limit clamping groove 13 is clamped with a limit clamping block 18, the bottom of the telescopic rod 9 is provided with a mounting base plate 7, the surface of the mounting base plate 7 is provided with two groups of fixed mounting holes 8, and the two groups of fixed mounting holes 8 are symmetrically arranged by taking the central axis of the mounting base plate 7 as the center.
Specifically, through rotatory roller 12 activity cup joints in the inside of spacing section of thick bamboo 11, rethread rotatory roller 12 rotates the setting with the axis of spacing section of thick bamboo 11 as the center, and the staff of being convenient for adjusts signal receiver 16's angle, rethread telescopic link 9's flexible effect, the staff of being convenient for adjusts signal receiver 16's height.
The communication transmission module experimental equipment based on the space-time satellite provided by the embodiment of the utility model has the following working principle:
through the arrangement of the signal receiver 16, signals are transmitted to the signal converter 6, then through the arrangement of the high-efficiency amplifier 5 (model number is QPA 9940), the purpose of improving satellite signal transmission efficiency can be achieved, and a plurality of groups of holes 15 are formed in the surface of the satellite pan 14 and at one end close to the signal receiver 16, so that rainwater is prevented from accumulating in the satellite pan 14, and damage to the signal receiver 16 is prevented;
through rotatory roller 12 activity cup joints in the inside of spacing section of thick bamboo 11, rethread rotatory roller 12 rotates the setting with the axis of spacing section of thick bamboo 11 as the center, and the staff of being convenient for adjusts signal receiver 16's angle, rethread telescopic link 9's flexible effect is convenient for the staff to signal receiver 16's height adjustment.
Although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit and scope of the technical solutions of the embodiments of the present utility model.
Claims (8)
1. Communication transmission module experimental facilities based on space-time satellite, including protective housing (1) and signal receiver (16), its characterized in that: the high-efficiency amplifier (5) is arranged in the protective shell (1), the signal converter (6) is arranged in the protective shell (1), and the satellite pan (14) is arranged on the surface of the signal receiver (16);
the satellite dish is characterized in that a plurality of groups of holes (15) are formed in the surface of the satellite dish (14) and one end close to a signal receiver (16), a telescopic rod (9) is arranged under the signal receiver (16), a mounting base plate (7) is arranged at the bottom of the telescopic rod (9), a connecting block (10) is arranged at the top of the telescopic rod (9), a limiting cylinder (11) is arranged above the telescopic rod (9), the limiting cylinder (11) is located at the top of the connecting block (10), and a rotary roller (12) is arranged above the telescopic rod (9).
2. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: the bottom of the protective shell (1) is provided with a plurality of groups of fixed supporting legs (2), and the fixed supporting legs (2) are arranged in a rectangular array by taking the central axis of the protective shell (1) as the center.
3. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: a plurality of groups of wiring through holes (3) are connected to the two opposite side walls of the protective shell (1) in a penetrating way, and the groups of wiring through holes (3) are symmetrically arranged with the central axis of the protective shell (1) as the center.
4. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: the top of the protective shell (1) is provided with a heat dissipation window (4), and the central axis of the heat dissipation window (4) coincides with the central axis of the protective shell (1).
5. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: the plurality of groups of holes (15) are arranged in an annular array with the central axis of the signal receiver (16) as the center, and the bottom of the signal receiver (16) is provided with a fixed block (17).
6. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: two groups of fixed mounting holes (8) are formed in the surface of the mounting base plate (7), and the two groups of fixed mounting holes (8) are symmetrically arranged with the central axis of the mounting base plate (7) as the center.
7. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: the rotary roller (12) is movably sleeved in the limiting cylinder (11), and the rotary roller (12) is rotatably arranged by taking the central axis of the limiting cylinder (11) as the center.
8. The space-time satellite-based communication transmission module experimental equipment according to claim 1, wherein: the bottom of signal receiver (16) is equipped with spacing joint piece (18), the surface of rotatory roller (12) is equipped with spacing joint groove (13), spacing joint groove (13) and spacing joint piece (18) joint setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322287391.7U CN220545008U (en) | 2023-08-24 | 2023-08-24 | Communication transmission module experimental facility based on space satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322287391.7U CN220545008U (en) | 2023-08-24 | 2023-08-24 | Communication transmission module experimental facility based on space satellite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220545008U true CN220545008U (en) | 2024-02-27 |
Family
ID=89964189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322287391.7U Active CN220545008U (en) | 2023-08-24 | 2023-08-24 | Communication transmission module experimental facility based on space satellite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220545008U (en) |
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2023
- 2023-08-24 CN CN202322287391.7U patent/CN220545008U/en active Active
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