CN215871415U - Small satellite communication integrated system - Google Patents
Small satellite communication integrated system Download PDFInfo
- Publication number
- CN215871415U CN215871415U CN202122172466.8U CN202122172466U CN215871415U CN 215871415 U CN215871415 U CN 215871415U CN 202122172466 U CN202122172466 U CN 202122172466U CN 215871415 U CN215871415 U CN 215871415U
- Authority
- CN
- China
- Prior art keywords
- pipe
- satellite communication
- fixedly connected
- integrated system
- wall
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Details Of Aerials (AREA)
Abstract
The utility model discloses a small satellite communication integrated system, which relates to the technical field of satellite communication and comprises a communication antenna and a satellite communication integrated system body, wherein a plastic waterproof shell is fixedly arranged at the bottom of the communication antenna, a waterproof sealing door is movably connected to the front surface of the plastic waterproof shell, an observation window is fixedly arranged on the front surface of the waterproof sealing door, a heat dissipation mechanism is arranged on the back surface of the plastic waterproof shell, and a buffer protection mechanism is arranged in an inner cavity of the plastic waterproof shell. According to the utility model, the satellite communication integrated system body can be elastically supported through the design of the elastic piece, when the satellite communication integrated system body falls, the falling force borne by the satellite communication integrated system body is buffered through the matching of the rubber triangular block and the air bag, the problem that the satellite communication integrated system body is damaged due to overlarge falling force is avoided, and the safety of the device is improved.
Description
Technical Field
The utility model relates to a satellite communication system, relates to the technical field of satellite communication, and particularly relates to a small satellite communication integrated system.
Background
The satellite communication system is actually microwave communication, which uses a satellite as a relay station to transmit microwave signals and communicates among a plurality of ground stations, the main purpose of the satellite communication is to realize seamless coverage on the ground, and because the satellite works on an orbit of hundreds, thousands or even tens of thousands of kilometers, the coverage range is far larger than that of a general mobile communication system. The following problems exist in the prior art:
1. the common satellite communication integrated system body does not have the function of buffer protection, and the common satellite communication integrated system body carelessly falls off from a hand when being held by a user, so that the safety of devices in the system can be influenced by the impact force generated by falling;
2. the common satellite communication integrated system body does not have a heat dissipation function, and the temperature of an internal device rises after the system is used for a long time, so that the operation efficiency of the system is influenced and needs to be improved.
SUMMERY OF THE UTILITY MODEL
The utility model provides a small satellite communication integrated system, which has a buffer protection function and solves the problem that a satellite communication integrated system body is easily damaged due to falling; the other purpose is to solve the problem that the operation efficiency of the system is affected by the temperature rise of the internal devices, so that the effect of radiating the devices in the satellite communication integrated system body is achieved.
In order to solve the technical problems, the technical scheme adopted by the utility model is as follows:
the utility model provides a little satellite communication integration system, includes communication antenna and satellite communication integration system body, communication antenna's bottom fixed mounting has the waterproof casing of plastics, the positive swing joint of the waterproof casing of plastics has waterproof sealing door, the positive fixed mounting of waterproof sealing door has the observation window, the back of the waterproof casing of plastics is provided with heat dissipation mechanism, be provided with buffer protection mechanism in the inner chamber of the waterproof casing of plastics.
The heat dissipation mechanism comprises a back connection shell and a bent heat dissipation main pipe, the back fixed mounting of the back connection shell is provided with a fan, the bent heat dissipation main pipe comprises a copper pipe, the copper pipe is fixedly mounted on the back of an inner cavity of the plastic waterproof shell, and a graphene layer is fixedly connected to the inner wall of the copper pipe.
The buffering protection mechanism comprises an elastic piece, the elastic piece is movably connected to the top and the bottom of the satellite communication integrated system body, one end, far away from the satellite communication integrated system body, of the elastic piece is fixedly connected with the inner wall of the plastic waterproof shell, and a cavity is formed in the plastic waterproof shell.
The technical scheme of the utility model is further improved as follows: the heat-absorbing coating is coated on the inner wall of the graphene layer, the heat-radiating fins are fixedly connected to the inner wall of the graphene layer, the lower discharging pipe is fixedly connected to the back of the copper pipe, and the back of the lower discharging pipe extends to the back of the back connection shell.
The technical scheme of the utility model is further improved as follows: the air outlet pipe of the fan extends to the inner cavity of the back connecting shell and is fixedly connected with a three-way pipe, the top and the bottom of the three-way pipe are fixedly connected with an air pipe, and one end, away from the three-way pipe, of the air pipe is fixedly connected with the back of the copper pipe.
The technical scheme of the utility model is further improved as follows: the air inlet pipe fixedly connected with protective tube of fan, the dismantlement formula is connected with the protection network on the inner wall of protective tube, the bottom fixedly connected with connecting pipe of protective tube inner chamber.
The technical scheme of the utility model is further improved as follows: the bottom fixed mounting of protective tube inner chamber has the water conservancy diversion piece, the top fixed mounting of connecting pipe has the arc cover.
The technical scheme of the utility model is further improved as follows: the corner fixed mounting of plastics waterproof housing inner wall has three hornblocks of rubber, three hornblocks of rubber keep away from the one end fixedly connected with gasbag of the waterproof casing of plastics, the one end fixedly connected with connecting block of three hornblocks of rubber is kept away from to the gasbag, the outer wall of satellite communication integration system body is connected with the inner wall dismantlement formula of connecting block.
Due to the adoption of the technical scheme, compared with the prior art, the utility model has the technical progress that:
1. the utility model provides a small satellite communication integrated system, which adopts the combination of an elastic piece, a rubber triangular block and an air bag, can elastically support a satellite communication integrated system body through the design of the elastic piece, and can buffer the falling force applied to the satellite communication integrated system body through the matching of the rubber triangular block and the air bag when the satellite communication integrated system body falls, so as to avoid the problem that the satellite communication integrated system body is damaged due to overlarge falling force.
2. The utility model provides a small satellite communication integrated system, which adopts the combination of a copper pipe, a graphene layer, a heat absorption coating, a heat dissipation fin and a fan, can absorb heat emitted by a satellite communication integrated system body in an inner cavity of a plastic waterproof shell into the inner cavity of the copper pipe through the design of the copper pipe, the graphene layer and the heat absorption coating, and can drive external air to move through the inner cavity of the copper pipe through the operation of the fan, so that the heat is emitted from a lower discharge pipe through the cooperation of the heat dissipation fin, the function of dissipating heat of the satellite communication integrated system body is realized, the problem that the operation efficiency of the system is influenced by the temperature rise of internal devices is avoided, and the practicability of the device is improved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the internal structure of the plastic waterproof case of the present invention;
FIG. 3 is a schematic structural diagram of a heat dissipation mechanism according to the present invention;
FIG. 4 is a schematic view of the internal structure of the shielding tube of the present invention;
fig. 5 is a schematic cross-sectional structure view of the bent heat dissipation main tube of the present invention.
In the figure: 1. a communication antenna; 11. a satellite communication integrated system body; 2. a plastic waterproof housing; 3. a waterproof closure door; 4. an observation window;
5. a heat dissipation mechanism; 51. the back part is connected with the shell; 52. a fan; 53. a three-way pipe; 54. bending the heat dissipation main pipe; 541. a copper pipe; 542. a graphene layer; 543. a heat absorbing coating; 544. heat dissipation fins; 55. discharging the pipes; 56. a protective tube; 561. a protective net; 562. a connecting pipe; 563. an arc-shaped cover; 564. a flow guide block;
6. a buffer protection mechanism; 61. an elastic member; 62. a rubber triangular block; 63. an air bag; 64. connecting blocks; 65. a cavity.
Detailed Description
The present invention will be described in further detail with reference to the following examples:
example 1
As shown in fig. 1-5, the present invention provides a small satellite communication integrated system, which comprises a communication antenna 1 and a satellite communication integrated system body 11, wherein a plastic waterproof casing 2 is fixedly installed at the bottom of the communication antenna 1, a waterproof closing door 3 is movably connected to the front surface of the plastic waterproof casing 2, an observation window 4 is fixedly installed at the front surface of the waterproof closing door 3, a heat dissipation mechanism 5 is installed at the back surface of the plastic waterproof casing 2, a buffer protection mechanism 6 is installed in the inner cavity of the plastic waterproof casing 2, the heat dissipation mechanism 5 comprises a back connection casing 51 and a bent heat dissipation main pipe 54, a fan 52 is fixedly installed at the back surface of the back connection casing 51, the bent heat dissipation main pipe 54 comprises a copper pipe 541, the copper pipe is fixedly installed at the back surface of the inner cavity of the plastic waterproof casing 2, a graphene layer 542 is fixedly connected to the inner wall of the copper pipe 541, the buffer protection mechanism 6 comprises an elastic member 61, elastic component 61 swing joint is in the top and the bottom of satellite communication integration system body 11, the one end that satellite communication integration system body 11 was kept away from to elastic component 61 and the inner wall fixed connection of waterproof casing 2 of plastics, cavity 65 has been seted up to the inside of waterproof casing 2 of plastics, control fan 52 moves, can drive outside air and remove in the inner chamber through copper pipe 541, thereby cooperation heat dissipation wing 544 distributes the heat from lower tub of 55, the realization is to satellite communication integration system body 11 carry out radiating function.
Example 2
As shown in fig. 1 to 5, on the basis of embodiment 1, the present invention provides a technical solution: preferably, scribble on graphite alkene layer 542's the inner wall and be equipped with heat absorption coating 543, fixedly connected with heat dissipation wing 544 on graphite alkene layer 542's the inner wall, calandria 55 under copper 541's the back fixedly connected with, the back of calandria 55 extends to the back and connects the back of casing 51 down, fan 52's play tuber pipe extends to fixedly connected with three-way pipe 53 in the inner chamber of casing 51 is connected at the back, the equal fixedly connected with tuber pipe in top bottom of three-way pipe 53, the one end that three-way pipe 53 was kept away from to the tuber pipe and copper 541's back fixed connection, heat absorption coating 543 can design for the black nickel coating, cooperation graphite alkene layer 542 absorbs the heat that satellite communication integration system body 11 gived off to the inner chamber of copper pipe fast, be convenient for this device radiating going on.
Example 3
As shown in fig. 1 to 5, on the basis of embodiment 1, the present invention provides a technical solution: preferably, the air inlet pipe of the fan 52 is fixedly connected with the protective pipe 56, the inner wall of the protective pipe 56 is detachably connected with the protective net 561, the bottom of the inner cavity of the protective pipe 56 is fixedly connected with the connecting pipe 562, the bottom of the inner cavity of the protective pipe 56 is fixedly provided with the flow guide block 564, the top of the connecting pipe 562 is fixedly provided with the arc-shaped cover 563, the corner of the inner wall of the plastic waterproof shell 2 is fixedly provided with the rubber triangular block 62, one end of the rubber triangular block 62 away from the plastic waterproof shell 2 is fixedly connected with the air bag 63, one end of the air bag 63 away from the rubber triangular block 62 is fixedly connected with the connecting block 64, the outer wall of the satellite communication integrated system body 11 is detachably connected with the inner wall of the connecting block 64, the satellite communication integrated system body 11 can be elastically supported through the design of the elastic piece 61, when the satellite communication integrated system body 11 falls, the falling force received by the satellite communication integrated system body 11 is buffered through the cooperation of the rubber block 62 and the air bag 63, the problem that the satellite communication integrated system body 11 is damaged due to the fact that the falling force is too large is avoided, large impurities can be blocked through the design of the protective net 561, the problem that the fan 52 normally operates is avoided, dust can be further blocked through the arc-shaped cover 563, and the blocked impurities partially slide to the bottom of the protective pipe 56 from the top of the arc-shaped cover 563 when the fan 52 is idle.
The working principle of the integrated system for communication of small satellites is described in detail below.
As shown in fig. 1-5, when the waterproof sealing door 3 is opened, the satellite communication integrated system body 11 can be matched with the communication antenna 1 to perform communication work, the fan 52 is controlled to operate, and the outside air is driven to move through the inner cavity of the copper pipe 541, so that the satellite communication integrated system body 11 is cooled, the satellite communication integrated system body 11 can be buffered and protected through the matching of the elastic piece 61, the rubber triangular block 62 and the air bag 63, and the satellite communication integrated system body 11 can be protected from water through the matching of the plastic waterproof shell 2 and the waterproof sealing door 3.
The present invention has been described in general terms in the foregoing, but it will be apparent to those skilled in the art that modifications and improvements can be made thereto based on the present invention. Therefore, modifications or improvements are within the scope of the utility model without departing from the spirit of the inventive concept.
Claims (6)
1. A moonlet communication integration system, includes communication antenna (1) and satellite communication integration system body (11), its characterized in that: a plastic waterproof shell (2) is fixedly installed at the bottom of the communication antenna (1), a waterproof sealing door (3) is movably connected to the front of the plastic waterproof shell (2), an observation window (4) is fixedly installed on the front of the waterproof sealing door (3), a heat dissipation mechanism (5) is arranged on the back of the plastic waterproof shell (2), and a buffer protection mechanism (6) is arranged in an inner cavity of the plastic waterproof shell (2);
the heat dissipation mechanism (5) comprises a back connection shell (51) and a bent heat dissipation main pipe (54), a fan (52) is fixedly installed on the back of the back connection shell (51), the bent heat dissipation main pipe (54) comprises a copper pipe (541), the copper pipe (541) is fixedly installed on the back of an inner cavity of the plastic waterproof shell (2), and a graphene layer (542) is fixedly connected to the inner wall of the copper pipe (541);
buffering protection mechanism (6) include elastic component (61), elastic component (61) swing joint is in the top and the bottom of satellite communication integration system body (11), the one end of satellite communication integration system body (11) and the inner wall fixed connection of plastics waterproof housing (2) are kept away from in elastic component (61), cavity (65) have been seted up to the inside of plastics waterproof housing (2).
2. The integrated moonlet communication system according to claim 1, wherein: the utility model discloses a copper pipe, including graphite pipe (541), copper pipe (542), heat absorption coating (543) is scribbled on the inner wall of graphite pipe layer (542), fixedly connected with heat dissipation fin (544) on the inner wall of graphite pipe layer (542), calandria (55) down in the back fixedly connected with of copper pipe (541), the back of calandria (55) down extends to the back of back connection casing (51).
3. The integrated moonlet communication system according to claim 1, wherein: the air outlet pipe of the fan (52) extends into an inner cavity of the back connecting shell (51) and is fixedly connected with a three-way pipe (53), the top and the bottom of the three-way pipe (53) are fixedly connected with an air pipe, and one end, far away from the three-way pipe (53), of the air pipe is fixedly connected with the back face of the copper pipe (541).
4. The integrated moonlet communication system according to claim 1, wherein: the air inlet pipe of the fan (52) is fixedly connected with a protective pipe (56), the inner wall of the protective pipe (56) is detachably connected with a protective net (561), and the bottom of the inner cavity of the protective pipe (56) is fixedly connected with a connecting pipe (562).
5. The integrated moonlet communication system according to claim 4, wherein: the bottom fixed mounting of protective tube (56) inner chamber has water conservancy diversion piece (564), the top fixed mounting of connecting pipe (562) has arc cover (563).
6. The integrated moonlet communication system according to claim 1, wherein: corner fixed mounting of waterproof casing of plastics (2) inner wall has three hornblocks of rubber (62), the one end fixedly connected with gasbag (63) of the waterproof casing of plastics (2) are kept away from to three hornblocks of rubber (62), the one end fixedly connected with connecting block (64) of three hornblocks of rubber (62) are kept away from in gasbag (63), the outer wall of satellite communication integration system body (11) is connected with the inner wall dismantlement formula of connecting block (64).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122172466.8U CN215871415U (en) | 2021-09-09 | 2021-09-09 | Small satellite communication integrated system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122172466.8U CN215871415U (en) | 2021-09-09 | 2021-09-09 | Small satellite communication integrated system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215871415U true CN215871415U (en) | 2022-02-18 |
Family
ID=80257738
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122172466.8U Active CN215871415U (en) | 2021-09-09 | 2021-09-09 | Small satellite communication integrated system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215871415U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115605007A (en) * | 2022-11-30 | 2023-01-13 | 航大防务（海南）科技有限公司（Cn） | Satellite remote sensing data transmission processing equipment |
-
2021
- 2021-09-09 CN CN202122172466.8U patent/CN215871415U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115605007A (en) * | 2022-11-30 | 2023-01-13 | 航大防务（海南）科技有限公司（Cn） | Satellite remote sensing data transmission processing equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN215871415U (en) | Small satellite communication integrated system | |
| CN111314797A (en) | 5G base station cooling system based on big data processing | |
| CN208433493U (en) | Battery cooling cycle assembly | |
| CN210607625U (en) | Vehicle-mounted antenna with protection structure | |
| CN113904089A (en) | Foldable portable dual-mode ultra-wideband omnidirectional antenna | |
| CN105974371A (en) | Phased array meteorological radar antenna structure | |
| CN112490663B (en) | Integrated antenna | |
| CN211858850U (en) | 5G signal antenna capable of being adjusted at multiple degrees of freedom | |
| CN214084732U (en) | Front radome for aircraft | |
| CN209375843U (en) | A kind of high power router heat-dissipating casing | |
| CN205844516U (en) | Phased array weather radar scanner structure | |
| CN221324835U (en) | Protective cover with heat radiation function | |
| CN212518655U (en) | Remote control generating set | |
| CN207474950U (en) | A kind of drawer-type switch cabinet of shockproof heat dissipation | |
| CN215188014U (en) | Isolated heat radiation structure | |
| CN116991216B (en) | Waterproof type reinforced notebook with liquid diversion component | |
| CN219937160U (en) | Battery tray heat radiation structure | |
| CN216437389U (en) | PoE PD protocol converter | |
| CN209111960U (en) | A kind of hermetically sealed wall-mounted charging pile carrying body structure | |
| CN216016461U (en) | Solar charging controller with intelligent battery management function | |
| CN213124643U (en) | Protection structure of potassium ion battery | |
| CN211234016U (en) | Counter-flow cooling tower | |
| CN217300897U (en) | Gear atomizer that radiating rate is fast is with heat dissipation shell | |
| CN216389685U (en) | Integrated antenna structure | |
| CN208834304U (en) | A kind of high security wireless information carrying device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: 9th Floor, Building 3, Zone 6, No. 188 South Fourth Ring West Road, Fengtai District, Beijing, 100070 Patentee after: Beijing Guolian video information technology Co.,Ltd. Address before: Room 703, building 1, No. 1, Shangdi Information Road, Haidian District, Beijing 100089 Patentee before: Beijing Guolian video information technology Co.,Ltd. |