CN113966107A - Satellite power box of satellite application industry - Google Patents
Satellite power box of satellite application industry Download PDFInfo
- Publication number
- CN113966107A CN113966107A CN202111011209.4A CN202111011209A CN113966107A CN 113966107 A CN113966107 A CN 113966107A CN 202111011209 A CN202111011209 A CN 202111011209A CN 113966107 A CN113966107 A CN 113966107A
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- CN
- China
- Prior art keywords
- power box
- satellite
- satellite power
- fixedly connected
- extrusion
- 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.)
- Withdrawn
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 43
- 238000001125 extrusion Methods 0.000 claims abstract description 41
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 37
- 229920000742 Cotton Polymers 0.000 claims abstract description 34
- 230000017525 heat dissipation Effects 0.000 claims abstract description 17
- 238000010521 absorption reaction Methods 0.000 claims abstract description 16
- 238000004140 cleaning Methods 0.000 claims description 9
- 238000001179 sorption measurement Methods 0.000 claims description 5
- 238000001704 evaporation Methods 0.000 abstract description 2
- 230000008020 evaporation Effects 0.000 abstract description 2
- 238000010030 laminating Methods 0.000 abstract description 2
- 239000000428 dust Substances 0.000 description 6
- 230000000903 blocking effect Effects 0.000 description 5
- 238000001514 detection method Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 206010061218 Inflammation Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- JJWKPURADFRFRB-UHFFFAOYSA-N carbonyl sulfide Chemical compound O=C=S JJWKPURADFRFRB-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000004054 inflammatory process Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/2029—Modifications to facilitate cooling, ventilating, or heating using a liquid coolant with phase change in electronic enclosures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B1/00—Cleaning by methods involving the use of tools
- B08B1/10—Cleaning by methods involving the use of tools characterised by the type of cleaning tool
- B08B1/12—Brushes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B9/00—Cleaning hollow articles by methods or apparatus specially adapted thereto
- B08B9/08—Cleaning containers, e.g. tanks
- B08B9/087—Cleaning containers, e.g. tanks by methods involving the use of tools, e.g. brushes, scrapers
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/02—Details
- H05K5/0213—Venting apertures; Constructional details thereof
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/2029—Modifications to facilitate cooling, ventilating, or heating using a liquid coolant with phase change in electronic enclosures
- H05K7/20327—Accessories for moving fluid, for connecting fluid conduits, for distributing fluid or for preventing leakage, e.g. pumps, tanks or manifolds
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- Filtering Of Dispersed Particles In Gases (AREA)
Abstract
The invention discloses a satellite power box in the satellite application industry, and relates to the technical field of the satellite application industry. This satellite power box of satellite application industry, including being used for carrying out the extruded gas extrusion mechanism to gas, be used for the extrusion to carry out the extrusion deashing mechanism of deashing and be used for adsorbing and carry out radiating absorption heat dissipation mechanism to the device, the inside of gas extrusion mechanism is provided with the satellite power box, gas extrusion mechanism is through the satellite power box bottom fixedly connected with extrusion deashing mechanism that sets up. This satellite power box of industry is used to satellite makes inside water evaporation through outside temperature, then floats in the satellite power box cavity to insulate against heat to outside high temperature, avoided the too high of inside temperature, first cotton can adsorb vapor of absorbing in addition, then the laminating satellite power box inner wall cools off, and the air in the urceolus is generated heat after being extruded, then when gaseous entering into the aquatic, the heat absorption behind the molecular force doing work.
Description
Technical Field
The invention relates to the technical field of satellite application industries, in particular to a satellite power box of a satellite application industry.
Background
Satellites can be classified into three categories according to their purposes: the scientific satellite is used for scientific detection and research, mainly comprises a space physical detection satellite and an astronomical satellite, is used for researching high-rise atmosphere, an earth radiation zone, an earth magnetic layer, a cosmic ray, solar radiation and the like, and can observe other stars; the use of satellites is closely linked to the use of terrestrial satellite receivers, and the most commonly used satellite receivers are power boxes.
Under summer inflammation, the internal elements of the power box at high temperature are very easy to damage, so that the transmission of satellite signals is interrupted, and the use of satellites is influenced.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a satellite power box in the satellite application industry, which dissipates heat to avoid the damage of internal elements by using the cyclic conversion of water and steam.
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides a satellite power box of satellite application industry, is including being used for carrying out the extruded gas extrusion mechanism to gas, being used for the extrusion to carry out the extrusion deashing mechanism of deashing and being used for adsorbing the absorption heat dissipation mechanism that carries out the heat dissipation to the device, the inside of gas extrusion mechanism is provided with the satellite power box, gas extrusion mechanism is through the satellite power box bottom fixedly connected with extrusion deashing mechanism that sets up, gas extrusion mechanism adsorbs heat dissipation mechanism through the satellite power box medial surface fixedly connected with that sets up.
Preferably, the inside of the gas extrusion mechanism comprises a satellite power box and an extruder, the outer wall of the satellite power box is fixedly connected with supporting legs, the satellite power box is fixedly connected with the extruder through the supporting legs, and an extrusion plate is inserted in the axis of the extruder.
Preferably, the bottom of the satellite power box is fixedly connected with an automatic blocking device, the satellite power box is fixedly connected with an outer barrel through the automatic blocking device, and the extruding machine is inserted into the inner wall of the outer barrel through an extruding plate.
Preferably, the inside of extrusion deashing mechanism includes elastic webbing, bell mouth, first elastic rod, arc and cleaning brush, the cavity has been seted up to the inside of satellite power box, elastic webbing fixed connection is at the interior bottom of satellite power box cavity, a plurality of bell mouth has been seted up to the interior bottom of satellite power box, the first elastic rod of inner wall fixedly connected with of bell mouth, the outer wall fixedly connected with arc of first elastic rod, the top fixedly connected with cleaning brush of first elastic rod.
Preferably, the adsorption and heat dissipation mechanism comprises first water absorption cotton and a small air bag, the inner wall of the cavity of the satellite power box is fixedly connected with the first water absorption cotton, the water storage bin is arranged inside the first water absorption cotton, a plurality of holes are formed in the position, located in the first water absorption cotton, of the inner wall of the satellite power box, the small air bag is fixedly connected to the position, located in the holes, of the inner wall of the satellite power box, and the first water absorption cotton is made of sponge materials.
Preferably, the satellite power box is connected with the second water-absorbing cotton through the inner top of the cavity, the inner wall of the cavity is fixedly connected with a second elastic rod at the position where the second water-absorbing cotton is located, and the tail end of the second elastic rod is fixedly connected with a third water-absorbing cotton.
The invention provides a satellite power box in the satellite application industry. The method has the following beneficial effects:
1. this satellite power box of satellite application industry generates heat after being extruded through the air in the urceolus, and then when gaseous entering aquatic, the molecular force absorbs the heat after doing work to make water and satellite power box cooling.
2. This satellite power box of satellite application industry makes inside water evaporation through outside temperature, then floats in the satellite power box cavity to insulate against heat to outside high temperature, avoided the too high of inside temperature, first cotton can adsorb vapor that absorbs water moreover, then the laminating satellite power box inner wall cools off, has ensured the normal use of satellite power box.
3. According to the satellite power box in the satellite application industry, air in the elastic belt is discharged from the conical opening through the impact of airflow on the elastic belt and flows inside the satellite power box, so that dust on internal elements is cleaned, and the heat dissipation of the internal elements is ensured.
4. This satellite power box of satellite application industry, the air current through the bell mouth is when the arc, and first elastic rod can be rocked by air current blowing left and right sides to make the cleaning brush dispel the heat to the interior component in the satellite power box, ensured the heat dissipation of interior component.
5. This satellite power box of satellite application industry sets up through the toper of bell mouth to make the dust get into easily, be difficult to go out moreover, ensured the collection of dust.
Drawings
FIG. 1 is a schematic axial side perspective view of the present invention;
FIG. 2 is a schematic cross-sectional view of FIG. 1 in accordance with the present invention;
FIG. 3 is an enlarged view of portion A of FIG. 2 according to the present invention;
FIG. 4 is an enlarged view of the portion B of FIG. 2 according to the present invention.
In the figure: 1. a gas extrusion mechanism; 11. a satellite power box; 12. an outer cylinder; 13. an extruder; 14. an automatic plugging device; 2. an extrusion ash removal mechanism; 21. an elastic band; 22. a tapered mouth; 23. a first elastic rod; 24. an arc-shaped plate; 25. cleaning a brush; 3. an adsorption heat dissipation mechanism; 31. first absorbent cotton; 32. second absorbent cotton; 33. third absorbent cotton; 34. a small-sized air bag; 35. a second elastic rod;
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a satellite power box of satellite application industry, including being used for carrying out the extruded gas extrusion mechanism 1 to gas, be used for the extrusion to carry out the extrusion deashing mechanism 2 of deashing and be used for adsorbing to carry out radiating absorption heat dissipation mechanism 3 to the device, the inside of gas extrusion mechanism 1 is provided with satellite power box 11, gas extrusion mechanism 1 is through the 11 bottom fixedly connected with extrusion deashing mechanisms 2 of satellite power box that set up, gas extrusion mechanism 1 is through the 11 medial surface fixedly connected with absorption heat dissipation mechanism 3 of satellite power box that set up.
In this embodiment, the extruder 13 is a conventional device, and extrudes air.
Specifically, the inside of the gas extrusion mechanism 1 comprises a satellite power box 11 and an extruder 13, the outer wall of the satellite power box 11 is fixedly connected with supporting legs, the satellite power box 11 is fixedly connected with the extruder 13 through the supporting legs, and an extrusion plate is inserted in the axis of the extruder 13.
In this embodiment, some water is added to the cavity of the satellite power box 11 during the daytime.
Specifically, an automatic blocking device 14 is fixedly connected to the bottom of the satellite power box 11, an outer cylinder 12 is fixedly connected to the satellite power box 11 through the arranged automatic blocking device 14, and the extruding machine 13 is inserted into the inner wall of the outer cylinder 12 through the arranged extruding plate.
In this embodiment, the extruder 13 is continuously and cyclically extruded in the outer cylinder 12 by the extrusion plate.
Specifically, the inside of extrusion deashing mechanism 2 includes elastic webbing 21, bell 22, first elastic rod 23, arc 24 and cleaning brush 25, the cavity has been seted up to satellite power box 11's inside, elastic webbing 21 fixed connection is at the interior bottom of satellite power box 11 cavity, a plurality of bell 22 has been seted up to satellite power box 11's interior bottom, the first elastic rod 23 of inner wall fixedly connected with of bell 22, the outer wall fixedly connected with arc 24 of first elastic rod 23, the top fixedly connected with cleaning brush 25 of first elastic rod 23.
In the present embodiment, when the pressing plate is pressed while being located in the outer cylinder 12, the gas inside the outer cylinder 12 is pressed, so that the distance between molecules becomes small, thereby increasing the molecular frictional heat generation.
Specifically, the inside of the adsorption and heat dissipation mechanism 3 includes first absorbent cotton 31 and a small airbag 34, the first absorbent cotton 31 is fixedly connected to the inner wall of the cavity of the satellite power box 11, the water storage bin is arranged inside the first absorbent cotton 31, a plurality of holes are formed in the position of the inner wall of the satellite power box 11, which is located in the first absorbent cotton 31, and the small airbag 34 is fixedly connected to the position of the inner wall of the satellite power box 11, which is located in the holes.
In this embodiment, water in the satellite power box 11 is continuously evaporated at a high temperature outdoors and then flows in the satellite power box 11.
Specifically, the satellite power box 11 is fixedly connected with the second water-absorbing cotton 32 through the inner top of the cavity, the inner wall of the cavity is located at the position fixedly connected with the second elastic rod 35 of the second water-absorbing cotton 32, and the tail end fixedly connected with the third water-absorbing cotton 33 of the second elastic rod 35.
In this embodiment, at night, the water vapor inside the satellite power box 11 is condensed again into water and collected in the elastic band 21.
When the device is used, in daytime, some water is added into the cavity of the satellite power box 11, the extruder 13 continuously and circularly extrudes in the outer barrel 12 through the extrusion plate, when the extrusion plate is positioned in the outer barrel 12 for extrusion, the gas in the outer barrel 12 is extruded, so that the space between molecules is reduced, the molecular friction heating is intensified, then the automatic blocking device 14 is opened to release the gas, when the gas enters the cavity of the satellite power box 11, the molecular force does work and absorbs heat, so that the water temperature is reduced, air blown out from the outer barrel 12 impacts the water in the cavity of the satellite power box 11, water flow shakes towards two sides under the arc of the elastic belt 21, the water in the satellite power box 11 is continuously evaporated at outdoor high temperature and then flows in the satellite power box 11, and when the steam flows upwards in the cavity of the satellite power box 11, the steam has certain heat insulation effect on the high temperature, when steam floats to the upper part, the steam is gathered in the second absorbent cotton 32 and the third absorbent cotton 33, water gathered in the second absorbent cotton 32 also drops on the third absorbent cotton 33, then water drops continuously drop, when the water drops, the second elastic rod 35 vibrates, so that the dropping of the water drops is accelerated, the water drops drop on the first absorbent cotton 31 in the dropping process, the water gathers in a water storage bin of the first absorbent cotton 31 and then is attached to the inner wall of the satellite power box 11 for heat dissipation, the water in the first absorbent cotton 31 enters the small air bag 34 and is further attached to the inside of the satellite power box 11 for heat dissipation, when air flow impacts on the elastic belt 21, the elastic belt 21 extrudes the air between the satellite power box 11 and the elastic belt 21 from the conical opening 22, so that the air is cleaned in the satellite power box 11, and dust on internal elements drops, then the elastic band 21 resets under self elasticity, inhales to inside through bell 22, and the dust enters into the elastic band 21 through bell 22 and stores, when the air current blew off from bell 22, the air current blew on arc 24 to make first elastic rod 23 constantly rock, make cleaning brush 25 clear up the internal component dust, when evening, the inside vapor of satellite power box 11 condenses into water and gathers in elastic band 21 again.
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 should be equivalent or changed within the scope of the present invention.
Claims (6)
1. The utility model provides a satellite power box of satellite application industry, is used for carrying out extruded gas extrusion mechanism (1), is used for the extrusion to carry out extrusion deashing mechanism (2) of deashing and is used for adsorbing to carry out radiating absorption heat dissipation mechanism (3) to the device that is used for gas, its characterized in that: the inside of gas extrusion mechanism (1) is provided with satellite power box (11), bottom fixedly connected with extrusion deashing mechanism (2) are gone up through satellite power box (11) that set up in gas extrusion mechanism (1), gas extrusion mechanism (1) is through satellite power box (11) medial surface fixedly connected with absorption heat dissipation mechanism (3) that set up.
2. The satellite power box of the satellite application industry of claim 1, wherein: the inside of gas extrusion mechanism (1) includes satellite power box (11) and extruder (13), the outer wall fixedly connected with landing leg of satellite power box (11), satellite power box (11) is through landing leg fixedly connected with extruder (13) that sets up, the axle center department of extruder (13) is pegged graft and is had the stripper plate.
3. The satellite power box of the satellite application industry according to claim 2, wherein: the automatic plugging device (14) is fixedly connected to the bottom of the satellite power box (11), the outer barrel (12) is fixedly connected to the satellite power box (11) through the arranged automatic plugging device (14), and the extruding machine (13) is inserted into the inner wall of the outer barrel (12) through the arranged extruding plate.
4. The satellite power box of the satellite application industry of claim 1, wherein: the inside of extrusion deashing mechanism (2) includes elastic webbing (21), bell mouth (22), first elastic rod (23), arc (24) and cleaning brush (25), the cavity has been seted up to the inside of satellite power box (11), elastic webbing (21) fixed connection is in the interior bottom of satellite power box (11) cavity, a plurality of bell mouth (22) have been seted up to the interior bottom of satellite power box (11), the first elastic rod (23) of inner wall fixedly connected with of bell mouth (22), the outer wall fixedly connected with arc (24) of first elastic rod (23), the top fixedly connected with cleaning brush (25) of first elastic rod (23).
5. The satellite power box of the satellite application industry according to claim 4, wherein: the adsorption heat dissipation mechanism (3) is characterized in that the adsorption heat dissipation mechanism comprises first water absorption cotton (31) and small air bags (34), the first water absorption cotton (31) is fixedly connected to the inner wall of a cavity of the satellite power box (11), a water storage bin is arranged inside the first water absorption cotton (31), a plurality of holes are formed in the position, located on the first water absorption cotton (31), of the inner wall of the satellite power box (11), and the small air bags (34) are fixedly connected to the position, located on the holes, of the inner wall of the satellite power box (11).
6. The satellite power box of the satellite application industry of claim 5, wherein: satellite power box (11) are through the cotton (32) of absorbing water of the interior top fixedly connected with second of cavity, and the cavity inner wall is located the second and absorbs water position fixedly connected with second elastic rod (35) of cotton (32), cotton (33) are absorbed to the terminal fixedly connected with third of second elastic rod (35).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111011209.4A CN113966107A (en) | 2021-08-31 | 2021-08-31 | Satellite power box of satellite application industry |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111011209.4A CN113966107A (en) | 2021-08-31 | 2021-08-31 | Satellite power box of satellite application industry |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113966107A true CN113966107A (en) | 2022-01-21 |
Family
ID=79460561
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111011209.4A Withdrawn CN113966107A (en) | 2021-08-31 | 2021-08-31 | Satellite power box of satellite application industry |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113966107A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116130863A (en) * | 2022-12-28 | 2023-05-16 | 江苏河马自动化设备有限公司 | Low-power consumption battery box fire alarm controller |
-
2021
- 2021-08-31 CN CN202111011209.4A patent/CN113966107A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116130863A (en) * | 2022-12-28 | 2023-05-16 | 江苏河马自动化设备有限公司 | Low-power consumption battery box fire alarm controller |
| CN116130863B (en) * | 2022-12-28 | 2024-03-26 | 南京睿实智能安全科技有限公司 | Low-power consumption battery box fire alarm controller |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20220121 |