CN112711310A - Quick radiating radar machine case - Google Patents
Quick radiating radar machine case Download PDFInfo
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- CN112711310A CN112711310A CN202110015515.9A CN202110015515A CN112711310A CN 112711310 A CN112711310 A CN 112711310A CN 202110015515 A CN202110015515 A CN 202110015515A CN 112711310 A CN112711310 A CN 112711310A
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- 230000017525 heat dissipation Effects 0.000 claims abstract description 80
- 238000009423 ventilation Methods 0.000 claims abstract description 5
- 238000013500 data storage Methods 0.000 claims description 3
- 238000010030 laminating Methods 0.000 claims description 2
- 238000002791 soaking Methods 0.000 claims 5
- 238000004378 air conditioning Methods 0.000 claims 1
- 239000000203 mixture Substances 0.000 claims 1
- 239000002994 raw material Substances 0.000 claims 1
- 230000007306 turnover Effects 0.000 claims 1
- 238000010438 heat treatment Methods 0.000 abstract description 4
- 238000013461 design Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 238000012986 modification Methods 0.000 description 5
- 230000004048 modification Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 238000011161 development Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000004140 cleaning Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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Classifications
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
- G06F1/16—Constructional details or arrangements
- G06F1/18—Packaging or power distribution
- G06F1/183—Internal mounting support structures, e.g. for printed circuit boards, internal connecting means
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
- G06F1/16—Constructional details or arrangements
- G06F1/20—Cooling means
Abstract
The invention discloses a quick-heat-dissipation radar case which comprises a case, wherein each electronic element of a radar is arranged in the case, and the case comprises a case body and a ventilation unit; the heat dissipation device is arranged in the case and is connected with the air exchange unit in a matching way; and the quick connection device is matched and connected with the heat dissipation device and comprises a rebound unit and a support unit. The rapid heat dissipation radar case solves the problems of heat conduction and internal and external heat exchange of a relatively dense heating main body, is convenient to replace related structures, is convenient to maintain and clean, ensures that a radar host can conduct heat well, and ensures that a system can work reliably in a severe environment.
Description
Technical Field
The invention relates to the technical field of radars, in particular to a rapid heat dissipation radar case.
Background
The radar is an electronic device for detecting a target by using electromagnetic waves, has the advantages that the radar can detect a long-distance target at night and in the daytime, is not blocked by fog, cloud and rain, has the characteristics of all weather and all day time, and has certain penetrating power. Therefore, in addition to being indispensable in military affairs, radar is also widely used in scientific research and socioeconomic development. The specific use and structure of various radars vary, but the basic form is consistent, including transmitters, transmit antennas, receivers, receive antennas, processing sections, and displays. With the technical development of modern equipment, a miniaturized and high-density sealed case becomes a normal requirement of a modern radar, so that a plurality of dense electronic components are required, and the problems of structural design and heat dissipation brought by the electronic components also become one of the key points of system design.
Disclosure of Invention
This section is for the purpose of summarizing some aspects of embodiments of the invention and to briefly introduce some preferred embodiments. In this section, as well as in the abstract and the title of the invention of this application, simplifications or omissions may be made to avoid obscuring the purpose of the section, the abstract and the title, and such simplifications or omissions are not intended to limit the scope of the invention.
The present invention has been made in view of the above and/or other problems with existing radar capsule cases.
Therefore, the present invention is to solve the problem of a radar chassis with fast heat dissipation, which solves the problem of poor heat dissipation effect of the current miniaturized and high-density sealed chassis.
In order to solve the technical problem, the invention provides the following technical scheme that the rapid heat dissipation radar case comprises a case, wherein each electronic element of a radar is arranged in the case, and the case comprises a case body and a ventilation unit; the heat dissipation device is arranged in the case and is connected with the air exchange unit in a matching way; and the quick connection device is matched and connected with the heat dissipation device and comprises a rebound unit and a support unit.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the air exchange unit comprises an air duct cover plate, an air deflector and a heat dissipation plate, the air deflector is of a rectangular structure with two open sides, one open side of the air deflector is connected with the air duct cover plate, an air port is formed in the air duct cover plate, filter yarns are arranged in the air port, the heat dissipation plate is of a rectangular fin structure and is mounted at the open end of the other side of the air deflector, and fins are located inside the air deflector.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the heat dissipation device comprises a heat dissipation fan and a vapor chamber, the heat dissipation fan comprises an air suction fan and an air outlet fan, an opening is formed in one side of the heat dissipation plate, the air suction fan and the air outlet fan are respectively installed close to openings at two ends, and the vapor chamber is of a fin structure.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the case body comprises a case body and a cover plate, the air inlet and the air outlet are formed in the case body, the vapor chamber is provided with a plurality of blocks and is respectively arranged between the bottom surfaces of the case body and the cover plate, the vapor chamber is provided with modules required by radars such as a power supply, a CPU (central processing unit), an anti-interference module, a temperature sensor, a receiving and sending module and a data storage module, and the fin direction of the vapor chamber is consistent with the air inlet and outlet direction of the case.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the resilience unit is arranged in the box body and comprises a base, a sliding block, a pull rod and a buckle, wherein the sliding block is arranged on the base, one end of the sliding block is connected with one end of the base through a first elastic piece, the other end of the sliding block is provided with a limiting groove, the other end of the base is provided with a first hinge hole, two ends of the pull rod are provided with first hinges, and the first hinges are positioned on the same side and one side of the first hinges is connected with the first hinge hole in a matched mode.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the bottom surface of the limiting groove is of a staggered slope structure, and the other first hinge column moves in the limiting groove and can only move anticlockwise along the limiting groove.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the side of slider bottom surface is equipped with the second hinge hole, the buckle is installed in the second hinge hole, the buckle front end is hook-like structure, the base side is equipped with the hypotenuse, the laminating of buckle surface the hypotenuse just can the downthehole motion of second hinge, heat dissipation fan another side is equipped with the draw-in groove, the draw-in groove with the buckle is mutually supported.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the supporting unit is installed in the apron, including supporting seat, splint, the supporting seat bottom surface is equipped with a plurality of fixed orificess, splint simultaneously are equipped with a plurality of screw thread posts, the screw thread post with the fixed orifices cooperation is connected just splint are in along axial motion in the fixed orifices, splint with still be equipped with the second elastic component between the supporting seat, the jack-up of second elastic component splint.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the electrode is arranged on one side of the heat dissipation fan, the electrode is connected with a lead of the heat dissipation fan, an electrode connecting hole is formed in the side edge of the supporting seat, and the electrode is matched with the electrode connecting hole.
As a preferred scheme of the rapid heat dissipation radar chassis of the present invention, wherein: the side face of the box body is provided with a plug port, the heat dissipation fan is installed at the plug port, and the resilience unit and the supporting unit are matched and fixed with the heat dissipation fan.
The invention has the beneficial effects that: the invention solves the problems of heat conduction and internal and external heat exchange of a relatively dense heating main body, is convenient for replacing related structures, is convenient for maintenance and cleaning, ensures that a radar host can better conduct heat conduction, and ensures that the system can reliably work in a severe environment.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise. Wherein:
fig. 1 is an overall assembly diagram of a rapid heat dissipation radar chassis.
Fig. 2 is a structural diagram of a heat dissipation unit of a radar chassis capable of dissipating heat quickly.
Fig. 3 is an overall structure diagram of a quick-connection device of a radar case capable of quickly dissipating heat.
Fig. 4 is a connection diagram of a heat dissipation fan and a buckle of a radar case with rapid heat dissipation.
Fig. 5 is a structural diagram of a supporting unit of the rapid heat dissipation radar case.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be practiced in other ways than those specifically described and will be readily apparent to those of ordinary skill in the art without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Furthermore, reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one implementation of the invention. The appearances of the phrase "in one embodiment" in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments.
Example 1
Referring to fig. 1 and 2, a first embodiment of the present invention provides a rapid heat dissipation radar chassis that can solve the heat dissipation problem of a miniaturized, high-density chassis.
The quick-radiating radar case comprises a case 100 for mounting various parts of a radar, a radiating device 200 mounted inside the case 100, and a quick-connecting device 300 connected with the radiating device 200 in a quick-matching manner.
The enclosure 100 includes an enclosure body 101 and a ventilation unit 102.
The air exchange unit 102 comprises an air duct cover plate 102a, an air guide plate 102b and a heat dissipation plate 102c, the air guide plate 102b is of a rectangular structure with two open sides, one open side of the air guide plate 102b is connected with the air duct cover plate 102a, an air opening 102a-1 is formed in the air duct cover plate 102a, filter yarns 102a-2 are arranged in the air opening 102a-1, the heat dissipation plate 102c is of a rectangular fin structure, the heat dissipation plate is mounted at the open end of the other side of the air guide plate 102b, and fins are located inside the air guide plate 102 a. When the air duct cover plate 102a is installed, the heat dissipation plate 102c is installed firstly, the heat dissipation plate 102c is connected with the air deflector 102b, the air deflector 102b is installed between the air inlet 101a and the air outlet 101b, and finally the air duct cover plate 102a is installed outside the air deflector 102 b. The fin structure of the heat dissipation plate 102c enables the hot air in the case to be fully contacted with the metal heat dissipation plate, so that heat conduction and heat dissipation are rapidly carried out; the air deflector 102b enables air flow to uniformly pass along the heat dissipation plate 102c, and hot air backflow is reduced; the air duct cover plate 102a ensures the sealing performance of the case, only the air inlet 102a-1 is reserved for air exchange, and meanwhile, the filter gauze 102a-2 is arranged in the air inlet 102a-1 to prevent dust and other impurities from entering the case.
Further, the heat dissipating device 200 includes a heat dissipating fan 201 and a heat spreader 202, the heat dissipating fan 201 includes an air intake fan 201a and an air outlet fan 201b, an opening 102c-1 is formed at a connecting portion of one side of the heat dissipating plate 102c, the air intake fan 201a and the air outlet fan 201b are respectively mounted in close proximity to the openings 102c-1 at two ends, and the heat spreader 202 is a fin structure. The air suction fan 201a and the air outlet fan 201b are matched with each other, so that the flow of air flow in the case can be accelerated, the air cooling heat dissipation effect is better, and the heat dissipation speed is higher.
Still further, chassis body 101 includes box 101c and apron 101d, air inlet 101a and gas outlet 101b set up on box 101c, vapor chamber 201b is equipped with the polylith, set up respectively in the middle of the inside bottom surface of box 101c and apron 101d, vapor chamber 201b is last to be equipped with the power, CPU, anti-interference module, temperature sensor, transceiver module, the required module of radar such as data storage module, vapor chamber 201b fin direction is consistent with the machine case 100 direction of admitting air so that the air current takes away the heat between the vapor chamber 201b fin. The installation mode solves the problem of heat conduction of the relatively dense heating main bodies, and the heat source main bodies in the system are tiled on the system in rows and columns, so that the heat dissipation area is increased to the maximum extent; meanwhile, for the heat energy with relatively dense middle area, temperature balance can be realized through the temperature equalizing plate in time, and then heat dissipation is carried out through air cooling.
In this embodiment, the start and stop of the heat dissipation fan 201 are controlled by an internal CPU, the temperature is detected by an internal temperature sensor, and if the temperature is too high, the heat dissipation fan 201 is started to dissipate heat at the same time. When the use is finished, the heat is dissipated to the same temperature as the ambient temperature, and the heat dissipation fan 201 stops working.
Example 2
Referring to fig. 3 to 5, a second embodiment of the present invention is based on the previous embodiment, and is different from the previous embodiment in that: the general heat dissipation structure adopts a fan, and the fan is easy to be polluted by static electricity and adsorb dust in the long-term working process, and the equipment is troublesome to disassemble and clean, so the invention also comprises a quick connection device 300 which is matched and connected with the heat dissipation device 200 and comprises a rebound unit 301 and a support unit 302.
Specifically, the rebounding unit 301 is disposed in the box 101c and includes a base 301a, a slider 301b, a pull rod 301c, and a buckle 301d, the slider 301b is mounted on the base 301a, one end of the slider 301b is connected to one end of the base 301a through a first elastic element 301e, the other end of the slider 301b is provided with a limiting groove 301b-1, the other end of the base 301a is provided with a first hinge hole 301a-1, two ends of the pull rod 301c are provided with first hinges 301c-1, the first hinges 301c-1 are located on the same side, one of the first hinges is connected to the first hinge hole 301a-1 in a matching manner, the bottom surfaces of the limiting grooves 301b-1 are in a staggered slope structure, and the other first hinge column 301c-1 moves in the limiting groove 301b-1 and can only move counterclockwise along the inside of the limiting groove 301 b-1.
Further, a second hinge hole 301b-2 is formed in a side edge of the bottom surface of the slider 301b, the buckle 301d is installed in the second hinge hole 301b-2, the front end of the buckle 301d is in a hook-shaped structure, an inclined edge 301a-2 is formed in a side edge of the base 301a, and the surface of the buckle 301d is attached to the inclined edge 301a-2 and can move in the second hinge hole 301b-2
Wherein, first elastic component 301e adopts tension spring, and first articulated post 301c-1 is at the activity in-process, when sliding to recess front end middle part, under the tension spring effect, can hook whole slider 301b for slider 301b keeps fixed. Meanwhile, in the moving process of the buckle 301d, under the action of the inclined edge 301a-2, the buckle 301d moves towards the groove where the second hinge hole 301b-2 is located, a clamping groove 201c is formed in the side edge of one side of the heat dissipation fan 201, and the clamping groove 201c is matched with and buckled with the buckle 301d, so that the heat dissipation fan 201 is fixed.
In addition, the supporting unit 302 is installed in the cover plate 101d and includes a supporting seat 302a and a clamping plate 302b, a plurality of fixing holes 302a-1 are formed in a bottom surface of the supporting seat 302a, a plurality of threaded columns 302b-1 are formed in one surface of the clamping plate 302b, the threaded columns 302b-1 are connected with the fixing holes 302a-1 in a matching manner, the clamping plate 302b moves in the fixing holes 302a-1 in an axial direction, a second elastic member 302c is further arranged between the clamping plate 302b and the supporting seat 302a, and the second elastic member 302c adopts a compression spring to jack up the clamping plate 302 b.
Wherein, one side of the heat dissipation fan 201 is provided with an electrode 201d, the electrode 201d is connected with a lead of the heat dissipation fan 201, the side of the supporting seat 302a is provided with an electrode connecting hole 302a-2, and the electrode 201d is matched with the electrode connecting hole 302 a-2. The side surface of the box body 101c is provided with a plug port 101c-6, the heat dissipation fan 201 is installed from the plug port 101c-6, and the rebound unit 301 and the supporting unit 302 are matched to fix the heat dissipation fan 201.
In the embodiment, the heat dissipation fan 201 is installed into the radar case from the insertion port 101c-6 and fastened under the combined action of the rebound unit 301 and the support unit 302, and the electrode of the heat dissipation fan 201 is connected with the internal circuit of the radar case; when the heat dissipation fan 201 needs to be replaced and cleaned, the heat dissipation fan 201 is pressed inwards, the pull rod 301c moves along the limiting groove 301b-1 and returns to the original position, the heat dissipation fan 201 is connected with the rebounding unit 301 loosely, and the heat dissipation fan 201 can be pulled out for replacement.
The invention solves the problems of heat conduction and internal and external heat exchange of a relatively dense heating main body, is convenient for replacing related structures, is convenient for maintenance and cleaning, ensures that a radar host can better conduct heat conduction, and ensures that the system can reliably work in a severe environment.
It is important to note that the construction and arrangement of the present application as shown in the various exemplary embodiments is illustrative only. Although only a few embodiments have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters (e.g., temperatures, pressures, etc.), mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited in this application. For example, elements shown as integrally formed may be constructed of multiple parts or elements, the position of elements may be reversed or otherwise varied, and the nature or number of discrete elements or positions may be altered or varied. Accordingly, all such modifications are intended to be included within the scope of this invention. The order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments. In the claims, any means-plus-function clause is intended to cover the structures described herein as performing the recited function and not only structural equivalents but also equivalent structures. Other substitutions, modifications, changes and omissions may be made in the design, operating conditions and arrangement of the exemplary embodiments without departing from the scope of the present inventions. Therefore, the present invention is not limited to a particular embodiment, but extends to various modifications that nevertheless fall within the scope of the appended claims.
Moreover, in an effort to provide a concise description of the exemplary embodiments, all features of an actual implementation may not be described (i.e., those unrelated to the presently contemplated best mode of carrying out the invention, or those unrelated to enabling the invention).
It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions may be made. Such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure, without undue experimentation.
It should be noted that the above-mentioned embodiments are only for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the claims of the present invention.
Claims (10)
1. The utility model provides a quick radiating radar machine case which characterized in that: comprises the steps of (a) preparing a mixture of a plurality of raw materials,
the radar box comprises a case (100), wherein each electronic element of a radar is installed in the case (100), and the case (100) comprises a case body (101) and a ventilation unit (102); and the number of the first and second groups,
a heat sink (200) mounted inside the chassis (100) and cooperating with the ventilation unit (102); and the number of the first and second groups,
the quick connection device (300) is matched and connected with the heat dissipation device (200) and comprises a rebound unit (301) and a support unit (302).
2. The rapid thermal dissipation radar chassis of claim 1, wherein: the air-conditioning cabinet is characterized in that an air inlet (101a) and an air outlet (101b) are respectively arranged on two sides of the cabinet body (101), the air exchange unit (102) is respectively installed in the air inlet (101a) and the air outlet (101b), the air exchange unit (102) comprises an air duct cover plate (102a), an air guide plate (102b) and a heat dissipation plate (102c), the air guide plate (102b) is of a rectangular structure with two open sides, one open side of the air guide plate is connected with the air duct cover plate (102a), an air opening (102a-1) is formed in the air duct cover plate (102a), filter yarns (102a-2) are arranged in the air opening (102a-1), the heat dissipation plate (102c) is of a rectangular fin structure and is installed at the open end of the other side of the air guide plate (102 b).
3. The rapid thermal dissipation radar chassis of claim 2, wherein: the heat dissipation device (200) comprises a heat dissipation fan (201) and a soaking plate (202), the heat dissipation fan (201) comprises an air suction fan (201a) and an air outlet fan (201b), one side of the heat dissipation plate (102c) is provided with an opening (102c-1), the air suction fan (201a) and the air outlet fan (201b) are respectively installed near two end openings (102c-1), and the soaking plate (202) is of a fin structure.
4. The rapid heat dissipation radar chassis of any one of claims 1 to 3, wherein: case body (101) includes box (101c) and apron (101d), air inlet (101a) and gas outlet (101b) set up in on box (101c), soaking board (202) are equipped with the polylith, set up respectively in the middle of box (101c) and apron (101d) inside bottom surface, be equipped with the required module of radar such as power, CPU, anti-interference module, temperature sensor, transceiver module, data storage module on soaking board (202), soaking board (202) fin direction is unanimous with quick-witted case (100) business turn over gas direction.
5. The rapid thermal dissipation radar chassis of claim 4, wherein: rebound unit (301) is located in box (101c), including base (301a), slider (301b), pull rod (301c), buckle (301d), slider (301b) is installed base (301a) is gone up and the one end of slider (301b) passes through first elastic component (301e) with the one end of base (301a) links to each other, slider (301b) other end is equipped with spacing groove (301b-1), base (301a) other end is equipped with first hinge hole (301a-1), pull rod (301c) both ends are equipped with first hinge head (301c-1), first hinge head (301c-1) be located and one of them with first same one side hinge hole (301a-1) cooperation is connected.
6. The rapid thermal dissipation radar chassis of claim 5, wherein: the bottom surface of the limiting groove (301b-1) is of a staggered slope structure, and the other first hinge column (301c-1) moves in the limiting groove (301b-1) and can only move anticlockwise along the limiting groove (301 b-1).
7. The rapid thermal dissipation radar chassis of claim 6, wherein: the side of slider (301b) bottom surface is equipped with second hinge hole (301b-2), buckle (301d) is installed in second hinge hole (301b-2), buckle (301d) front end is hook-shaped structure, base (301a) side is equipped with hypotenuse (301a-2), buckle (301d) surface laminating hypotenuse (301a-2) and can second hinge hole (301b-2) internal motion, heat dissipation fan (201) another side is equipped with draw-in groove (201c), draw-in groove (201c) with buckle (301d) are mutually supported.
8. The rapid thermal dissipation radar chassis of claim 7, wherein: the supporting unit (302) is installed in the cover plate (101d), and comprises a supporting seat (302a) and a clamping plate (302b), wherein a plurality of fixing holes (302a-1) are formed in the bottom surface of the supporting seat (302a), a plurality of threaded columns (302b-1) are arranged on one surface of the clamping plate (302b), the threaded columns (302b-1) are connected with the fixing holes (302a-1) in a matched mode, the clamping plate (302b) moves in the fixing holes (302a-1) along the axial direction, a second elastic piece (302c) is further arranged between the clamping plate (302b) and the supporting seat (302a), and the clamping plate (302b) is jacked up by the second elastic piece (302 c).
9. The rapid thermal dissipation radar chassis of claim 8, wherein: one side of the heat dissipation fan (201) is provided with an electrode (201d), the electrode (201d) is connected with a lead of the heat dissipation fan (201), the side edge of the supporting seat (302a) is provided with an electrode connecting hole (302a-2), and the electrode (201d) is matched with the electrode connecting hole (302 a-2).
10. The rapid thermal dissipation radar chassis of claim 9, wherein: the side surface of the box body (101c) is provided with a plug-in port (101c-6), the heat dissipation fan (201) is installed from the plug-in port (101c-6), and the rebound unit (301) and the supporting unit (302) are matched and fixed with the heat dissipation fan (201).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110015515.9A CN112711310B (en) | 2021-01-07 | 2021-01-07 | Quick radiating radar machine case |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110015515.9A CN112711310B (en) | 2021-01-07 | 2021-01-07 | Quick radiating radar machine case |
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| CN112711310A true CN112711310A (en) | 2021-04-27 |
| CN112711310B CN112711310B (en) | 2023-11-07 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116053749A (en) * | 2023-01-31 | 2023-05-02 | 中国电子科技集团公司第三十八研究所 | Antenna array face deicing equipment and application method thereof |
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| CN112711310B (en) | 2023-11-07 |
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