CN217884260U - Heat radiation structure and satellite communication equipment - Google Patents
Heat radiation structure and satellite communication equipment Download PDFInfo
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- CN217884260U CN217884260U CN202220973022.6U CN202220973022U CN217884260U CN 217884260 U CN217884260 U CN 217884260U CN 202220973022 U CN202220973022 U CN 202220973022U CN 217884260 U CN217884260 U CN 217884260U
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- heat
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Abstract
The utility model belongs to the technical field of communication equipment, in particular to a heat dissipation structure and satellite communication equipment, which comprises a base, a shell and an upper cover which are connected in sequence, wherein the upper cover is provided with a first ventilation hole; a stepped through hole is formed in the middle of the base, and a fan is installed in the stepped through hole; a plurality of supporting platforms are annularly distributed on the inner wall of the shell, and the supporting platforms are provided with second ventilation holes; one end of the support platform, which is close to the upper cover, is connected with an annular heat conduction pipe, and the side wall of the annular heat conduction pipe is connected with heat conduction plate groups which correspond to the second vent holes one by one; the annular heat conduction pipe is further connected with cooling fins which are in one-to-one correspondence with the ventilation holes.
Description
Technical Field
The utility model belongs to the technical field of communication equipment, concretely relates to heat radiation structure and satellite communication equipment.
Background
Satellite communication equipment is widely applied to the field of communication. When the satellite communication equipment is used, internal elements of the satellite communication equipment generate heat, and if the heat is not dissipated in time, the internal elements of the satellite communication equipment are damaged. The heat radiation structure in the prior art can influence the installation of communication equipment body to also not easy dismouting maintenance after damaging.
SUMMERY OF THE UTILITY MODEL
To the above-mentioned not enough, the utility model aims at providing a heat radiation structure and satellite communication equipment.
The utility model provides a following technical scheme:
a heat dissipation structure comprises a base, a shell and an upper cover which are sequentially connected, wherein the upper cover is provided with a first ventilation hole;
a stepped through hole is formed in the middle of the base, and a fan is installed in the stepped through hole;
a plurality of supporting platforms are annularly distributed on the inner wall of the shell, and the supporting platforms are provided with second ventilation holes;
one end of the support platform, which is close to the upper cover, is connected with an annular heat conduction pipe, and the side wall of the annular heat conduction pipe is connected with heat conduction plate groups which correspond to the two vent holes one to one;
the annular heat conduction pipe is further connected with cooling fins which are in one-to-one correspondence with the ventilation holes.
And one end of the annular heat conducting pipe, which is close to the upper cover, is provided with a plurality of slots, and the radiating fins are spliced with the annular heat conducting pipe.
A third ventilation hole is formed in the shell on one side of the radiating fin; and a third dust screen is arranged on the inner side of the third ventilation hole.
The inner side of the first ventilation hole is provided with a first dust screen.
The shell positioned at one side of the support platform close to the base is internally provided with a funnel-shaped air deflector.
Be located the fan and deviate from the ladder through-hole of shell one side and install the baffle, be the annular on the baffle and laid a plurality of ventilation hole four, ventilation hole four inboard is installed dust screen four.
The utility model provides a satellite communication equipment, still includes the equipment body of being connected with a platform, and the equipment body is close to upper cover one side and installs heat conduction copper pipe, and heat conduction copper pipe is connected with annular heat pipe through the heat conduction strip.
The utility model has the advantages that:
the utility model discloses an install the communication equipment body in the shell to set up independent annular heat pipe with the heat conduction copper pipe in through heat conduction strip and the shell and be connected, when can avoiding installing the radiating part, cause the influence to communication equipment. The utility model discloses an install the fan in the ladder through-hole of base, can conveniently change the fan, the utility model discloses a set up infundibulate aviation baffle, heat conduction piece group and fin, can improve ventilation cooling performance.
Drawings
Fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a top view of the baffle;
fig. 3 is a plan view of the annular heat conductive pipe.
Labeled in the figure as: the air conditioner comprises a base 101, a baffle plate 102, a vent hole four 103, a dust screen four 104, a fan 105, a funnel-shaped air deflector 106, a shell 107, an equipment body 108, a vent hole three 109, a dust screen three 110, a dust screen one 111, a vent hole one 112, an upper cover 113, a vent hole two 201, a support 202, a cooling fin 203, a heat conducting fin group 204, an annular heat conducting pipe 205, a heat conducting copper pipe 206, a heat conducting strip 207 and a slot 208.
Detailed Description
As shown in the figure, the heat dissipation structure comprises a base 101, a shell 107 and an upper cover 113 which are connected in sequence, wherein the base 101, the shell 107 and the upper cover 113 are all connected through bolts, so that the heat dissipation structure is convenient to disassemble. The upper cover 113 is provided with a first vent hole 112, and the first vent holes 112 are arranged in a ring shape. And a first dust screen 111 is arranged on the inner side of the first ventilation hole 112.
A plurality of support platforms 202 are annularly arranged on the inner wall of the shell 107, and the support platforms 202 are provided with a second ventilation hole 201. One end of the support 202 close to the upper cover 113 is connected with an annular heat conduction pipe 205, and the side wall of the annular heat conduction pipe 205 is connected with heat conduction plate groups 204 which are in one-to-one correspondence with the second air vents 201. The housing 107 on the side of the support 202 adjacent to the base 101 has a funnel-shaped air deflector 106 mounted therein. The cold air pumped by the fan 105 is blown into the second air vent 201, and the cold air is blown through the heat conducting plate group 204, so that heat dissipation is performed.
The annular heat conductive pipe 205 is also connected with the cooling fins 203 which correspond to the first ventilation holes 112 one by one. Specifically, a plurality of slots 208 are formed at one end of the annular heat conducting pipe 205 close to the upper cover 113, and the heat sink 203 is inserted into the annular heat conducting pipe 205. The heat sink 203 may also function to dissipate heat. By inserting the heat radiating fins 203 into the annular heat conductive pipes 205, it is possible to facilitate the installation or replacement of the heat radiating fins 203.
The housing 107 on the side of the heat sink 203 is provided with a third ventilation hole 109, and the inner side of the third ventilation hole 109 is provided with a third dust screen 110. By providing the third vent 109, the heat dissipation effect can be improved.
A satellite communication device comprises the heat dissipation structure; the device further comprises a device body 108 connected with the support 202, wherein a heat conducting copper pipe 206 is installed on one side, close to the upper cover 113, of the device body 108, and the heat conducting copper pipe 206 is connected with an annular heat conducting pipe 205 through a heat conducting strip 207.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described above, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. A heat dissipation structure comprises a base (101), a shell (107) and an upper cover (113) which are sequentially connected, wherein the upper cover (113) is provided with a first ventilation hole (112); the method is characterized in that:
a stepped through hole is formed in the center of the base (101), and a fan (105) is installed in the stepped through hole;
a plurality of supporting platforms (202) are annularly arranged on the inner wall of the shell (107), and the supporting platforms (202) are provided with second ventilation holes (201);
one end of the support (202), which is close to the upper cover (113), is connected with an annular heat-conducting pipe (205), and the side wall of the annular heat-conducting pipe (205) is connected with heat-conducting pipe groups (204) which correspond to the second vent holes (201) one by one;
the annular heat conduction pipe (205) is also connected with cooling fins (203) which correspond to the first ventilation holes (112) one by one.
2. The heat dissipation structure of claim 1, wherein: a plurality of slots (208) are formed in one end, close to the upper cover (113), of the annular heat conduction pipe (205), and the radiating fins (203) are inserted into the annular heat conduction pipe (205).
3. The heat dissipation structure according to claim 2, wherein: a third vent hole (109) is arranged on the shell (107) positioned on one side of the radiating fin (203); and a third dust screen (110) is arranged on the inner side of the third ventilation hole (109).
4. The heat dissipation structure according to claim 1, wherein: the inner side of the first ventilation hole (112) is provided with a first dust screen (111).
5. The heat dissipation structure according to claim 1, wherein: a funnel-shaped air deflector (106) is arranged in the shell (107) which is positioned on one side of the support platform (202) close to the base (101).
6. The heat dissipation structure of claim 1, wherein: and a baffle (102) is arranged in the stepped through hole on one side of the fan (105) departing from the shell (107), a plurality of four ventilation holes (103) are annularly distributed on the baffle (102), and a dust screen four (104) is arranged on the inner side of the four ventilation holes (103).
7. A satellite communication device, characterized by: comprising the heat dissipation structure as recited in any one of claims 1 to 6; the device is characterized by further comprising a device body (108) connected with the supporting platform (202), wherein a heat conducting copper pipe (206) is installed on one side, close to the upper cover (113), of the device body (108), and the heat conducting copper pipe (206) is connected with an annular heat conducting pipe (205) through a heat conducting strip (207).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220973022.6U CN217884260U (en) | 2022-04-25 | 2022-04-25 | Heat radiation structure and satellite communication equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220973022.6U CN217884260U (en) | 2022-04-25 | 2022-04-25 | Heat radiation structure and satellite communication equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217884260U true CN217884260U (en) | 2022-11-22 |
Family
ID=84087657
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220973022.6U Active CN217884260U (en) | 2022-04-25 | 2022-04-25 | Heat radiation structure and satellite communication equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217884260U (en) |
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2022
- 2022-04-25 CN CN202220973022.6U patent/CN217884260U/en active Active
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