CN209949768U - Heat dissipation device for aerospace transmitter based on phase-change heat storage material - Google Patents
Heat dissipation device for aerospace transmitter based on phase-change heat storage material Download PDFInfo
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- CN209949768U CN209949768U CN201920681227.5U CN201920681227U CN209949768U CN 209949768 U CN209949768 U CN 209949768U CN 201920681227 U CN201920681227 U CN 201920681227U CN 209949768 U CN209949768 U CN 209949768U
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- transmitter based
- storage material
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Abstract
The utility model discloses a heat abstractor for aerospace transmitter based on phase transition heat-retaining material, including base, water pump and slider, both ends are provided with at a distance from the cavity about the inside of base, and separate the middle part fixed mounting that the cavity was indoor and have the reservoir chamber, the top of base is connected with placing the board through first spring, and the surface of placing the board is connected with places the board to both ends are fixed with the slider about placing the board, both ends are fixed with the curb plate about the top of base, the fixed surface of curb plate has the dead lever, and is connected with fixed frame on the dead lever to be provided with the protection strip on the fixed frame, the surface of placing the board is provided with the heat dissipation pad. This heat abstractor for aerospace transmitter based on phase transition heat-retaining material is provided with the cooling pad of phase transition heat-retaining material, can absorb the heat that the transmitter bottom produced conveniently in the cooling pad, and the convenient absorption to transmitter bottom heat has made things convenient for the heat dissipation of transmitter.
Description
Technical Field
The utility model relates to an aerospace transmitter technical field specifically is a heat abstractor for aerospace transmitter based on phase transition heat-retaining material.
Background
The transmitter is a device capable of transmitting signals according to a certain frequency, and is widely applied to the fields of televisions, broadcasting, aerospace and the like, and the transmitter can generate a large amount of heat during working, so that the transmitter needs to be matched with a heat dissipation device for use;
for the existing heat dissipation device for the aerospace transmitter, a great part of problems still exist, such as poor heat dissipation effect, inconvenience in fixing the transmitter, no damping function and influence on the use effect of the heat dissipation device, so that the heat dissipation device for the aerospace transmitter based on the phase change heat storage material is provided so as to solve the problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a heat abstractor for aerospace transmitter based on phase transition heat-retaining material to it is not good to solve the radiating effect that above-mentioned background art provided current heat abstractor, and the fixing of inconvenient transmitter does not have shock-absorbing function, influences heat abstractor's result of use's problem.
In order to achieve the above object, the utility model provides a following technical scheme: a heat dissipation device for an aerospace transmitter based on a phase change heat storage material comprises a base, a water pump and sliders, wherein the left end and the right end of the inside of the base are provided with a separation chamber, the middle part of the separation chamber is fixedly provided with a water storage chamber, the upper part of the base is connected with a placing plate through a first spring, the surface of the placing plate is connected with the placing plate, the left end and the right end of the placing plate are fixedly provided with the sliders, the left end and the right end of the upper part of the base are fixedly provided with side plates, the right side surfaces of the side plates are provided with heat dissipation holes, the lower surfaces of the side plates are provided with sliding chutes, the inside of each side plate is provided with a condensation pipe, one end of each condensation pipe is connected with the water storage chamber, the other end of each condensation pipe is connected with the output end of the water pump, the water pump, and the fixed rod is connected with a fixed frame, the fixed frame is provided with a protection strip, and the surface of the placing plate is provided with a heat dissipation pad.
Preferably, the two ends of the placing plate form a sliding structure in clamping connection with the sliding grooves at the bottoms of the side plates through the sliding blocks, and the placing plate forms an elastic structure with the base through the first spring.
Preferably, the inside of curb plate is hollow column structure, and the surface evenly distributed of curb plate has the louvre.
Preferably, the condenser pipe is of a bent structure, the condenser pipe is connected with the fixing sleeve in a sleeved mode, and the fixing sleeve is fixedly installed at the top end inside the side plate.
Preferably, the condenser pipe, the water pump and the water storage chamber form a water cooling mechanism, and the condenser pipe is in rigid connection with the water storage chamber.
Preferably, the fixing rod comprises a first rod body, a second rod body and a second spring, the second spring is connected between the first rod body and the second rod body, and the second rod body and the first rod body form a telescopic structure through the second spring.
Preferably, the dead lever is welded connection with the connected mode of fixed frame, and fixed frame is "mouth" font structure to the connected mode of fixed frame and protection strip is adhesive bonding, and the protection strip adopts the rubber material simultaneously.
Preferably, the cooling pad is of a circular structure, the cooling pad is uniformly distributed on the upper surface of the placing plate, and the placing plate is made of a phase-change heat storage material.
Compared with the prior art, the beneficial effects of the utility model are that: the heat dissipation device for the aerospace transmitter based on the phase-change heat storage material,
(1) the heat dissipation pad provided with the phase-change heat storage material can absorb heat generated at the bottom of the transmitter into the heat dissipation pad conveniently, so that the heat generated at the bottom of the transmitter can be absorbed conveniently, the heat dissipation of the transmitter is facilitated, and meanwhile, the heat dissipation pad is matched with a water cooling mechanism formed by a water pump and a condensation pipe to be used, so that the cooling and heat dissipation of two sides of the transmitter are facilitated, and the heat dissipation effect of the device is further improved;
(2) the fixing rod and the fixing frame are arranged, so that the transmitter can be conveniently fixed through the telescopic structure formed by the first rod body and the second rod body on the fixing rod, and the working stability of the transmitter is improved;
(3) be provided with first spring, can place the vibrations that the board was gone up to transmitter work produced through the effectual buffering of first spring, and then make things convenient for the device to carry out the shock attenuation to the transmitter, improve the life of transmitter.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic side sectional view of the side plate of the present invention;
FIG. 3 is a schematic view of the side plate surface structure of the present invention;
FIG. 4 is a schematic view of the structure of the placing plate surface of the present invention;
fig. 5 is a schematic view of the fixing rod structure of the present invention.
In the figure: 1. a base; 2. a compartment; 3. a water storage chamber; 4. placing the plate; 5. a first spring; 6. a side plate; 7. heat dissipation holes; 8. a chute; 9. a condenser tube; 10. fixing a sleeve; 11. a water pump; 12. fixing the rod; 121. a first rod body; 122. a second rod body; 123. a second spring; 13. a fixing frame; 14. a protective strip; 15. a heat dissipation pad; 16. a slide block.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: a heat dissipation device for an aerospace transmitter based on a phase change heat storage material comprises a base 1, a separation chamber 2, a water storage chamber 3, a placing plate 4, a first spring 5, side plates 6, heat dissipation holes 7, a sliding groove 8, a condensation pipe 9, a fixing sleeve 10, a water pump 11, a fixing rod 12, a first rod body 121, a second rod body 122, a second spring 123, a fixing frame 13, a protection strip 14, a heat dissipation pad 15 and a sliding block 16, wherein the separation chamber 2 is arranged at the left end and the right end of the inside of the base 1, the water storage chamber 3 is fixedly arranged in the middle of the separation chamber 2, the upper portion of the base 1 is connected with the placing plate 4 through the first spring 5, the placing plate 4 is connected with the surface of the placing plate 4, the heat dissipation holes 16 are fixed at the left end and the right end of the placing plate 4, the side plates 6 are fixed at the left end and the right end of the upper portion of the base, the internally mounted of curb plate 6 has condenser pipe 9, and the one end of condenser pipe 9 is connected with reservoir chamber 3, and the other end of condenser pipe 9 is connected with the output of water pump 11, 11 fixed mounting of water pump are in the bottom that separates cavity 2, and the other end of water pump 11 is put through with reservoir chamber 3 mutually, the fixed surface of curb plate 6 has dead lever 12, and be connected with fixed frame 13 on the dead lever 12, and be provided with protection strip 14 on the fixed frame 13, the surface of placing board 4 is provided with the cooling pad 15.
The two ends of the placing plate 4 form a sliding structure connected with the side plate 6 through the sliding blocks 16 and the sliding grooves 8 at the bottoms of the side plates in a clamping mode, the placing plate 4 forms an elastic structure with the base 1 through the first springs 5, and vibration generated by the operation of the transmitter on the placing plate 4 is effectively buffered.
The inside of curb plate 6 is hollow column structure, and the surface evenly distributed of curb plate 6 has louvre 7, has made things convenient for the effluvium of air conditioning.
The fixing rod 12 includes a first rod 121, a second rod 122 and a second spring 123, the second spring 123 is connected between the first rod 121 and the second rod 122, and the second rod 122 and the first rod 121 form a telescopic structure through the second spring 123, so as to facilitate the extension and retraction of the fixing frame 13.
The connected mode of dead lever 12 and fixed frame 13 is welded connection, and fixed frame 13 is "mouth" font structure to fixed frame 13 is adhesive bonding with the connected mode of protection strip 14, and protection strip 14 adopts the rubber material simultaneously, can be through the effectual fixed transmitter of the protection strip 14 on fixed frame 13 surface.
The cooling pad 15 is circular structure, and the even distribution of cooling pad 15 is at the upper surface of placing board 4 to place board 4 and adopt the phase transition heat-retaining material, conveniently dispel the heat to the bottom of transmitter.
The working principle is as follows: firstly, as shown in fig. 1-5, when in use, the device is firstly connected with an external power supply, then the aerospace transmitter to be used is placed on the placing plate 4, when in placement, the fixing frame 13 at the end of the fixing rod 12 fixed on the inner side of the side plate 6 can make the fixing frame 13 fix both sides of the transmitter under the action of the second spring 123, thereby facilitating the stable use of the transmitter, when the transmitter works, the water pump 11 can be opened, the water pump 11 can lead the water in the water storage chamber 3 into the condenser pipe 9, and further the condenser pipe 9 can discharge the water into the water storage chamber 3 again, thereby achieving the water cooling effect, and then the generated cold air can be discharged through the heat dissipation holes 7 on the surface of the side plate 6 to dissipate the surface of the transmitter, the heat dissipation pads 15 uniformly distributed on the surface of the placing plate 4 are made of phase-change heat storage materials, which can effectively absorb the heat of the transmitting part, and improve the heat dissipation effect of the device, place and distribute first spring 5 between board 4 and base 1, can place the vibration that the transmitter work produced on board 4 through the effectual buffering of first spring 5, and then improved the device's shock attenuation effect, improved the life of transmitter, this is this heat abstractor for aerospace transmitter based on phase change heat-retaining material's theory of use, and the content that does not do detailed description in this specification belongs to the known prior art of the professional skilled in the art.
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 or portions thereof without departing from the spirit and scope of the invention.
Claims (8)
1. The utility model provides a heat abstractor for aerospace transmitter based on phase transition heat-retaining material, includes base (1), water pump (11) and slider (16), its characterized in that: the water storage and refrigeration device is characterized in that the left end and the right end inside the base (1) are provided with a separation chamber (2), the middle of the separation chamber (2) is fixedly provided with a water storage chamber (3), the upper part of the base (1) is connected with a placing plate (4) through a first spring (5), the surface of the placing plate (4) is connected with the placing plate (4), the left end and the right end of the placing plate (4) are fixedly provided with sliders (16), the left end and the right end above the base (1) are fixedly provided with side plates (6), the right side surface of each side plate (6) is provided with a heat dissipation hole (7), the lower surface of each side plate (6) is provided with a sliding chute (8), a condensation pipe (9) is installed inside each side plate (6), one end of each condensation pipe (9) is connected with the water storage chamber (3), the other end of each condensation pipe (9) is connected with the output end of a water pump (11), and, and the other end of water pump (11) and reservoir chamber (3) switch-on mutually, the fixed surface of curb plate (6) has dead lever (12), and is connected with fixed frame (13) on dead lever (12) to be provided with protective strip (14) on fixed frame (13), the surface of placing board (4) is provided with radiating pad (15).
2. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: the two ends of the placing plate (4) form a sliding structure in clamping connection with the sliding grooves (8) at the bottoms of the side plates (6) through the sliding blocks (16), and the placing plate (4) forms an elastic structure with the base (1) through the first springs (5).
3. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: the interior of the side plate (6) is of a hollow structure, and heat dissipation holes (7) are uniformly distributed in the surface of the side plate (6).
4. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: condenser pipe (9) are crooked column structure, and condenser pipe (9) are for cup jointing with fixed cover (10) and are connected to fixed cover (10) fixed mounting is on curb plate (6) inside top.
5. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: condenser pipe (9), water pump (11) and reservoir chamber (3) constitute water-cooling mechanism, and condenser pipe (9) and reservoir chamber (3) are rigid connection.
6. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: the fixing rod (12) comprises a first rod body (121), a second rod body (122) and a second spring (123), the second spring (123) is connected between the first rod body (121) and the second rod body (122), and the second rod body (122) and the first rod body (121) form a telescopic structure through the second spring (123).
7. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: the connection mode of dead lever (12) and fixed frame (13) is welded connection, and fixed frame (13) are "mouth" font structure to the connection mode of fixed frame (13) and protection strip (14) is adhesive bonding, and protection strip (14) adopt the rubber material simultaneously.
8. The heat dissipation device for the aerospace transmitter based on the phase-change heat storage material as claimed in claim 1, wherein: the radiating pad (15) is of a circular structure, the radiating pad (15) is uniformly distributed on the upper surface of the placing plate (4), and the placing plate (4) is made of a phase-change heat storage material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920681227.5U CN209949768U (en) | 2019-05-13 | 2019-05-13 | Heat dissipation device for aerospace transmitter based on phase-change heat storage material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920681227.5U CN209949768U (en) | 2019-05-13 | 2019-05-13 | Heat dissipation device for aerospace transmitter based on phase-change heat storage material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209949768U true CN209949768U (en) | 2020-01-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920681227.5U Active CN209949768U (en) | 2019-05-13 | 2019-05-13 | Heat dissipation device for aerospace transmitter based on phase-change heat storage material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209949768U (en) |
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2019
- 2019-05-13 CN CN201920681227.5U patent/CN209949768U/en active Active
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