CN218662422U - Waterproof unmanned aerial vehicle with heat radiation structure - Google Patents
Waterproof unmanned aerial vehicle with heat radiation structure Download PDFInfo
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- CN218662422U CN218662422U CN202223251227.2U CN202223251227U CN218662422U CN 218662422 U CN218662422 U CN 218662422U CN 202223251227 U CN202223251227 U CN 202223251227U CN 218662422 U CN218662422 U CN 218662422U
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- aerial vehicle
- unmanned aerial
- heat radiation
- radiation structure
- heat dissipation
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Abstract
The utility model discloses a waterproof unmanned aerial vehicle with heat radiation structure, including the sealed main casing body and the electronic component of setting in main casing internal portion, be equipped with at least one windowing on the main casing body, windowing department inlays and is equipped with radiator unit, radiator unit contradicts electronic component. This waterproof unmanned aerial vehicle with heat radiation structure, through set up radiator unit on the main casing body of unmanned aerial vehicle, for the inside electronic component (if control electroplax) heat dissipation of unmanned aerial vehicle, compare in the fan heat dissipation among the prior art, it need not inside the air current organism to set up radiator unit, can not influence the water-proof effects of organism, and simultaneously, radiator unit has effectively avoided electronic component to cause the damage because of the high temperature, is favorable to promoting unmanned aerial vehicle's life.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a waterproof unmanned aerial vehicle with heat radiation structure.
Background
Unmanned aerial vehicle is called unmanned aerial vehicle for short, utilize radio remote control equipment and the unmanned aerial vehicle that the program control device of self-contained was controlled, along with the miniaturized requirement of unmanned aerial vehicle, and functional stronger and stronger, unmanned aerial vehicle is littleer and smaller, when the structure is compacter and more, but more and more components and parts, especially some electronic component, have very big calorific capacity, generally through add the fan among the prior art and accelerate the circulation of air, realize the heat dissipation, but this kind of method can cause harmful effects to the water-proof effects of organism, can't be applied to on the waterproof unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem that will solve is: the utility model provides a waterproof unmanned aerial vehicle with heat radiation structure.
In order to solve the technical problem, the utility model discloses a technical scheme be: the utility model provides a waterproof unmanned aerial vehicle with heat radiation structure, includes the sealed main casing body and sets up the electronic component in main casing body inside, be equipped with at least one windowing on the main casing body, windowing department inlays and is equipped with radiator unit, radiator unit contradicts electronic component.
Further, the fenestration is arranged close to the windward side of the main shell.
Further, the window is disposed at the front side of the main housing and/or at the upper side of the main housing.
Furthermore, the contact part of the heat dissipation component and the electronic element is coated with heat dissipation silica gel.
Further, the heat dissipation assembly is detachably connected with the main shell.
Further, a sealing ring is arranged between the heat dissipation assembly and the main shell.
Further, a fixing support is mounted inside the main housing, and the electronic element is mounted on the fixing support.
Further, the fixed bolster is equipped with the installation department, the fixed bolster passes through the installation department with main casing body coupling.
Furthermore, the fixed support is in a hollow rectangular frame shape.
Further, the main casing body includes integral type injection moulding's last casing and integral type injection moulding's lower casing, go up the casing with inferior valve body coupling, go up the casing with be equipped with seal structure down between the casing.
The beneficial effects of the utility model reside in that: this waterproof unmanned aerial vehicle with heat radiation structure, through set up radiator unit on the unmanned aerial vehicle main casing body, for the inside electronic component heat dissipation of unmanned aerial vehicle, compare in the fan heat dissipation among the prior art, set up inside radiator unit need not the air current and advances the organism, can not influence the water-proof effects of organism, and simultaneously, radiator unit has effectively avoided electronic component to cause the damage because of the high temperature, is favorable to promoting unmanned aerial vehicle's life.
Drawings
Fig. 1 is a schematic structural view of a waterproof unmanned aerial vehicle with a heat dissipation structure in a first embodiment of the present invention;
fig. 2 is a schematic structural view of a lower shell of a waterproof unmanned aerial vehicle with a heat dissipation structure in a first embodiment of the present invention;
fig. 3 is the embodiment of the utility model provides a have heat radiation structure's waterproof unmanned aerial vehicle's fixed bolster's in the first structural sketch.
Description of reference numerals:
1. a main housing; 11. an upper housing; 12. a lower housing; 13. windowing;
2. a heat dissipating component; 21. a contact surface;
3. fixing a bracket; 31. an installation part.
Detailed Description
In order to explain the technical content, the objects and the effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.
Referring to fig. 1 to 3, a waterproof unmanned aerial vehicle with a heat dissipation structure includes a sealed main housing 1 and an electronic component disposed inside the main housing 1, at least one window 13 is disposed on the main housing 1, a heat dissipation assembly 2 is embedded at the window 13, and the heat dissipation assembly 2 abuts against the electronic component.
The utility model discloses a structural principle brief follows as follows: set up the radiator unit 2 that runs through main casing body 1 on main casing body 1 to make radiator unit 2 contradict with the radiating electronic component of needs, the heat transfer that makes electronic component produce gives radiator unit 2, and unmanned aerial vehicle is when the flight, and the air current of windward side can be for radiator unit 2 cooling, thereby the indirect electronic component cooling that is inside.
From the above description, the beneficial effects of the present invention are: this waterproof unmanned aerial vehicle with heat radiation structure, through set up radiator unit on the unmanned aerial vehicle main casing body, for the inside electronic component heat dissipation of unmanned aerial vehicle, compare in the fan heat dissipation among the prior art, set up inside radiator unit need not the air current and advances the organism, can not influence the water-proof effects of organism, and simultaneously, radiator unit has effectively avoided electronic component to cause the damage because of the high temperature, is favorable to promoting unmanned aerial vehicle's life.
Further, the window 13 is disposed near the windward side of the main housing 1.
According to the description, the air flow speed of the windward side is higher, and the heat dissipation effect is better.
Further, the window is disposed at the front side of the main housing and/or at the upper side of the main housing.
As can be seen from the description, the front side and the upper side of the main shell are both close to the windward side, so that the air flow speed is high, and the heat dissipation effect is good.
Furthermore, the contact part of the heat dissipation component 2 and the electronic element is coated with heat dissipation silica gel.
From the above description, the heat-dissipating silica gel is beneficial to heat transfer and enhancing the heat-dissipating effect of the heat-dissipating component.
Further, the heat dissipation assembly 2 is detachably connected to the main housing 1.
As can be seen from the above description, the detachable connection of the heat dissipation assembly to the main housing facilitates the maintenance and replacement of the heat dissipation assembly.
Further, a sealing ring is installed between the heat dissipation assembly 2 and the main casing 1.
According to the above description, the sealing ring is arranged, so that the sealing performance of the window opening position is improved, and the waterproof performance of the machine body is improved.
Further, a fixing bracket 3 is installed inside the main housing 1, and the electronic component is installed on the fixing bracket 3.
As can be seen from the above description, the fixing bracket is used for fixing an electronic component.
Further, the fixed bracket 3 is provided with an installation part 31, and the fixed bracket 3 is connected with the main casing 1 through the installation part 31.
Furthermore, the fixed support is in a hollow rectangular frame shape.
As can be seen from the description, the fixing bracket is simple in structure and convenient to use.
Further, the main casing body includes integral type injection moulding's last casing and integral type injection moulding's lower casing, go up the casing with inferior valve body coupling, go up the casing with be equipped with seal structure down between the casing.
According to the description, the main shell is simple in structure and good in sealing and waterproof performance, the die is saved, and the production cost of the main shell is reduced.
Example one
Referring to fig. 1 to fig. 3, a first embodiment of the present invention is: the utility model provides a waterproof unmanned aerial vehicle with heat radiation structure, includes sealed main casing body 1 and sets up the electronic component in main casing body 1 inside, main casing body 1 includes integral type injection moulding's last casing 11 and integral type injection moulding's lower casing 12, go up casing 11 with casing 12 passes through the fastener and connects down, go up casing 11 with be equipped with seal structure down between casing 12, go up casing 11 with form airtight cavity down between casing 12, electronic component sets up the inside of main casing body 1's airtight cavity, be equipped with at least one 13 of windowing on the main casing body 1, 13 departments of windowing inlay and be equipped with radiator unit 2, radiator unit 2 contradicts electronic component, in this embodiment, radiator unit 2 has contact surface 21, contact surface 21 passes through 13 of windowing stretches into inside main casing body 1, contact surface 21 contradicts electronic component.
Optionally, the heat dissipation assembly 2 is a heat dissipation block or a heat dissipation fin, in this embodiment, the heat dissipation assembly 2 is a heat dissipation block, and in order to improve the heat dissipation capability of the heat dissipation block, the outer surface of the heat dissipation block is further provided with heat dissipation grooves or heat dissipation patterns.
Referring to fig. 1, the windows 13 are disposed on the front side of the main housing 1 and/or the upper side of the main housing 1, in this embodiment, the windows 13 are disposed near the windward side of the main housing 1, the number of the windows 13 is two, one of the windows is disposed on the front side of the lower housing 12, the other window 13 is disposed above the upper housing 11, one of the heat dissipation assemblies 2 is embedded in each of the windows 13, in other embodiments, the number of the windows 13 may be one, and the windows 13 are disposed on the front side of the lower housing 12 or the upper side of the upper housing 11.
In this embodiment, in order to further improve the heat dissipation effect of the heat dissipation assembly 2 on the electronic component, the contact position between the heat dissipation assembly 2 and the electronic component is coated with heat dissipation silica gel, and in other embodiments, the heat dissipation assembly 2 and the electronic component may also be selectively provided with other heat dissipation media or directly contacted.
In this embodiment, the electronic component includes, but is not limited to, a WIFI module, an MCU module, and the like.
Referring to fig. 1 and 2, the heat dissipation assembly 2 is detachably connected to the main housing 1, in this embodiment, an installation hole is formed in an edge of the heat dissipation assembly 2, and the heat dissipation assembly 2 is installed on the main housing 1 by a screw penetrating through the installation hole, in other embodiments, optionally, the connection mode between the heat dissipation assembly 2 and the main housing 1 is riveting, welding or plugging connection.
The heat dissipation assembly 2 with install the sealing washer between the main casing body 1, it is optional, the sealing washer is rubber seal, latex seal etc. in other embodiments, heat dissipation assembly 2 with sealed glue also can be filled between the main casing body 1.
Referring to fig. 2, a fixing support 3 is installed inside the main housing 1, the electronic component is installed on the fixing support 3, and optionally, the electronic component and the fixing support 3 are connected by riveting, fastening, screwing or gluing, in this embodiment, the fixing support 3 is in a rectangular frame shape, the fixing support 3 is disposed on the lower housing 12, the fixing support 3 is disposed near the heat dissipation assembly 2, the fixing support 3 and the electronic component are connected by fastening, and the edge of the fixing support 3 is provided with a side fastener and an end fastener for fixing the electronic component.
Referring to fig. 3, the fixing bracket 3 is provided with an installation portion 31, the fixing bracket 3 is connected to the main housing 1 through the installation portion 31, in this embodiment, two ends of the fixing bracket 3 are provided with four fixing bolt seats, and the fixing bracket 3 is installed on the main housing 1 through bolts pressing the fixing bolt seats.
To sum up, the waterproof unmanned aerial vehicle with the heat dissipation structure provided by the utility model has the advantages that the heat dissipation assembly is arranged on the main shell of the unmanned aerial vehicle, so that the electronic elements in the unmanned aerial vehicle can dissipate heat, compared with the fan heat dissipation in the prior art, the heat dissipation assembly is arranged without air flowing into the unmanned aerial vehicle body, the waterproof effect of the unmanned aerial vehicle body cannot be influenced, meanwhile, the heat dissipation assembly effectively avoids the damage of the electronic elements caused by overhigh temperature, and the service life of the unmanned aerial vehicle is prolonged; the main shell is reasonable in structure, low in production difficulty, good in sealing and waterproof performance and high in reliability.
The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (10)
1. The utility model provides a waterproof unmanned aerial vehicle with heat radiation structure, its characterized in that: including sealed main casing body and the electronic component who sets up in main casing body inside, be equipped with at least one windowing on the main casing body, windowing department inlays and is equipped with radiator unit, radiator unit contradicts electronic component.
2. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: the windowing is arranged close to the windward side of the main shell.
3. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: the window is disposed at a front side of the main housing and/or an upper side of the main housing.
4. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: the heat dissipation assembly is coated with heat dissipation silica gel at the position where the heat dissipation assembly abuts against the electronic element.
5. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: the heat dissipation assembly is detachably connected with the main shell.
6. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: and a sealing ring is arranged between the heat dissipation assembly and the main shell.
7. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: the main casing body internally mounted has the fixed bolster, electronic component installs on the fixed bolster.
8. The waterproof unmanned aerial vehicle with heat radiation structure of claim 7, characterized in that: the fixed bolster is equipped with the installation department, the fixed bolster passes through the installation department with main casing body coupling.
9. The waterproof unmanned aerial vehicle with heat radiation structure of claim 7, characterized in that: the fixed support is in a hollow rectangular frame shape.
10. The waterproof unmanned aerial vehicle with heat radiation structure of claim 1, characterized in that: the main casing body includes integral type injection moulding's last casing and integral type injection moulding's lower casing, go up the casing with inferior valve body coupling, go up the casing with be equipped with seal structure down between the casing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223251227.2U CN218662422U (en) | 2022-12-05 | 2022-12-05 | Waterproof unmanned aerial vehicle with heat radiation structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223251227.2U CN218662422U (en) | 2022-12-05 | 2022-12-05 | Waterproof unmanned aerial vehicle with heat radiation structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218662422U true CN218662422U (en) | 2023-03-21 |
Family
ID=85548276
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223251227.2U Active CN218662422U (en) | 2022-12-05 | 2022-12-05 | Waterproof unmanned aerial vehicle with heat radiation structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218662422U (en) |
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2022
- 2022-12-05 CN CN202223251227.2U patent/CN218662422U/en active Active
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