CN210840492U - Heat dissipation device for airborne equipment of unmanned aerial vehicle - Google Patents
Heat dissipation device for airborne equipment of unmanned aerial vehicle Download PDFInfo
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- CN210840492U CN210840492U CN201921736061.9U CN201921736061U CN210840492U CN 210840492 U CN210840492 U CN 210840492U CN 201921736061 U CN201921736061 U CN 201921736061U CN 210840492 U CN210840492 U CN 210840492U
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- radiating fin
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Abstract
The utility model discloses a heat abstractor for unmanned aerial vehicle airborne equipment, including radiator upper fixed plate, fan and vertical flexible post, the upper end that copper aluminium combines the fin is provided with radiator upper fixed plate, and the lower extreme that copper aluminium combines the fin is provided with fin bottom plate, the upper end of radiator upper fixed plate is fixed with the fixed foot of fan, and the upper end four corners of the fixed foot of fan is provided with the fan bolt, the upper end of fan bolt is connected with the fan. This a heat abstractor for unmanned aerial vehicle airborne equipment is provided with horizontal flexible post and fin bottom plate and is the level form and distributes, and the effective working range of radiator is guaranteed in flexible structural design, can install on the equipment of variation in size and shape, and the bolt that the cooperation was provided with improves the fastness that the radiator need carry out the heat abstractor in the installation, the condition that unmanned aerial vehicle can drop at flight in-process heat abstractor can not appear.
Description
Technical Field
The utility model relates to a heat abstractor technical field of unmanned aerial vehicle airborne equipment specifically is a heat abstractor for unmanned aerial vehicle airborne equipment.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle controlled by a radio remote control device or an onboard computer program control system. The equipment can generate heat in the operation process, the size of the heat generated according to the size and the power of the equipment is different, if the generated heat cannot be timely discharged, the equipment can be greatly influenced, the service life of the equipment can be shortened, and the heat radiator can solve the problem.
The heat abstractor of unmanned aerial vehicle airborne equipment in market installs very loaded down with trivial details and the equipment size that can install also receives the restriction and can only be applicable to the problem of some unmanned aerial vehicle airborne equipment, for this reason, we propose the heat abstractor of unmanned aerial vehicle airborne equipment of installation application scope extensive of being convenient for.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a heat abstractor for unmanned aerial vehicle airborne equipment to solve the problem that the heat abstractor installation of the unmanned aerial vehicle airborne equipment that proposes in the above-mentioned background very loaded down with trivial details and the equipment size that can install also received the restriction and can only be applicable to partly unmanned aerial vehicle airborne equipment.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a heat abstractor for unmanned aerial vehicle airborne equipment, includes fixed plate, fan and the vertical flexible post on the fin, the upper end that copper aluminium combines the fin is provided with the fixed plate on the fin, and the lower extreme that copper aluminium combines the fin is provided with fin bottom plate, the upper end of fixed plate is fixed with the fixed foot of fan on the fin, and the upper end four corners of the fixed foot of fan is provided with the fan bolt, the upper end of fan bolt is connected with the fan, the both sides of fin bottom plate are provided with horizontal flexible post, and are provided with horizontal flexible post bolt on the both sides of fin bottom plate, the lower extreme of horizontal flexible post is connected with the vertical flexible post, and the lower extreme outer wall of horizontal flexible post is provided with vertical flexible post bolt, the lower extreme of vertical flexible post is provided with the splint bolt, and one.
Preferably, the upper fixing plate and the lower fixing plate of the radiating fin are parallel, and the copper-aluminum combined radiating fins are distributed at equal intervals along the inner walls of the upper fixing plate and the lower fixing plate of the radiating fin.
Preferably, the fans are distributed at equal intervals along four edges of the upper fixing plate of the heat sink, and a detachable structure is arranged between the fans and the upper fixing plate of the heat sink.
Preferably, the transverse telescopic column and the lower fixing plate of the radiating fin are distributed horizontally, and a telescopic structure is arranged between the transverse telescopic column and the lower fixing plate of the radiating fin.
Preferably, be vertical form distribution between vertical flexible post and the horizontal flexible post, and the inner wall of vertical flexible post outer wall laminating in horizontal flexible post.
Preferably, the clamping plate bolt penetrates through the inner side of the clamping plate, and a rotating structure is formed between the clamping plate bolt and the clamping plate.
Compared with the prior art, the beneficial effects of the utility model are that: the radiating device for the airborne equipment of the unmanned aerial vehicle is provided with the radiating fin upper fixing plate and the radiating fin lower fixing plate which are parallel, radiating fins are distributed at equal intervals, so that the radiating effect of the radiating device is improved to the maximum extent, uneven radiating may be caused by different distance distribution, the service life of the equipment is directly shortened due to poor radiating effect, good stability and firmness can be provided for the whole radiating device due to the equal distance distribution, and the situation of shaking cannot occur in the using process;
the fans are distributed at equal intervals along the four edges of the fixing plate on the radiating fin, the fan positioned at the upper end of the copper-aluminum combined radiating fin can effectively disperse heat conducted out by the radiating fin, radiating efficiency is improved, meanwhile, the detachable structure also provides convenience for cleaning and replacing the fan in the later period when a fault occurs, and working efficiency of the radiating device is greatly improved;
the transverse telescopic columns and the lower fixing plate of the radiating fin are distributed horizontally, the telescopic structural design ensures the effective working range of the radiator, the radiator can be installed on equipment with different sizes and shapes, the bolts are arranged in a matched mode to improve the firmness of the radiator in the installation process of the radiator needing radiating equipment, and the situation that a radiating device of the unmanned aerial vehicle can fall off in the flying process can be avoided;
the longitudinal telescopic columns and the transverse telescopic columns are vertically distributed, and the inner walls are mutually attached, so that the stability of the whole heat dissipation device is ensured under the condition of ensuring the overall attractive appearance, the service life of the heat dissipation device is prolonged, the heat dissipation device is very convenient and quick to mount, convenient to carry and free of occupying a large space;
the splint bolt runs through in the inboard of splint, and splint that can rotate not only can install on the equipment not of uniform size, and the equipment that the shape is different also can install, only needs the rotation angle of adjusting splint can convenient and fast very, avoids the numerous and diverse problem of conventional installation, but provides convenience when promoting radiator working range.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic diagram of the structure of the telescopic column clamping plate of the present invention;
fig. 3 is a schematic view of the fan of the present invention.
In the figure: 1. copper-aluminum combined radiating fins; 2. a fixing plate on the heat sink; 3. a fan fixing pin; 4. a fan; 5. a fan bolt; 6. a lower fixing plate of the heat sink; 7. a transverse telescopic stud; 8. a transverse telescopic column; 9. a longitudinally telescoping stud; 10. a longitudinal telescopic column; 11. a clamp plate bolt; 12. and (4) clamping the plate.
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. 1-3, the present invention provides a technical solution: a heat dissipation device for airborne equipment of an unmanned aerial vehicle comprises a copper-aluminum combined heat dissipation fin 1, a heat dissipation fin upper fixing plate 2, a fan fixing pin 3, a fan 4, a fan bolt 5, a heat dissipation fin lower fixing plate 6, a transverse telescopic column bolt 7, a transverse telescopic column 8, a longitudinal telescopic column bolt 9, a longitudinal telescopic column 10, a clamping plate bolt 11 and a clamping plate 12, wherein the upper end of the copper-aluminum combined heat dissipation fin 1 is provided with the heat dissipation fin upper fixing plate 2, the lower end of the copper-aluminum combined heat dissipation fin 1 is provided with the heat dissipation fin lower fixing plate 6, the heat dissipation fin upper fixing plate 2 and the heat dissipation fin lower fixing plate 6 are parallel, the copper-aluminum combined heat dissipation fin 1 is distributed along the inner walls of the heat dissipation fin upper fixing plate 2 and the heat dissipation fin lower fixing plate 6 at equal intervals, the heat dissipation effect of the heat dissipation device is improved to, the equidistant distribution can also provide good stability for the whole heat dissipation device, and the heat dissipation device is very firm and can not shake in the use process;
the upper end of the upper fixing plate 2 of the heat sink is fixed with a fan fixing pin 3, four corners of the upper end of the fan fixing pin 3 are provided with fan bolts 5, the upper end of each fan bolt 5 is connected with a fan 4, the fans 4 are distributed at equal intervals along four sides of the upper fixing plate 2 of the heat sink, a detachable structure is arranged between each fan 4 and the upper fixing plate 2 of the heat sink, the fans 4 positioned at the upper ends of the copper-aluminum combined heat sinks 1 can effectively disperse heat conducted out by the heat sinks, the heat dissipation efficiency is improved, meanwhile, the detachable structure also provides convenience for cleaning and replacement of the fans 4 in the later period when faults occur, and the working efficiency of the heat dissipation device;
the two sides of the lower radiating fin fixing plate 6 are provided with transverse telescopic columns 8, the upper ends of the two sides of the lower radiating fin fixing plate 6 are provided with transverse telescopic column bolts 7, the transverse telescopic columns 8 and the lower radiating fin fixing plate 6 are distributed in a horizontal shape, a telescopic structure is arranged between the transverse telescopic columns 8 and the lower radiating fin fixing plate 6, the effective working range of the radiator is guaranteed through telescopic structural design, the radiator can be installed on equipment with different sizes and shapes, the firmness of the radiator needing radiating equipment in installation is improved by matching with the bolts, and the situation that a radiating device of the unmanned aerial vehicle can fall off in the flying process is avoided;
the lower end of the transverse telescopic column 8 is connected with a longitudinal telescopic column 10, the outer wall of the lower end of the transverse telescopic column 8 is provided with a longitudinal telescopic column bolt 9, the longitudinal telescopic column 10 and the transverse telescopic column 8 are distributed vertically, the outer wall of the longitudinal telescopic column 10 is attached to the inner wall of the transverse telescopic column 8, and the inner walls are attached to each other, so that the stability of the whole heat dissipation device is ensured under the condition of ensuring the integral attractiveness, the service life of the heat dissipation device is prolonged, the heat dissipation device is very convenient and rapid to install, and the heat dissipation device is convenient to carry and does not occupy a large space;
the lower extreme of vertical flexible post 10 is provided with splint bolt 11, and one side of splint bolt 11 is connected with splint 12, splint bolt 11 runs through in the inboard of splint 12, and constitute revolution mechanic between splint bolt 11 and the splint 12, splint 12 that can rotate not only can install on the equipment not of uniform size, the equipment that the shape is different also can install, only need adjust splint 12's rotation angle can be convenient and fast very, avoid the miscellaneous problem of conventional installation, but provide convenience when promoting radiator working range.
The working principle is as follows: for the heat dissipation device for the airborne equipment of the unmanned aerial vehicle, firstly, the transverse telescopic column 8 and the longitudinal telescopic column 10 on the heat dissipation device are adjusted to be proper in size, the telescopic structural design ensures the effective working range of the heat dissipation device, the heat dissipation device can be installed on equipment with different sizes and shapes, the firmness of the heat dissipation device required to be installed on the heat dissipation device is improved by matching with the arranged bolts, the situation that the heat dissipation device drops in the flying process of the unmanned aerial vehicle is avoided, the inner part and the inner part are mutually attached to the wall, the stability of the whole heat dissipation device is ensured under the condition of ensuring the integral attractiveness, the service life of the heat dissipation device is prolonged, the heat dissipation device is also very convenient and rapid to install, the heat dissipation device is convenient to carry and does not need to occupy a large space, the angle of the clamping plate 12 is adjusted, the clamping plate 12 capable of rotating can be installed, only need adjust splint 12's rotation angle can be very convenient and fast, avoid the numerous and diverse problem of conventional installation, but promote radiator working range and provide convenience, embolia the equipment that need carry out the heat dissipation, the heat of equipment can combine fin 1 along with the laminating copper aluminium in the outside to derive, fan 4 through the heat abstractor top is gone out the heat dispersion of deriving, reached and given the radiating effect of equipment, just accomplish whole heat abstractor's that is used for unmanned aerial vehicle machine to carry equipment use like this.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a heat abstractor for unmanned aerial vehicle airborne equipment, includes on the fin fixed plate (2), fan (4) and vertical flexible post (10), its characterized in that: the upper end of the copper-aluminum combined radiating fin (1) is provided with a radiating fin upper fixing plate (2), the lower end of the copper-aluminum combined radiating fin (1) is provided with a radiating fin lower fixing plate (6), the upper end of the radiating fin upper fixing plate (2) is fixed with a fan fixing pin (3), fan bolts (5) are arranged at four corners of the upper end of the fan fixing pin (3), the upper end of each fan bolt (5) is connected with a fan (4), two sides of the radiating fin lower fixing plate (6) are provided with transverse telescopic columns (8), the upper ends of two sides of the radiating fin lower fixing plate (6) are provided with transverse telescopic column bolts (7), the lower ends of the transverse telescopic columns (8) are connected with longitudinal telescopic columns (10), the outer walls of the lower ends of the transverse telescopic columns (8) are provided with longitudinal telescopic column bolts (9), and the lower ends of the longitudinal, and one side of the clamping plate bolt (11) is connected with a clamping plate (12).
2. The heat dissipation device of claim 1, wherein: the upper fixing plate (2) and the lower fixing plate (6) of the radiating fin are parallel, and the copper-aluminum combined radiating fins (1) are distributed at equal intervals along the inner walls of the upper fixing plate (2) and the lower fixing plate (6) of the radiating fin.
3. The heat dissipation device of claim 1, wherein: the fans (4) are distributed at equal intervals along the four sides of the upper fixing plate (2) of the heat sink, and the fans (4) and the upper fixing plate (2) of the heat sink are of detachable structures.
4. The heat dissipation device of claim 1, wherein: the transverse telescopic columns (8) and the radiating fin lower fixing plate (6) are distributed horizontally, and a telescopic structure is arranged between the transverse telescopic columns (8) and the radiating fin lower fixing plate (6).
5. The heat dissipation device of claim 1, wherein: the longitudinal telescopic column (10) and the transverse telescopic column (8) are vertically distributed, and the outer wall of the longitudinal telescopic column (10) is attached to the inner wall of the transverse telescopic column (8).
6. The heat dissipation device of claim 1, wherein: the clamping plate bolt (11) penetrates through the inner side of the clamping plate (12), and a rotating structure is formed between the clamping plate bolt (11) and the clamping plate (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921736061.9U CN210840492U (en) | 2019-10-16 | 2019-10-16 | Heat dissipation device for airborne equipment of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921736061.9U CN210840492U (en) | 2019-10-16 | 2019-10-16 | Heat dissipation device for airborne equipment of unmanned aerial vehicle |
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| CN210840492U true CN210840492U (en) | 2020-06-23 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921736061.9U Active CN210840492U (en) | 2019-10-16 | 2019-10-16 | Heat dissipation device for airborne equipment of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112074180A (en) * | 2020-10-10 | 2020-12-11 | 珠海格力电器股份有限公司 | Adjustable flow guide control system capable of dissipating heat quickly, control method of adjustable flow guide control system and water heater |
-
2019
- 2019-10-16 CN CN201921736061.9U patent/CN210840492U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112074180A (en) * | 2020-10-10 | 2020-12-11 | 珠海格力电器股份有限公司 | Adjustable flow guide control system capable of dissipating heat quickly, control method of adjustable flow guide control system and water heater |
| CN112074180B (en) * | 2020-10-10 | 2024-03-19 | 珠海格力电器股份有限公司 | Adjustable diversion control system, control method thereof and water heater |
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