CN206149683U - High -efficient unmanned aerial vehicle heat abstractor - Google Patents
High -efficient unmanned aerial vehicle heat abstractor Download PDFInfo
- Publication number
- CN206149683U CN206149683U CN201620954630.7U CN201620954630U CN206149683U CN 206149683 U CN206149683 U CN 206149683U CN 201620954630 U CN201620954630 U CN 201620954630U CN 206149683 U CN206149683 U CN 206149683U
- Authority
- CN
- China
- Prior art keywords
- copper pipe
- fin
- insulating material
- heat
- heat abstractor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model discloses a high -efficient unmanned aerial vehicle heat abstractor, including support, the heat -insulating material that looses, copper pipe and fuselage. The fuselage is equipped with four supports, annular protection frame is installed on the support top, be provided with the spiral leaf in the annular protection frame, the support inner chamber runs through and is equipped with the copper pipe, the setting of copper pipe one end is in the frame wall of annular protection frame, the copper pipe other end is connected with scattered heat -insulating material, the heat -insulating material that looses is five airtight bottom surface open -ended box bodys, scattered heat -insulating material upper portion is equipped with the plenum, the plenum wall is equipped with the mouth of giving a dinner for a visitor from afar, just the exhaust fan is installed on the top in the plenum, scattered heat -insulating material lower part is provided with a plurality of fin. The unmanned aerial vehicle heat abstractor, structural design is equitable and practical, and giving a dinner for a visitor from afar mouthful of the heat -insulating material that looses can be for the fin provides cold wind in order reaching the desuperheat, and 3 groups and exhaust fan are no less than in the fin setting can make and form the air current in the heat -insulating material that looses to reach the efficient cooling, simultaneously with the copper union coupling, not only regard as the ventilation pipe in order to reach the copper pipe, can also cool down together with the fin.
Description
Technical field
This utility model is related to unmanned plane heat abstractor technical field, specially a kind of efficient unmanned plane heat abstractor.
Background technology
At present, with the development of social economy, unmanned plane is particularly civilian unmanned plane and shows one's capabilities in recent years, in each portion
Door, industry-by-industry play more and more important effect.
Inside unmanned plane of the prior art, main heating module is to calculate the module concentrated, at control module like flying, vision
Reason module, high definition transport module etc., in these modules, components and parts and sensor for temperature are very sensitive, and existing market is to dissipating
Heat treatment is not fine, if can not continue and efficient radiating, it will huge injury is caused to unmanned plane, or even is difficult to work
Make.
Utility model content
The purpose of this utility model is to provide a kind of efficient unmanned plane heat abstractor, to solve to carry in above-mentioned background technology
The problem for going out.
For achieving the above object, this utility model provides following technical scheme：A kind of efficient unmanned plane heat abstractor, including
Support, radiating piece, copper pipe and fuselage, the fuselage are provided with four supports, and the cantilever tip is provided with annular shield frame, described
Helical-blade is provided with annular shield frame, through copper pipe is provided with, described copper pipe one end is arranged on annular shield to the support interior wall
In the frame wall of frame, the copper pipe other end is connected with radiating piece, box body of the radiating piece for five-surfac airtight bottom surface opening, described
Radiating piece top is provided with air compartment, and four wall of the air compartment is provided with top in mouth of giving a dinner for a visitor from afar, and the air compartment and is provided with exhaust fan, described to dissipate
Warmware bottom is provided with some fin.
Preferably, the copper pipe is arranged in flat, and the copper pipe is provided with arc with the seam of annular shield frame and fills wind
Mouthful, the copper pipe other end is contacted with fin with a mouthful airtight connection of giving a dinner for a visitor from afar, and copper pipe.
Preferably, the fin is arranged no less than 3 groups.
Preferably, the position of the fuselage bottom correspondence radiating piece opening is provided with some air vents.
Compared with prior art, the beneficial effects of the utility model are：The unmanned plane heat abstractor, reasonable in design and
Practicality, the mouth of giving a dinner for a visitor from afar of radiating piece can provide cold wind for fin to reach desuperheat, and fin is arranged no less than 3 groups and exhaust fan
Can make in radiating piece, to form air-flow, to reach efficient cooling, while being connected with copper pipe, ventilation is served not only as to reach copper pipe
Pipe, can be lowering the temperature together with fin.
Description of the drawings
Fig. 1 is this utility model structural representation；
Fig. 2 is radiating piece cross-sectional view of the present utility model.
In figure：1 support, 2 radiating pieces, 3 copper pipes, 4 annular shield framves, 5 helical-blades, 21 fin, 22 exhaust fan, 23 are given a dinner for a visitor from afar
Mouthful.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only this utility model a part of embodiment, rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of this utility model protection.
Fig. 1-2 is referred to, this utility model provides a kind of technical scheme：A kind of efficient unmanned plane heat abstractor, including
Frame 1, radiating piece 2, copper pipe 3 and fuselage.The fuselage is provided with four supports 1, and 1 top of the support is provided with annular shield frame 4,
Helical-blade is provided with the annular shield frame 4, through copper pipe 3 is provided with, 3 one end of the copper pipe is arranged on 1 inner chamber of the support
In the frame wall of annular shield frame 4, the copper pipe 3 is arranged in flat, and the copper pipe 3 is provided with arc with 4 seam of annular shield frame
Shape fills air port, and 3 other end of the copper pipe is contacted with fin 21 with 23 airtight connection of mouth of giving a dinner for a visitor from afar, and copper pipe 3, and the copper pipe 3 is another
One end is connected with radiating piece 2, box body of the radiating piece 2 for five-surfac airtight bottom surface opening, and 2 top of the radiating piece is provided with wind
Room, four wall of the air compartment are provided with top in mouth 23 of giving a dinner for a visitor from afar, and the air compartment and are provided with exhaust fan 22, and 2 bottom of the radiating piece sets
Some fin 21 are equipped with, the fin 21 is arranged no less than 3 groups, the position of the fuselage bottom correspondence opening of radiating piece 21
It is provided with some air vents.
Operation principle：During 2 normal work of heat abstractor, copper pipe 3 is entered by filling air port air-flow, reach air compartment to radiating
Piece 21 is lowered the temperature, while exhaust fan 22 starts discharging the thermal current in radiating piece 2, to reach the air current flow of circulation, works as temperature
When too high, the copper pipe 3 contacted with fin 21 can play assistance cooling.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
Be appreciated that these embodiments can be carried out various changes in the case of without departing from principle of the present utility model and spirit, repair
Change, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (4)
1. a kind of efficient unmanned plane heat abstractor, including support (1), radiating piece (2), copper pipe (3) and fuselage, it is characterised in that：
The fuselage is provided with four supports (1), and support (1) top is provided with annular shield frame (4), the annular shield frame (4)
Helical-blade (5) is provided with inside, through copper pipe (3) is provided with, it is anti-that described copper pipe (3) one end is arranged on annular to support (1) inner chamber
In the frame wall of retaining frame (4), copper pipe (3) other end is connected with radiating piece (2), and the radiating piece (2) is five-surfac airtight bottom surface
The box body of opening, radiating piece (2) top are provided with air compartment, and four wall of the air compartment is provided with mouth of giving a dinner for a visitor from afar (23), and in the air compartment
Top is provided with exhaust fan (22), and radiating piece (2) bottom is provided with some fin (21), sets between the fin (21)
Put radiating groove.
2. a kind of efficient unmanned plane heat abstractor according to claim 1, it is characterised in that：The copper pipe (3) is in flat
Shape is arranged, and the copper pipe (3) and annular shield frame (4) seam are provided with arc and fill air port, copper pipe (3) other end with give a dinner for a visitor from afar
Mouthful (23) airtight connection, and copper pipe (3) contacted with fin (21).
3. a kind of efficient unmanned plane heat abstractor according to claim 1, it is characterised in that：The fin (21) is arranged
No less than 3 groups.
4. a kind of efficient unmanned plane heat abstractor according to claims 1, it is characterised in that：The fuselage bottom correspondence
The position that radiating piece (2) is open is provided with some air vents.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620954630.7U CN206149683U (en) | 2016-08-26 | 2016-08-26 | High -efficient unmanned aerial vehicle heat abstractor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620954630.7U CN206149683U (en) | 2016-08-26 | 2016-08-26 | High -efficient unmanned aerial vehicle heat abstractor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206149683U true CN206149683U (en) | 2017-05-03 |
Family
ID=58628446
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620954630.7U Expired - Fee Related CN206149683U (en) | 2016-08-26 | 2016-08-26 | High -efficient unmanned aerial vehicle heat abstractor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206149683U (en) |
-
2016
- 2016-08-26 CN CN201620954630.7U patent/CN206149683U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170503 Termination date: 20200826 |