CN208775025U - A kind of unmanned plane radiator - Google Patents
A kind of unmanned plane radiator Download PDFInfo
- Publication number
- CN208775025U CN208775025U CN201821395779.1U CN201821395779U CN208775025U CN 208775025 U CN208775025 U CN 208775025U CN 201821395779 U CN201821395779 U CN 201821395779U CN 208775025 U CN208775025 U CN 208775025U
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- CN
- China
- Prior art keywords
- fixedly connected
- inner cavity
- motor
- motor housing
- unmanned plane
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The utility model discloses a kind of unmanned plane radiators, including body and belt, the left and right ends of the organism bottom are fixedly connected with bracket, the bottom of the body inner cavity is fixedly connected with fixed column, motor housing is fixedly connected at the top of the fixed column, motor is fixedly installed at the top of the motor box cavity, the output shaft of the motor is fixedly connected with first rotating shaft, the first rotating shaft runs through the top of motor box cavity and extends to the upper end of body, wing is fixedly connected at the top of the first rotating shaft, the outer surface of the first rotating shaft and be located at body inner cavity be arranged with the first belt pulley.The utility model is cooperated by body, first rotating shaft, the first belt pulley, belt, motor housing, the second shaft, the second belt pulley, water tank, agitating plate, curved tube, motor, escape pipe, blower, air intake duct and wing, it is poor to solve present unmanned plane radiator heat dissipation effect, is unable to satisfy the problem of people use.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane radiator.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, with someone
It driving an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ", and unmanned plane presses application field,
It can be divided into military with civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone, civilian aspect, and unmanned plane+industrial application is
Unmanned plane has really just needed；It taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself, developed country also in actively extension industrial application and develop unmanned air vehicle technique, nobody
Machine can generate amount of heat after prolonged use, but unmanned plane radiator heat dissipation effect is poor now, and being unable to satisfy people makes
With for this purpose, it is proposed that a kind of unmanned plane radiator.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane radiators, have the advantages of good heat dissipation effect, solve
Present unmanned plane radiator heat dissipation effect is poor, is unable to satisfy the problem of people use.
To achieve the above object, the utility model provides the following technical solutions: a kind of unmanned plane radiator, including body
And belt, the left and right ends of the organism bottom are fixedly connected with bracket, the bottom of the body inner cavity is fixedly connected with fixation
Column is fixedly connected with motor housing at the top of the fixed column, motor, the electricity is fixedly installed at the top of the motor box cavity
The output shaft of machine is fixedly connected with first rotating shaft, and the first rotating shaft runs through the top of motor box cavity and extends to the upper of body
End, is fixedly connected with wing at the top of the first rotating shaft, the outer surface of the first rotating shaft and inner cavity for being located at body is arranged
There is the first belt pulley, the bottom of the motor box cavity is provided with curved tube, and water tank, institute are fixedly connected on the left of the motor housing
The left end for stating body inner cavity top is rotatably connected to the second shaft by bearing, and the top of second shaft outer surface is arranged with
Second belt pulley, second belt pulley are sequentially connected by belt and the first belt pulley, and the bottom of second shaft is run through
The lower part of the middle-end of tank top and the bottom for extending to water tank cavity, the second shaft outer surface is fixedly connected with stirring
The water inlet of plate, the curved tube is fixedly connected with the bottom on the right side of water tank cavity, the water outlet of the curved tube and tank top
Right end is fixedly connected, and blower is fixedly installed on the right side of the motor housing, and the air entry of the blower is fixedly connected with air intake duct,
The other end of the air intake duct is fixedly connected with the top on the right side of motor housing, and the gas outlet of the blower is fixedly connected with outlet
The other end of pipe, the escape pipe runs through the middle-end of body intracavity bottom and extends to the bottom of body.
Preferably, the left and right ends of the motor are fixedly connected with fixed block, and the top of fixed block and motor box cavity
Top be fixedly connected.
Preferably, the left end of the tank top is fixedly connected with water injection pipe, and body inner cavity is run through at the top of water injection pipe
Top.
Preferably, the top movable of the water filling tube cavity is equipped with valve, and the outer surface of valve is provided with anti-skid chequer.
Compared with prior art, the beneficial effects of the utility model are as follows:
1, the utility model first rotating shaft outer surface and be located at the inner cavity of body and be arranged with the first belt pulley, while the
The top of two shaft outer surfaces is arranged with the second belt pulley, and the second belt pulley is sequentially connected by belt and the first belt pulley,
Using motor drive first rotating shaft rotation allow unmanned plane to fly up come when, also allow the second shaft to rotate under the action of motor,
It is fixedly connected with agitating plate by the lower part of the second shaft outer surface, and curved tube water inlet is fixed with the bottom on the right side of water tank cavity
Connection drives agitating plate to rotate using the second shaft, so that the water in water tank be allowed to rotate, using centrifugal force by water from curved tube
Water inlet flows into curved tube, is cooled down using curved tube to motor housing, passes through the water outlet of curved tube and the fixed company of the right end of tank top
It connects, the water in curved tube can be allowed to circulate, improve cooling effect, air intake duct is fixedly connected with by the air entry of blower, and
The other end of air intake duct is fixedly connected with the top on the right side of motor housing, is inhaled the hot gas in motor housing by air intake duct using blower
Out, then by the gas outlet of blower it is fixedly connected with escape pipe, and the other end of escape pipe runs through the middle-end of body intracavity bottom
And the bottom of body is extended to, hot gas is sent out from the bottom of body using escape pipe, improves radiating efficiency, so that heat dissipation effect
Fruit improves, and it is poor to solve present unmanned plane radiator heat dissipation effect, is unable to satisfy the problem of people use.
2, the utility model is fixedly connected with fixed block in the left and right ends of motor, and in the top and motor housing of fixed block
It is fixedly connected at the top of chamber, using the fixed motor of fixed block, prevents motor from loosening the operation for influencing unmanned plane, pass through tank top
Left end be fixedly connected with water injection pipe, and the top of body inner cavity is run through at the top of water injection pipe, facilitates people couple using water injection pipe
Water tank is filled the water, then the top movable by filling the water tube cavity is equipped with valve, and the outer surface of valve is provided with anti-skid chequer,
Water injection pipe is closed after injecting good water using valve, prevents foreign matter from entering, and recycles anti-skid chequer that people is facilitated to tighten valve.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model schematic view of the front view.
In figure: 1 body, 2 first rotating shafts, 3 first belt pulleys, 4 belts, 5 motor housings, 6 second shafts, 7 valves, 8 water fillings
Pipe, 9 second belt pulleys, 10 water tanks, 11 agitating plates, 12 brackets, 13 fixed columns, 14 curved tubes, 15 motors, 16 fixed blocks, 17 outlets
Pipe, 18 blowers, 19 air intake ducts, 20 wings.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
The left and right ends of a kind of unmanned plane radiator referring to FIG. 1-2, including body 1 and belt 4,1 bottom of body are solid
Surely it is connected with bracket 12, the bottom of 1 inner cavity of body is fixedly connected with fixed column 13, and the top of fixed column 13 is fixedly connected with motor
Case 5 is fixedly installed with motor 15 at the top of 5 inner cavity of motor housing, and the left and right ends of motor 15 are fixedly connected with fixed block 16, and solid
Determine to be fixedly connected at the top of the top and 5 inner cavity of motor housing of block 16, using the fixed motor 15 of fixed block 16, prevents motor 15 from loosening
The operation of unmanned plane is influenced, the output shaft of motor 15 is fixedly connected with first rotating shaft 2, and first rotating shaft 2 is through 5 inner cavity of motor housing
Top and the upper end for extending to body 1, the top of first rotating shaft 2 are fixedly connected with wing 20, the outer surface and position of first rotating shaft 2
It is arranged with the first belt pulley 3 in the inner cavity of body 1, the bottom of 5 inner cavity of motor housing is provided with curved tube 14, and the left side of motor housing 5 is solid
Surely it is connected with water tank 10, the left end at 10 top of water tank is fixedly connected with water injection pipe 8, and 1 inner cavity of body is run through at the top of water injection pipe 8
Top, facilitate people to fill the water water tank 10 using water injection pipe 8, the top movable of 8 inner cavity of water injection pipe is equipped with valve 7,
And the outer surface of valve 7 is provided with anti-skid chequer, closes water injection pipe 8 after injecting good water using valve 7, prevents foreign matter from entering, then benefit
People are facilitated to tighten valve 7 with anti-skid chequer, the left end of 1 inner cavity top of body is rotatably connected to the second shaft 6 by bearing, and second
The top of 6 outer surface of shaft is arranged with the second belt pulley 9, and the second belt pulley 9 is sequentially connected by belt 4 and the first belt pulley 3,
Using motor 15 drive first rotating shaft 2 rotation allow unmanned plane to fly up come when, also allow the second shaft 6 under the action of motor 15
Rotation, the bottom of the second shaft 6 runs through the middle-end at 10 top of water tank and extends to the bottom of 10 inner cavity of water tank, outside the second shaft 6
The lower part on surface is fixedly connected with agitating plate 11, and the water inlet of curved tube 14 is fixedly connected with the bottom on the right side of 10 inner cavity of water tank, benefit
Agitating plate 11 is driven to rotate with the second shaft 6, so that the water in water tank 10 be allowed to rotate, using centrifugal force by water from curved tube 14
Water inlet flows into curved tube 14, is cooled down using curved tube 14 to motor housing 5, and the right end at 10 top of water outlet and water tank of curved tube 14 is solid
Fixed connection, can allow the water in curved tube 14 to circulate, and improve cooling effect, and the right side of motor housing 5 is fixedly installed with blower 18,
The air entry of blower 18 is fixedly connected with air intake duct 19, and the other end of air intake duct 19 is fixedly connected with the top on 5 right side of motor housing,
The hot gas in motor housing 5 is sucked out by air intake duct 19 using blower 18, the gas outlet of blower 18 is fixedly connected with escape pipe 17,
The other end of escape pipe 17 through 1 intracavity bottom of body middle-end and extend to the bottom of body 1, using escape pipe 17 by hot gas
It is sent out from the bottom of body 1, improves radiating efficiency, so that heat dissipation effect improves, solved present unmanned plane radiator and dissipate
Thermal effect is poor, is unable to satisfy the problem of people use.
In use, first rotating shaft 2 outer surface and be located at body 1 inner cavity be arranged with the first belt pulley 3, while second
The top of 6 outer surface of shaft is arranged with the second belt pulley 9, and the second belt pulley 9 is connected by belt 4 and the transmission of the first belt pulley 3
Connect, using motor 15 drive first rotating shaft 2 rotation allow unmanned plane to fly up come when, also allow the second shaft 6 in the work of motor 15
With lower rotation, agitating plate 11 is fixedly connected with by the lower part of 6 outer surface of the second shaft, and in 14 water inlet of curved tube and water tank 10
Bottom on the right side of chamber is fixedly connected, and drives agitating plate 11 to rotate using the second shaft 6, so that the water in water tank 10 be allowed to rotate
Come, flowed into curved tube 14 by water from 14 water inlet of curved tube using centrifugal force, is cooled down using curved tube 14 to motor housing 5, pass through curved tube
14 water outlet is fixedly connected with the right end at 10 top of water tank, and the water in curved tube 14 can be allowed to circulate, and improves cooling effect,
It is fixedly connected with air intake duct 19 by the air entry of blower 18, and the top on 5 right side of the other end of air intake duct 19 and motor housing is solid
It is fixed to connect, the hot gas in motor housing 5 is sucked out by air intake duct 19 using blower 18, then the fixed company in gas outlet for passing through blower 18
It is connected to escape pipe 17, and the other end of escape pipe 17 runs through the middle-end of 1 intracavity bottom of body and extends to the bottom of body 1, benefit
Hot gas is sent out from the bottom of body 1 with escape pipe 17, radiating efficiency is improved, so that heat dissipation effect improves, solves now
Unmanned plane radiator heat dissipation effect is poor, is unable to satisfy the problem of people use, is fixedly connected in the left and right ends of motor 15
Fixed block 16, and be fixedly connected at the top of the top of fixed block 16 and 5 inner cavity of motor housing, motor 15 is fixed using fixed block 16,
It prevents motor 15 from loosening the operation for influencing unmanned plane, water injection pipe 8, and water injection pipe is fixedly connected with by the left end at 10 top of water tank
The top of 1 inner cavity of body is run through at 8 top, facilitates people to fill the water water tank 10 using water injection pipe 8, then passes through water injection pipe 8
The top movable of inner cavity is equipped with valve 7, and the outer surface of valve 7 is provided with anti-skid chequer, is closed after injecting good water using valve 7
Water injection pipe 8, prevents foreign matter from entering, and recycles anti-skid chequer that people is facilitated to tighten valve 7.
In summary: the unmanned plane radiator passes through body 1, first rotating shaft 2, the first belt pulley 3, belt 4, motor
Case 5, the second shaft 6, the second belt pulley 9, water tank 10, agitating plate 11, curved tube 14, motor 15, escape pipe 17, blower 18, air-breathing
Pipe 19 and wing 20 cooperate, and solve that present unmanned plane radiator heat dissipation effect is poor, and be unable to satisfy that people use asks
Topic.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (4)
1. a kind of unmanned plane radiator, including body (1) and belt (4), it is characterised in that: a left side for body (1) bottom
Right both ends are fixedly connected with bracket (12), and the bottom of body (1) inner cavity is fixedly connected with fixed column (13), the fixed column
(13) it is fixedly connected at the top of motor housing (5), is fixedly installed with motor (15) at the top of motor housing (5) inner cavity, it is described
The output shaft of motor (15) is fixedly connected with first rotating shaft (2), and the first rotating shaft (2) runs through the top of motor housing (5) inner cavity
And the upper end of body (1) is extended to, it is fixedly connected with wing (20) at the top of the first rotating shaft (2), the first rotating shaft (2)
Outer surface and be located at body (1) inner cavity be arranged with the first belt pulley (3), the bottom of motor housing (5) inner cavity is provided with
Curved tube (14) is fixedly connected with water tank (10) on the left of the motor housing (5), and the left end of body (1) inner cavity top passes through
Bearing is rotatably connected to the second shaft (6), and the top of the second shaft (6) outer surface is arranged with the second belt pulley (9), described
Second belt pulley (9) is sequentially connected by belt (4) and the first belt pulley (3), and water tank is run through in the bottom of second shaft (6)
(10) middle-end at the top of and the bottom for extending to water tank (10) inner cavity, the lower part of the second shaft (6) outer surface is fixedly connected
Have agitating plate (11), the water inlet of the curved tube (14) is fixedly connected with the bottom on the right side of water tank (10) inner cavity, the curved tube
(14) water outlet is fixedly connected with the right end at the top of water tank (10), is fixedly installed with blower on the right side of the motor housing (5)
(18), the air entry of the blower (18) is fixedly connected with air intake duct (19), the other end and motor housing of the air intake duct (19)
(5) top on the right side of is fixedly connected, and the gas outlet of the blower (18) is fixedly connected with escape pipe (17), the escape pipe (17)
The other end through body (1) intracavity bottom middle-end and extend to the bottom of body (1).
2. a kind of unmanned plane radiator according to claim 1, it is characterised in that: the left and right ends of the motor (15)
It is fixedly connected with fixed block (16), and is fixedly connected at the top of the top of fixed block (16) and motor housing (5) inner cavity.
3. a kind of unmanned plane radiator according to claim 1, it is characterised in that: the left end at the top of the water tank (10)
It is fixedly connected with water injection pipe (8), and the top of body (1) inner cavity is run through at the top of water injection pipe (8).
4. a kind of unmanned plane radiator according to claim 3, it is characterised in that: water injection pipe (8) inner cavity it is upper
Portion is movably installed with valve (7), and the outer surface of valve (7) is provided with anti-skid chequer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821395779.1U CN208775025U (en) | 2018-08-28 | 2018-08-28 | A kind of unmanned plane radiator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821395779.1U CN208775025U (en) | 2018-08-28 | 2018-08-28 | A kind of unmanned plane radiator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208775025U true CN208775025U (en) | 2019-04-23 |
Family
ID=66158866
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821395779.1U Expired - Fee Related CN208775025U (en) | 2018-08-28 | 2018-08-28 | A kind of unmanned plane radiator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208775025U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110138144A (en) * | 2019-06-06 | 2019-08-16 | 南京理工自动化研究院有限公司 | A kind of Over Electric Motor with PMSM cooling system and its control method |
| CN110450953A (en) * | 2019-08-13 | 2019-11-15 | 深圳市律远汇智科技有限公司 | A kind of unmanned flight's device with heat sinking function for marine security protection patrol |
-
2018
- 2018-08-28 CN CN201821395779.1U patent/CN208775025U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110138144A (en) * | 2019-06-06 | 2019-08-16 | 南京理工自动化研究院有限公司 | A kind of Over Electric Motor with PMSM cooling system and its control method |
| CN110450953A (en) * | 2019-08-13 | 2019-11-15 | 深圳市律远汇智科技有限公司 | A kind of unmanned flight's device with heat sinking function for marine security protection patrol |
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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 |
Granted publication date: 20190423 Termination date: 20200828 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |