CN207766756U - A kind of unmanned plane radiator of highly effective rainproof snow - Google Patents
A kind of unmanned plane radiator of highly effective rainproof snow Download PDFInfo
- Publication number
- CN207766756U CN207766756U CN201721806723.6U CN201721806723U CN207766756U CN 207766756 U CN207766756 U CN 207766756U CN 201721806723 U CN201721806723 U CN 201721806723U CN 207766756 U CN207766756 U CN 207766756U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- fixedly installed
- box
- inlet
- highly effective
- 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.)
- Active
Links
Landscapes
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model discloses a kind of unmanned plane radiators of highly effective rainproof snow, including unmanned plane shell, wing, the upper end of the unmanned plane shell is fixedly installed inlet box, it is fixedly installed wind turbine on the inside of the inlet box, the first air inlet is offered on the outside of the inlet box, the lower end of the inlet box is fixedly installed the first ventilating duct, and one end of the ventilating duct is fixedly installed air outlet box, and the air outlet box is fixed at the lower end of unmanned plane shell.Temperature sensor, control box is arranged in the utility model; when operating personnel set particular temperature value; when circuit board also generates heat while constantly generating control instruction, temperature sensor is by the temperature value detected by electric signal transmission to control box, and control box is after processing; if reaching the temperature value of setting; control box controls the operating of wind turbine, and wind turbine drives extraneous cold air to enter inside, achievees the effect that heat dissipation; circuit board is protected, the effect of automatic heat radiation is realized.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of unmanned plane radiator of highly effective rainproof snow.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Unmanned plane sector application, which is unmanned plane, really just have been needed；
It taking photo by plane at present, agricultural, plant protection, self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news
The application in report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane itself
On the way, developed country is also in actively extension sector application and development unmanned air vehicle technique.
Existing device has the following disadvantages：1, traditional unmanned plane is spread all in flight using exposed electric elements or fuselage
The mode that heat emission hole radiates, so can not lower flight in rain and snow；2, it is controlled during the operation or test of unmanned plane
System processed constantly generates control instruction, and circuit board also generates heat while constantly generating control instruction, which will
Many detrimental effects are brought to the body of unmanned plane, such as deforms, if also heat is excessively high can damage circuit board, causes to estimate
The damage of meter.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane radiators of highly effective rainproof snow, to solve above-mentioned background
The problem of being proposed in technology.
To achieve the above object, the utility model provides the following technical solutions：A kind of unmanned plane heat dissipation of highly effective rainproof snow
Device, including unmanned plane shell, wing, the upper end of the unmanned plane shell are fixedly installed inlet box, the inlet box it is interior
Side is fixedly installed wind turbine, offers the first air inlet on the outside of the inlet box, and the lower end of the inlet box is fixedly installed the
One end of one ventilating duct, first ventilating duct is fixedly installed air outlet box, and the air outlet box is fixed at unmanned plane shell
Lower end, the lower end of the air outlet box offers the first air outlet, and the wing is fixed at the side of unmanned plane shell, institute
The both sides for stating wing are fixedly installed propeller by connector, and the lower end of the propeller is fixedly installed dual-axle motor peace
Piece installing is fixedly installed dual-axle motor on the inside of the dual-axle motor installation part, and the both sides of the wing offer second respectively
Air inlet, second air inlet connect the second ventilating duct on the inside of connector, and second ventilating duct, which is connected, is located at twin shaft electricity
The second air outlet that the lower end of machine installation part opens up.
Preferably, circuit board, the outside fixed setting of the circuit board are fixedly installed on the inside of the unmanned plane shell
There is temperature sensor.
Preferably, the unmanned plane case inside is fixedly installed control box, and input terminal and the temperature of the control box pass
The output end of sensor is electrically connected, and the output end of the control box and the input terminal of wind turbine are electrically connected.
Preferably, it is bolted to connection respectively between the connector and wing, dual-axle motor installation part.
Preferably, first air inlet and the second air inlet are fixedly installed protection network respectively.
Preferably, the lower end of the dual-axle motor is movably installed with flabellum.
Compared with prior art, the utility model has the beneficial effects that：
1, the utility model passes through unmanned plane shell upper end inlet box side by the way that inlet box, wind turbine, when flight is arranged
First air inlet sucking cold air enters unmanned plane enclosure interior, is then discharged again by the first air outlet of unmanned plane housing bottom
Generated hot-air when electronic component works in unmanned plane shell, to reach cooling effect, in inlet box side and wing
Both sides open up air inlet, when preventing from descending flight in rain and snow, sleet because gravity enter in cabin, to realize rain
The safety work of snowy day gas；The protection network of air inlet can prevent sundries from entering in unmanned plane shell, reach and keep unmanned plane shell
Interior clean effect.
2, the utility model setting temperature sensor, control box, when operating personnel's setting particular temperature value, when circuit board exists
When also generating heat while constantly generating control instruction, temperature sensor arrives the temperature value detected by electric signal transmission
Control box, after processing, if reaching the temperature value of setting, control box controls the operating of wind turbine to control box, and wind turbine drives extraneous
Cold air enters inside, achievees the effect that heat dissipation, protects circuit board, improves the effect of automatic heat radiation.
Description of the drawings
Fig. 1 is a kind of unmanned plane radiator overall structure diagram of highly effective rainproof snow of the utility model；
Fig. 2 is the installation view of a kind of unmanned plane radiator inlet box of highly effective rainproof snow of the utility model, wind turbine；
Fig. 3 is the utility model a kind of unmanned plane radiator dual-axle motor installation part, dual-axle motor of highly effective rainproof snow
Structural schematic diagram.
In figure：1- unmanned plane shells；2- inlet boxes；The first air inlets of 3-；4- temperature sensors；The first ventilating ducts of 5-；6-
Circuit board；7- control box；8- air outlet box；The first air outlets of 9-；The second air inlets of 10-；11- connectors；12- dual-axle motors are installed
Part；13- wings；14- propellers；15- protection networks；16- wind turbines；17- dual-axle motors；The second air outlets of 18-；19- flabellums；20-
Second ventilating duct.
Specific implementation mode
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
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of unmanned plane heat dissipation dress of highly effective rainproof snow
It sets, including unmanned plane shell 1, wing 13, the upper end of the unmanned plane shell 1 is fixedly installed inlet box 2, the inlet box 2
Inside be fixedly installed wind turbine 16,2 outside of the inlet box offers the first air inlet 3, and the lower end of the inlet box 2 is fixed
It is provided with the first ventilating duct 5, one end of first ventilating duct 5 is fixedly installed air outlet box 8, and the air outlet box 8 is fixedly installed
In the lower end of unmanned plane shell 1, the lower end of the air outlet box 8 offers the first air outlet 9, and the wing 13 is fixed at nothing
The both sides of the side of man-machine shell 1, the wing 13 are fixedly installed propeller 14, the propeller 14 by connector 11
Lower end be fixedly installed dual-axle motor installation part 12, the inside of the dual-axle motor installation part 12 is fixedly installed dual-axle motor
17, the both sides of the wing 13 offer the second air inlet 10 respectively, and second air inlet 10 connects 11 inside of connector
Second ventilating duct 20, second ventilating duct 20 connect the second air outlet opened up positioned at the lower end of dual-axle motor installation part 12
18。
The inside of the unmanned plane shell 1 is fixedly installed circuit board 6, and the outside of the circuit board 6 is fixedly installed temperature
Spend sensor 4, the temperature of real-time detection circuit plate 6；1 inside of the unmanned plane shell is fixedly installed control box 7, the control
The input terminal of box 7 is electrically connected with the output end of temperature sensor 4, the input terminal of the output end and wind turbine 16 of the control box 7
It is electrically connected, is convenient for the operation of device, improves the degree of automation；The connector 11 and wing 13, dual-axle motor installation part
It is bolted to connection respectively between 12, is convenient for the stabilization of device；Distinguish at first air inlet, 3 and second air inlet 10
It is fixedly installed protection network 15, sundries is prevented to enter in unmanned plane shell 1；The lower end of the dual-axle motor 17 is movably installed with fan
Leaf 19 is convenient for the heat dissipation of unmanned plane dual-axle motor 17 in flight.
Operation principle：In use, working as unmanned plane in the process of running, pass through 17 band of dual-axle motor of 14 lower end of propeller
The flabellum 19 of dynamic 17 lower end of dual-axle motor, cool ambient air have the second ventilating duct 20 to enter dual-axle motor by the second air inlet 10
17 working regions, and the heat generated when the work of dual-axle motor 17 passes through the workspace that dual-axle motor 17 is discharged in the second air outlet 18
Domain, in unmanned plane before use, setting particular temperature value by operating personnel, when circuit board 6 is while constantly generating control instruction
When also generating heat, temperature sensor 4 is by the temperature value detected by electric signal transmission to control box 7, and control box 7 is through processing
Afterwards, if reaching the temperature value of setting, control box 7 controls the operating of wind turbine 16, and the first air inlet 3 of 2 side of upper end inlet box is inhaled
Enter cold air by the first ventilating duct 5 to be entered inside unmanned plane shell 1, then be opened up again by 1 bottom air outlet box 8 of unmanned plane shell
The first air outlet 9 discharge unmanned plane shell 1 in electronic component work when generated hot-air, to reach the work of heat dissipation
With.
It should be noted that herein, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also include other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane radiator of highly effective rainproof snow, including unmanned plane shell（1）, wing（13）, it is characterised in that：Institute
State unmanned plane shell（1）Upper end be fixedly installed inlet box（2）, the inlet box（2）Inside be fixedly installed wind turbine
（16）, the inlet box（2）Outside offers the first air inlet（3）, the inlet box（2）To be fixedly installed first logical for lower end
Air duct（5）, first ventilating duct（5）One end be fixedly installed air outlet box（8）, the air outlet box（8）It is fixed at nothing
Man-machine shell（1）Lower end, the air outlet box（8）Lower end offer the first air outlet（9）, the wing（13）Fixed setting
In unmanned plane shell（1）Side, the wing（13）Both sides pass through connector（11）It is fixedly installed propeller（14）,
The propeller（14）Lower end be fixedly installed dual-axle motor installation part（12）, the dual-axle motor installation part（12）Inside
It is fixedly installed dual-axle motor（17）, the wing（13）Both sides offer the second air inlet respectively（10）, described second into
Air port（10）Connect connector（11）Second ventilating duct of inside（20）, second ventilating duct（20）It connects and is located at dual-axle motor
Installation part（12）The second air outlet for opening up of lower end（18）.
2. a kind of unmanned plane radiator of highly effective rainproof snow according to claim 1, it is characterised in that：The unmanned plane
Shell（1）Inside be fixedly installed circuit board（6）, the circuit board（6）Outside be fixedly installed temperature sensor（4）.
3. a kind of unmanned plane radiator of highly effective rainproof snow according to claim 2, it is characterised in that：The unmanned plane
Shell（1）Inside is fixedly installed control box（7）, the control box（7）Input terminal and temperature sensor（4）Output end electricity
Property connection, the control box（7）Output end and wind turbine（16）Input terminal be electrically connected.
4. a kind of unmanned plane radiator of highly effective rainproof snow according to claim 3, it is characterised in that：The connector
（11）With wing（13）, dual-axle motor installation part（12）Between be bolted to connection respectively.
5. a kind of unmanned plane radiator of highly effective rainproof snow according to claim 1, it is characterised in that：Described first into
Air port（3）With the second air inlet（10）Place is fixedly installed protection network respectively（15）.
6. a kind of unmanned plane radiator of highly effective rainproof snow according to claim 1, it is characterised in that：The twin shaft electricity
Machine（17）Lower end be movably installed with flabellum（19）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721806723.6U CN207766756U (en) | 2017-12-21 | 2017-12-21 | A kind of unmanned plane radiator of highly effective rainproof snow |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721806723.6U CN207766756U (en) | 2017-12-21 | 2017-12-21 | A kind of unmanned plane radiator of highly effective rainproof snow |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207766756U true CN207766756U (en) | 2018-08-24 |
Family
ID=63187662
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721806723.6U Active CN207766756U (en) | 2017-12-21 | 2017-12-21 | A kind of unmanned plane radiator of highly effective rainproof snow |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207766756U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113381773A (en) * | 2021-08-16 | 2021-09-10 | 南京卡飞软件技术有限公司 | Wireless transmitting module for forest fire prevention exploration unmanned aerial vehicle |
| WO2021208099A1 (en) * | 2020-04-17 | 2021-10-21 | 深圳市大疆创新科技有限公司 | Circuit box and unmanned aerial vehicle |
-
2017
- 2017-12-21 CN CN201721806723.6U patent/CN207766756U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021208099A1 (en) * | 2020-04-17 | 2021-10-21 | 深圳市大疆创新科技有限公司 | Circuit box and unmanned aerial vehicle |
| CN113381773A (en) * | 2021-08-16 | 2021-09-10 | 南京卡飞软件技术有限公司 | Wireless transmitting module for forest fire prevention exploration unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207766756U (en) | A kind of unmanned plane radiator of highly effective rainproof snow | |
| CN207106876U (en) | A kind of rain-proof unmanned plane | |
| US20110196540A1 (en) | Environmental control system for precision airborne payloads | |
| CN106081088A (en) | A kind of professional big flood rescue unmanned plane rescuing disaster affected people in flood damage | |
| CN207818845U (en) | Container | |
| CN205632998U (en) | Unmanned aerial vehicle heat abstractor of high -efficient rain -proof snow | |
| CN208425091U (en) | A kind of radiator of unmanned plane | |
| CN108313277A (en) | A kind of patrol unmanned machine of monitoring | |
| CN208453234U (en) | A kind of novel adjustable arm unmanned plane | |
| CN205989813U (en) | A kind of professional big flood rescue unmanned plane for rescue disaster affected people in flood damage | |
| CN211893650U (en) | Unmanned aerial vehicle is with heat abstractor | |
| CN206885366U (en) | A kind of multi-functional model plane unmanned plane heat abstractor | |
| CN207773505U (en) | A kind of unmanned plane radiator | |
| CN108454840A (en) | A kind of unmanned plane of wing waterproof | |
| CN211792632U (en) | Multi-functional model aeroplane and model ship unmanned aerial vehicle heat abstractor | |
| CN109782780A (en) | A kind of winged control examination protective device of multi-rotor unmanned aerial vehicle | |
| CN107187585A (en) | A kind of unmanned plane | |
| CN207346091U (en) | A kind of six rotor wing unmanned aerial vehicle system of long endurance | |
| CN208453250U (en) | A kind of fixed-wing unmanned plane self-driving device with radiator structure | |
| CN205327407U (en) | Many rotor unmanned aerial vehicle that branch oar was independently supplied power | |
| CN207809812U (en) | Cyclone type air partition device | |
| CN215285291U (en) | Rotor unmanned aerial vehicle aircraft nacelle | |
| CN213443083U (en) | Unmanned aerial vehicle who possesses anticollision function | |
| CN209921619U (en) | Centralized heat abstractor that is used for unmanned aerial vehicle's motor drive power | |
| CN220465819U (en) | Infrared visual throwing device with heat dissipation function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |