CN208868303U - Radiator structure and unmanned vehicle - Google Patents
Radiator structure and unmanned vehicle Download PDFInfo
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- CN208868303U CN208868303U CN201820980901.5U CN201820980901U CN208868303U CN 208868303 U CN208868303 U CN 208868303U CN 201820980901 U CN201820980901 U CN 201820980901U CN 208868303 U CN208868303 U CN 208868303U
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- 230000017525 heat dissipation Effects 0.000 claims abstract description 13
- 230000005855 radiation Effects 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/90—Cooling
- B64U20/96—Cooling using air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
The utility model relates to a kind of radiator structure and unmanned vehicles.The radiator structure includes shell；It is set to the intracorporal radiator fan of the shell；And the first air inlet and the second air inlet being oppositely arranged, and the first air outlet and the second air outlet being oppositely arranged, the air inlet direction of first air inlet and second air inlet is perpendicular to the plane where the radiator fan, the air-out direction and the co-planar where the radiator fan of first air outlet and second air outlet.Radiator structure provided by the embodiment of the utility model has the first air inlet and the second air inlet being oppositely arranged, and the first air outlet and the second air outlet that are oppositely arranged, and structure is simple, and radiating efficiency with higher.The radiator structure is applied to unmanned vehicle, its heat dissipation performance is can be improved, saves its heat-dissipating space, and the heat radiation performance to the maximum extent while controlling the overall weight of unmanned vehicle, makes unmanned vehicle that there is higher safety reliability.
Description
[technical field]
The utility model relates to technical field of heat dissipation more particularly to a kind of unmanned vehicles and its radiator structure.
[background technique]
In recent years, with scientific and technological level and the improvement of people's living standards, unmanned vehicle answering in the world
With becoming increasingly popular, especially in fields such as agricultural, transport, public safety, mining, video display amusement and sports, to unmanned flight
The demand of device is stepped up.
At work, the circuit board for being installed in its fuselage interior can generate amount of heat to unmanned vehicle, and circuit board generates
Heat will affect its normal work, when unmanned vehicle works in the high temperature environment for a long time, not only low efficiency, also to using
Service life impacts, so needing that i.e. internal heat is dispersed into the external environment of unmanned vehicle in time, to guarantee nothing
The operating temperature of people's aircraft interior part is normal.Currently, unmanned vehicle is carried out by installing radiator structure in fuselage interior
Heat dissipation, but existing radiator structure usually has an air inlet and an air outlet, and radiating efficiency is poor, is unable to satisfy nobody
The demand of aircraft.
Therefore, a kind of radiator structure of good heat dissipation effect and the unmanned vehicle with the radiator structure are needed.
[utility model content]
The embodiments of the present invention aim to solve the problem that the technical problems existing in the prior art.For this purpose, the utility model
Embodiment provides a kind of radiator structure and the unmanned vehicle with the radiator structure.
In order to solve the above-mentioned technical problem, the technical solution that the utility model uses is to provide a kind of radiator structure,
Comprising:
Shell；
It is set to the intracorporal radiator fan of the shell；And
The first air inlet and the second air inlet being oppositely arranged, and the first air outlet being oppositely arranged and the second outlet air
Mouthful, wherein the air inlet direction of first air inlet and second air inlet perpendicular to the plane where the radiator fan,
Co-planar where the air-out direction of first air outlet and second air outlet and the radiator fan.
In some embodiments, first air inlet, second air inlet, first air outlet and described second
Air outlet is connected to.
In some embodiments, the shell include bottom wall, the roof parallel with the bottom wall and the connection bottom wall and
Four side walls of roof, the bottom wall, roof and four side walls enclose and are set as an accommodating chamber, and the radiator fan is accommodated in institute
It states in accommodating chamber.
In some embodiments, the plane where the radiator fan is parallel to the bottom wall, first air inlet with
Second air inlet is respectively arranged on the roof and the bottom wall, the air inlet direction of first air inlet and described the
The air inlet of two air inlets is contrary and is directed to the radiator fan；First air outlet and second air outlet are distinguished
It is set on two opposite side walls in four side walls of the shell, the air-out direction of first air outlet and institute
The air-out direction of the second air outlet is stated on the contrary and backwards to the radiator fan.
In some embodiments, the radiator fan includes: the multiple leaves of wheel hub and uniform ring on the wheel hub
Piece；Air inlet area is formed between the multiple blade；Wherein, when the radiator fan works, air-flow is entered the wind by described first
Mouth and second air inlet enter the air inlet area of the radiator fan, and form the first affluent-dividing by the air inlet area
With the second affluent-dividing；First affluent-dividing and second affluent-dividing pass through first air outlet and described second respectively and go out
Air port blowout.
In some embodiments, the radiator fan is cylindrical, first air inlet and second air inlet
The cross-sectional area of the equal sized and respectively less than described radiator fan, the size of first air outlet and second air outlet
The longitudinal section area of the equal and respectively less than described radiator fan.
In some embodiments, first air inlet and second air inlet are circle, and the round diameter is less than
The diameter of two circular end faces of the radiator fan.
In some embodiments, the length of first air outlet and the second air outlet rectangle, the rectangle is less than institute
The diameter of two circular end faces of radiator fan is stated, the width of the rectangle is less than the height of the radiator fan.
In order to solve the above-mentioned technical problem, another technical solution that the utility model uses is to provide one kind, and nobody flies
Row device comprising fuselage, the horn being connected with the fuselage and the power device being arranged on the horn, feature exist
In being installed with radiator structure as described above in the fuselage.
In some embodiments, the plane where the fuselage of the unmanned vehicle and the plane where the radiator structure
In parallel.
In some embodiments, the fuselage on it position corresponding with first air inlet offer first into
Wind opening, position corresponding with second air inlet offers the second air inlet opening on the downside of it.
In some embodiments, first circuit board and/or second circuit board, first circuit are also equipped in the fuselage
Plate setting is open between the radiator structure in first air inlet, and/or, the second circuit board is arranged described
Between second air inlet opening and the radiator structure.
In some embodiments, first air outlet and second air outlet are respectively facing the two sides of the fuselage.
In some embodiments, position corresponding with first air outlet offers first and goes out the fuselage to the left
Wind opening, position corresponding with second air inlet offers the second outlet air opening on the right side of it.
In some embodiments, wind guide component, described wind guide component one end and the fuselage are additionally provided in the fuselage
It is connected, the other end is connected to first air inlet and/or second air inlet.
In some embodiments, vibration-damped component is additionally provided in the periphery of the radiator structure.
The beneficial effect of the utility model embodiment is: radiator structure provided by the embodiment of the utility model, has opposite
The first air inlet and the second air inlet being arranged, and the first air outlet and the second air outlet that are oppositely arranged, structure is simple,
And radiating efficiency with higher.Further, which is applied to unmanned vehicle, nobody can be correspondinglyd increase and flown
The heat dissipation performance of row device can save heat-dissipating space, and fly controlling nobody simultaneously as the structure of the radiator structure is simple
Heat radiation performance to the maximum extent while the overall weight of row device makes unmanned vehicle have higher safety reliability.
[Detailed description of the invention]
In order to illustrate more clearly of the technical solution of the utility model embodiment, the utility model embodiment will be retouched below
Attached drawing needed in stating is briefly described, it should be apparent that, the accompanying drawings in the following description is only the utility model
Some embodiments for those of ordinary skill in the art without any creative labor, can be with root
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is a kind of schematic perspective view of unmanned vehicle of the utility model wherein embodiment；
Fig. 2 is the cross-sectional view of unmanned vehicle shown in Fig. 1；
Fig. 3 is the main view of radiator structure in unmanned vehicle shown in Fig. 2；
Fig. 4 is the solid of radiator structure in unmanned vehicle shown in Fig. 2；
Fig. 5-a be Fig. 2 shown in unmanned vehicle forward or backward row when, by radiator structure air-flow move towards signal
Figure；
Fig. 5-b is unmanned vehicle shown in Fig. 2 along when direction flight to the left, walking by the air-flow of radiator structure in figure
To schematic diagram；
Fig. 5-c is unmanned vehicle shown in Fig. 2 along when direction flight to the right, walking by the air-flow of radiator structure in figure
To schematic diagram.
[specific embodiment]
It is carried out for the ease of understanding the utility model, below in conjunction with technical solution of the attached drawing to the application clear, complete
Ground description, it is clear that described embodiment is some embodiments of the present application, instead of all the embodiments.Based on the application
In embodiment, every other implementation obtained by those of ordinary skill in the art without making creative efforts
Example, shall fall in the protection scope of this application.
In the description of the present application, it should be noted that term " center ", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for describe the application and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation,
It is constructed and operated in a specific orientation, therefore should not be understood as the limitation to the application.In addition, term " first ", " second " are only
For descriptive purposes, it is not understood to indicate or imply relative importance.
In the description of the present application, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in application.
As long as in addition, the non-structure each other of technical characteristic involved in the application different embodiments disclosed below
It can be combined with each other at conflict.
Radiator structure provided by the embodiment of the utility model is a kind of structure for radiating to electronic equipment, is fitted
For many electronic equipments with heating elements such as circuit boards, common application scenarios are for instance that laptop, warm wind
Machine, sound equipment, projector, water dispenser, game machine, electric vehicle etc..Radiator structure provided by the embodiment of the utility model especially can be with
Be installed with applied to various inside in the loose impediment for the electronic component that circuit board etc. can generate heat, including but not limited to nobody
Aircraft (unmanned aerial vehicle, UAV), unmanned boat, mechanical arm, robot etc..By the utility model embodiment
In will be illustrated by taking unmanned vehicle as an example.The radiator structure is applied to unmanned vehicle, nobody can be correspondinglyd increase and flown
The heat dissipation performance of row device can save heat-dissipating space, and fly controlling nobody simultaneously as the structure of the radiator structure is simple
Heat radiation performance to the maximum extent while the overall weight of row device makes unmanned vehicle have higher safety reliability.
It is a kind of the utility model unmanned vehicle 10 that wherein an embodiment provides comprising machine also referring to Fig. 1
Body 100, the horn 200 being connected with fuselage 100, and the Power Component being connected with horn 200.The Power Component is installed on described
Horn 200, for providing power for the unmanned vehicle 10.The Power Component includes motor 300 and is mounted on motor 300
On propeller (not shown), each propeller is rotated to produce under the driving of corresponding motor 300 makes unmanned flight
The lift or thrust of device flight.In other possible embodiments, shown Power Component can also include setting in horn 200 or
The electric tuned plate (not shown) of the inside of fuselage 100, electric tuned plate are used for the throttle generated according to throttle control or throttle generator
Signal generates the flying speed or flight that the needs of unmanned vehicle 10 are obtained for controlling the motor control signal of motor speed
Posture.
Fig. 2 is the cross-sectional view of the fuselage 100 of unmanned vehicle 10 shown in FIG. 1.It is installed in the fuselage 100 by circuit
The control circuit component of the electronic components such as plate 400a, 400b composition, which includes multiple control modules, e.g.,
For controlling the Power Component work to control the flight control modules of 10 flight attitude of unmanned vehicle, it is used for as institute
State the locating module that unmanned vehicle 10 navigates, and the number for handling environmental information acquired in related airborne equipment
According to processing module etc..It is also installed with inside the fuselage 100 for being circuit board 400a, the radiator structure that 400b radiates
500.In a preferred embodiment, the plane where the fuselage 100 of the unmanned vehicle 10 and 500 place of radiator structure
Plane is parallel.In the utility model embodiment, the quantity of the circuit board is two pieces, that is, circuit board 400a and 400b, respectively
It is installed in the upper and lower ends of the radiator structure 500.In some other embodiment, more muti-piece is can be set in unmanned vehicle 10
Circuit board, or one piece of circuit board is only set.
As shown in Figure 3 and Figure 4, the main view and solid of the radiator structure 500 in the unmanned vehicle 10 of respectively Fig. 2
Figure.This kind of radiator structure 500 includes: shell 505, the radiator fan 506 being set in the shell 505 and the first air inlet
The 501, second air inlet 502 of mouth, the first air outlet 503 and the second air outlet 504.In the utility model embodiment, described
One air inlet 501 and second air inlet 502 are relatively arranged on the two sides up and down of shell 505,503 He of the first air outlet
Second air outlet 504 is relatively arranged on the left and right sides of shell 505.When radiator structure 500 is installed in unmanned vehicle 10
Fuselage 100 on after, the first air inlet 501 and the second air inlet 502 are respectively facing the upper side and lower side of fuselage, the first air outlet
503 and second air outlet 504 be respectively facing the left and right side of fuselage 100.
The shell 505 is flat cuboid comprising bottom wall 505b, the roof 505a parallel with the bottom wall 505b
With four side walls for connecting the bottom wall and roof, left side wall and right side wall therein are shown in figure as 505a and 505d, preceding
Side wall and rear wall are being not shown in the figure.The bottom wall 505b, roof 505a and four side walls enclose and are set as an accommodating chamber, institute
Radiator fan 506 is stated to be accommodated in the accommodating chamber.The radiator fan 506 is substantially in flat cylinder, You Tuzhong dotted line
The plane A of the 506 place plane of radiator fan is shown.Plane A where the radiator fan 506 is parallel to the bottom wall 505b
With roof 505a.
In some embodiments of the utility model, first air inlet 501 is respectively set with second air inlet 502
In on the roof 505a and the bottom wall 505b of the shell 505.As shown by the arrows in Figure 3, first air inlet 501
Air inlet direction with second air inlet 502 is perpendicular to the plane A where the radiator fan 506.Specifically, described first
The air inlet direction of air inlet 501 and the air inlet direction of second air inlet 502 are opposite each other, and are directed to the radiator fan
506。
In some embodiments of the utility model, first air outlet 503 is respectively set with second air outlet 504
In on two opposite side walls of the shell 505, that is, on left side wall 505c and right side wall 505d.As shown by the arrows in Figure 3,
Plane where the air-out direction of first air outlet 503 and second air outlet 504 and the radiator fan 506 is total
Face.Specifically, the air-out direction of first air outlet 503 and the air-out direction of second air outlet 504 are opposite each other, and
Backwards to the radiator fan 506.
Further regard to Fig. 4, in some embodiments of the utility model, first air inlet 501 and described second into
Equal sized, and the cross-sectional area of the respectively less than described radiator fan 506 of 502 (not shown) of air port.First air outlet
The longitudinal section area of the equal sized and respectively less than described radiator fan 506 of (not shown) and second air outlet 504.Specifically
Ground, in some embodiments of the utility model, first air inlet 501 and second air inlet 502 are circle, the circle
Shape diameter is less than the diameter of two circular end faces at the cylindrical radiator fan 506.In some embodiments of the utility model
In, first air outlet 503 and second air outlet 504 are rectangle, and the length of the rectangle is less than the radiator fan
The diameter of two circular end faces, the width of the rectangle are less than the height of the radiator fan.
The radiator fan 506 includes the multiple blades of wheel hub 506a and uniform ring on the wheel hub 506a
506b.Air inlet area is formed between the multiple blade 506b.When the radiator fan 506 work, due to radiator fan 506
Rotation, air-flow by first air inlet 501 and second air inlet 502 enter the radiator fan 506 it is described into
Wind area, and the first affluent-dividing and the second affluent-dividing are formed by the air inlet area, first affluent-dividing goes out by described first
Air port 503 is blown out, and second affluent-dividing is blown out by second air outlet.
Radiator structure 500 provided by the embodiment of the utility model, have the first air inlet 501 being oppositely arranged and second into
Air port 502, and the first air outlet 503 and the second air outlet 504 that are oppositely arranged, structure is simple, and with higher scattered
The thermal efficiency.Further, which is applied to unmanned vehicle 10, unmanned vehicle 10 can be correspondinglyd increase
Heat dissipation performance can save heat-dissipating space, and in control unmanned vehicle simultaneously as the structure of the radiator structure 500 is simple
Heat radiation performance to the maximum extent while 10 overall weight makes unmanned vehicle 10 have higher safety reliability.
In some embodiments of the utility model, first air inlet 501, second air inlet 502, described first
Air outlet 503 is connected to second air outlet 504.In 10 flight of unmanned vehicle, the machine of unmanned vehicle 10 is flowed through
A part of air-flow in the air-flow of body 100 need not detour from the surrounding of fuselage 100 again, but can pass through from the side of fuselage 100
Cross the other side that radiator structure 500 is flowed directly to fuselage 100.Such design can efficiently reduce unmanned vehicle 10 and fly
Windage when row.
Further, referring again to Fig. 2, the fuselage 100 of the unmanned vehicle 10 is entered the wind with described first on it
501 corresponding positions of mouth offer the first air inlet opening 101, and position corresponding with second air inlet 502 is opened on the downside of it
Equipped with the second air inlet opening 101.The first circuit board 400a is installed in the first air inlet opening 101 and the radiator structure
Between 500, the second circuit board 400b is installed between the second air inlet opening 102 and the radiator structure 500.Setting
First air inlet opening 101 and the second air inlet opening 101, so that the air draught in 100 external environment of fuselage can be by described
First air inlet opening 101 and the second air inlet opening 102 flow separately through the first air inlet 501 and the second air inlet of radiator structure 500
Mouth 502, into the inside of the radiator structure 500.Simultaneously as first circuit board 400a is installed in the first air inlet opening
Between 101 and the radiator structure 500, the air draught outside fuselage 100 enters machine by the first air inlet opening 101
When 100 inside of body, first circuit board 400a is first passed around, the heat on first circuit board 400a is taken away, passes through radiator structure
500 the first air inlet 501, into radiator structure 500 inside take a breath, such setting can be effectively by the first circuit
Heat as much as possible is taken away on plate 400a, radiates；Similarly, due to second circuit board 400b be installed in described second into
Between wind opening 102 and the radiator structure 500, the air draught outside fuselage 100 passes through the second air inlet opening 102
When into 100 inside of fuselage, second circuit board 400b is first passed around, the heat on second circuit board 400b is taken away, is passed through scattered
Second air inlet 502 of heat structure 500, into radiator structure 500 inside take a breath, such setting can be effectively by
Heat as much as possible is taken away on two circuit board 400b, radiates.
Also position corresponding with first air outlet 503 offers the first outlet air opening to the fuselage 100 to the left
103, position corresponding with second air inlet 504 offers the second outlet air opening 104 on the right side of it.The first outlet air is arranged to open
Mouth 103 and the second outlet air opening 104 enter to flow through the first air inlet 501 and the second air inlet 502 of radiator structure 500
Air-flow inside radiator structure 500, can after the first air outlet 503 and the second air outlet 504 for flowing through radiator structure 500,
Respectively outside the first outlet air opening 103 and the second outlet air opening 104 being arranged on fuselage 100, blowout to fuselage 100, from
And reach heat dissipation purpose.
In order to further increase the heat dissipation effect of radiator structure 500, in some embodiments of the utility model, such as Fig. 2 institute
Show, wind guide component 600, the inner wall phase of described 600 one end of wind guide component and the fuselage 100 are additionally provided in the fuselage 100
Even, the other end is connected to first air inlet 501.It should be understood that being only provided with connection in the utility model embodiment
It can only be arranged in other embodiments to the wind guide component 600 of the first air inlet 501 and be connected to leading for the second air inlet 502
Wind part is respectively connected to the first air inlet 501 and the second air inlet 502 alternatively, two groups of wind guide components can be set.Wind-guiding
The setting of component 600, so that the air draught outside fuselage 100 is easier, is more concentrated at inflow radiator structure 500, Neng Goujin
The heat dissipation performance of one step enhancing radiator structure 500.
It, can be in the periphery of the radiator structure 500 since radiator structure 500 is in some embodiments of the utility model
Vibration-damped component 700 is installed, to absorb the vibration generated when the radiator fan 506 of radiator structure 500 rotates, to reduce radiator fan
Influence of 506 vibration to other electronic components in unmanned vehicle 10, for example, especially reducing to Inertial Sensor Unit
(IMU) influence.
Please refer to shown in Fig. 5-a to Fig. 5-c, respectively illustrate unmanned vehicle 10 to it is front/rear flight, to the right flight, to
When left flight, the trend of the air-flow of its fuselage 100 is flowed through.As shown in Fig. 5-a, when unmanned vehicle 10 flies forward or backward
When, that is, when along direction flight perpendicular to paper, the air draught in 100 external environment of fuselage is respectively from the upper of fuselage 100
Side and downside flow into the inside of fuselage 100, after flowing through radiator structure 500, flow out from the left and right side of fuselage 100；Such as Fig. 5-b
It is shown, when unmanned vehicle 10 is to when its right direction flight, that is, along in figure when direction flight to the right, outside fuselage 100
Air draught in environment still flows into the inside of fuselage 100 from the upper side and lower side of fuselage 100 respectively, but flows through radiator structure
It is no longer to be flowed out respectively from the left and right side of fuselage 100, but flowed out from the left side of fuselage 100 after 500；Such as Fig. 5-c institute
Show, when unmanned vehicle 10 is to when its left direction flight, that is, along in figure when direction flight to the left, 100 external rings of fuselage
Air draught in border still flows into the inside of fuselage 100 from the upper side and lower side of fuselage 100 respectively, but flows through radiator structure
After 500, it will be flowed out from the right side of fuselage 100.Therefore, it is oppositely arranged on the first air outlet of 500 left and right side of radiator structure
503 and 504, and it is correspondingly arranged at the first outlet air opening 103 and the second outlet air opening 103 of 100 left and right side of fuselage, no
But heat dissipation can be played the role of, additionally it is possible to windage when 10 flight of unmanned vehicle is reduced, because flowing through unmanned vehicle 10
External environment air draught, it is not necessary to all got around around fuselage 100, but some air-flow can be with diameter flow
Inside through fuselage, that is to say, that
When unmanned vehicle 10 is to when its right direction flight, the air draught of the external environment of unmanned vehicle 10 is flowed through
In some air-flow can be open followed by second outlet air on the right side of fuselage 100 104,500 right side wall of radiator structure
The first of 100 left side of the second air outlet 504 of 505d, the first air outlet 503 of 500 left side wall 505c of radiator structure and fuselage goes out
Wind opening 103, eventually off unmanned vehicle 10, to reduce windage when 10 flight of unmanned vehicle；Similarly, work as nothing
People's aircraft 10 flows through some in the air draught of the external environment of unmanned vehicle 10 to when its left direction flight
Air-flow can be followed by the first outlet air of the first outlet air opening 103,500 left side wall 505c of radiator structure in 100 left side of fuselage
The second outlet air opening 104 on 100 right side of mouth 503, the second air outlet 504 of 500 right side wall 505d of radiator structure and fuselage, finally
Unmanned vehicle 10 is left, to reduce windage when 10 flight of unmanned vehicle.
Radiator structure provided by the embodiment of the utility model has the first air inlet and the second air inlet being oppositely arranged,
And the first air outlet and the second air outlet being oppositely arranged, structure is simple, and radiating efficiency with higher.Further
The radiator structure is applied to unmanned vehicle, can correspondingly increase the heat dissipation performance of unmanned vehicle by ground, simultaneously as should
The structure of radiator structure is simple, can save heat-dissipating space, and maximum limit while controlling the overall weight of unmanned vehicle
Degree ground heat radiation performance, makes unmanned vehicle have higher safety reliability.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model
Protection scope within.
It finally goes back it is noted that above embodiments are only to illustrate the technical solution of the utility model, rather than limit it
System；Under the thinking of the utility model, group can also be carried out between the technical characteristic in above embodiments or different embodiments
It closes, step can realize with random order, and there are many other variations of the different aspect of the utility model as described above,
For simplicity, they are not provided in details；Although the utility model is described in detail with reference to the foregoing embodiments,
Those skilled in the art should understand that: it can still repair technical solution documented by foregoing embodiments
Change or equivalent replacement of some of the technical features；And these are modified or replaceed, and do not make corresponding technical solution
Essence departs from the scope of the technical solutions of the embodiments of the present invention.
Claims (16)
1. a kind of radiator structure (500) characterized by comprising
Shell (505)；
The radiator fan (506) being set in the shell (505)；And
The first air inlet (501) and the second air inlet (502) being oppositely arranged, and the first air outlet (503) being oppositely arranged
With the second air outlet (504), wherein the air inlet direction of first air inlet (501) and second air inlet (502) is vertical
Plane where the radiator fan (506), the outlet air of first air outlet (503) and second air outlet (504)
Co-planar where direction and the radiator fan (506).
2. radiator structure (500) according to claim 1, which is characterized in that first air inlet (501), described
Two air inlets (502), first air outlet (503) are connected to second air outlet (504).
3. radiator structure (500) according to claim 1, which is characterized in that the shell (505) includes bottom wall
Four of (505b), the roof parallel with the bottom wall (505b) (505a) and the connection bottom wall (505b) and roof (505a)
Side wall, the bottom wall (505b), roof (505a) and four side walls enclose and are set as an accommodating chamber, the radiator fan (506)
It is accommodated in the accommodating chamber.
4. radiator structure (500) according to claim 3, which is characterized in that the plane where the radiator fan (506)
It is parallel to the bottom wall (505b), first air inlet (501) and second air inlet (502) are respectively arranged at the top
On wall (505a) and the bottom wall (505b), the air inlet direction of first air inlet (501) and second air inlet (502)
Air inlet it is contrary and be directed to the radiator fan (506)；First air outlet (503) and second air outlet
(504) it is respectively arranged on two opposite side walls in four side walls of the shell (505), first air outlet
(503) air-out direction is opposite with the air-out direction of second air outlet (504) and backwards to the radiator fan.
5. radiator structure (500) according to any one of claim 1 to 4, which is characterized in that the radiator fan
It (506) include: the multiple blades (506b) of wheel hub (506a) and uniform ring on the wheel hub (506a)；It is the multiple
Air inlet area is formed between blade (506b)；Wherein, when the radiator fan (506) work, air-flow is entered the wind by described first
Mouth (501) and second air inlet (502) enter the air inlet area of the radiator fan (506), and pass through the air inlet
Area forms the first affluent-dividing and the second affluent-dividing；First affluent-dividing and second affluent-dividing pass through described first respectively and go out
Air port (503) and second air outlet (504) blowout.
6. radiator structure (500) according to claim 1, which is characterized in that the radiator fan (506) is cylindrical,
First air inlet (501) and the equal sized and respectively less than described radiator fan (506) of second air inlet (502)
The equal sized and respectively less than described heat dissipation of cross-sectional area, first air outlet (503) and second air outlet (504)
The longitudinal section area of fan (506).
7. radiator structure (500) according to claim 6, which is characterized in that first air inlet (501) and described
Two air inlets (502) are circle, and the round diameter is less than the diameter of two circular end faces of the radiator fan (506).
8. radiator structure (500) according to claim 6 or 7, which is characterized in that first air outlet (503) and institute
Stating the second air outlet (504) is rectangle, and the length of the rectangle is less than the diameter of two circular end faces of the radiator fan (506),
The width of the rectangle is less than the height of the radiator fan (506).
9. a kind of unmanned vehicle (10), including fuselage (100), the horn (200) being connected with the fuselage (100) and setting
Power device on the horn (200), which is characterized in that be installed with such as claim 1 to 8 in the fuselage (100)
Any one of described in radiator structure (500).
10. unmanned vehicle (10) according to claim 9, which is characterized in that the fuselage of the unmanned vehicle (10)
(100) plane where is parallel with plane (A) where the radiator structure (500).
11. unmanned vehicle (10) according to claim 9, which is characterized in that the fuselage (100) on it with institute
State the corresponding position of the first air inlet (501) offer the first air inlet opening (101), on the downside of it with second air inlet
(502) corresponding position offers the second air inlet opening (102).
12. unmanned vehicle (10) according to claim 11, which is characterized in that be also equipped with the in the fuselage (100)
One circuit board (400a) and/or second circuit board (400b), first circuit board (400a) setting are opened in first air inlet
Between mouthful (101) and the radiator structure (500), and/or, the second circuit board (400b) be arranged described second into
Wind is open (102) between the radiator structure (500).
13. unmanned vehicle (10) according to claim 9, which is characterized in that first air outlet (503) and described
Second air outlet (504) is respectively facing the two sides of the fuselage.
14. the unmanned vehicle according to any one of claim 9 to 13 (10), which is characterized in that the fuselage (100)
To the left position corresponding with the first air outlet (503) offer the first outlet air opening (103), on the right side of it with it is described
The corresponding position of second air outlet (504) offers the second outlet air opening (104).
15. unmanned vehicle (10) according to claim 14, which is characterized in that be additionally provided in the fuselage (100)
Wind guide component (600), described wind guide component (600) one end are connected with the fuselage (100), the other end be connected to described first into
Air port (501) and/or second air inlet (502).
16. unmanned vehicle (10) according to claim 14, which is characterized in that in the outer of the radiator structure (500)
It is additionally provided with vibration-damped component (700) week.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820980901.5U CN208868303U (en) | 2018-06-25 | 2018-06-25 | Radiator structure and unmanned vehicle |
| PCT/CN2019/090936 WO2020001273A1 (en) | 2018-06-25 | 2019-06-12 | Heat dissipation structure and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820980901.5U CN208868303U (en) | 2018-06-25 | 2018-06-25 | Radiator structure and unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208868303U true CN208868303U (en) | 2019-05-17 |
Family
ID=66462551
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820980901.5U Active CN208868303U (en) | 2018-06-25 | 2018-06-25 | Radiator structure and unmanned vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN208868303U (en) |
| WO (1) | WO2020001273A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020001273A1 (en) * | 2018-06-25 | 2020-01-02 | 深圳市道通智能航空技术有限公司 | Heat dissipation structure and unmanned aerial vehicle |
| CN112154103A (en) * | 2019-09-24 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| WO2021232258A1 (en) * | 2020-05-20 | 2021-11-25 | 深圳元戎启行科技有限公司 | Automatic driving device, and computing system used for automatic driving device |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112936347A (en) * | 2021-03-31 | 2021-06-11 | 追创科技(苏州)有限公司 | Fuselage and quadruped robot |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5056307A (en) * | 1990-05-25 | 1991-10-15 | The United States Of America As Represented By The Secretary Of The Air Force | Exhaust nozzle cooling utilizing total engine flow |
| CN1309065C (en) * | 2003-01-07 | 2007-04-04 | 华宇电脑股份有限公司 | Radiation device for electronic element |
| CN2800357Y (en) * | 2005-04-28 | 2006-07-26 | 仁宝电脑工业股份有限公司 | Heat radiation module |
| CN100529413C (en) * | 2006-11-17 | 2009-08-19 | 富准精密工业(深圳)有限公司 | Centrifugal fan, heat radiation device possessing the centrifugal fan and electronic device using the heat radiation device |
| CN101725564B (en) * | 2008-10-16 | 2013-06-05 | 富准精密工业(深圳)有限公司 | Centrifugal fan and radiating device using same |
| CN203854852U (en) * | 2014-03-28 | 2014-10-01 | 浙江省第二测绘院 | Rain-proof cooling device for unmanned aerial vehicle |
| CN206394888U (en) * | 2016-12-19 | 2017-08-11 | 重庆零度智控智能科技有限公司 | Unmanned plane |
| CN208868303U (en) * | 2018-06-25 | 2019-05-17 | 深圳市道通智能航空技术有限公司 | Radiator structure and unmanned vehicle |
-
2018
- 2018-06-25 CN CN201820980901.5U patent/CN208868303U/en active Active
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2019
- 2019-06-12 WO PCT/CN2019/090936 patent/WO2020001273A1/en active Application Filing
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020001273A1 (en) * | 2018-06-25 | 2020-01-02 | 深圳市道通智能航空技术有限公司 | Heat dissipation structure and unmanned aerial vehicle |
| CN112154103A (en) * | 2019-09-24 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| WO2021232258A1 (en) * | 2020-05-20 | 2021-11-25 | 深圳元戎启行科技有限公司 | Automatic driving device, and computing system used for automatic driving device |
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| Publication number | Publication date |
|---|---|
| WO2020001273A1 (en) | 2020-01-02 |
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Address after: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Patentee after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Patentee before: AUTEL ROBOTICS Co.,Ltd. |
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