CN109301900A - A kind of certainly cooling power module of unmanned plane - Google Patents
A kind of certainly cooling power module of unmanned plane Download PDFInfo
- Publication number
- CN109301900A CN109301900A CN201811236529.8A CN201811236529A CN109301900A CN 109301900 A CN109301900 A CN 109301900A CN 201811236529 A CN201811236529 A CN 201811236529A CN 109301900 A CN109301900 A CN 109301900A
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- CN
- China
- Prior art keywords
- unmanned plane
- shell
- power module
- radiator fan
- module
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- 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.)
- Pending
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 14
- 238000000034 method Methods 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 2
- 238000005457 optimization Methods 0.000 description 6
- 230000017525 heat dissipation Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000005662 electromechanics Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0068—Battery or charger load switching, e.g. concurrent charging and load supply
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/2089—Modifications to facilitate cooling, ventilating, or heating for power electronics, e.g. for inverters for controlling motor
- H05K7/20909—Forced ventilation, e.g. on heat dissipaters coupled to components
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The invention discloses a kind of certainly cooling power modules of unmanned plane, including shell, radiator fan and cable mounting head, the radiator fan is two groups, radiator fan described in two groups is installed in the top of the shell, the cable mounting head is fixed on the one end side of the shell, the shell is provided with outlet far from one end bottom middle-end of the cable mounting head, the case top two sides are mounted on radiating fin, the radiator fan two sides are fixedly connected with the radiating fin of two sides, the housing bottom both ends are provided with module fixing groove in the width direction.This, which is tethered at power module and can change common unmanned plane at any time, is adapted as being tethered at unmanned plane, and common unmanned plane is changeed back in the state of not needing long endurance.Be tethered at power supply module and battery power supply module be free to mutually replace and use, the same unmanned plane using when only installation can be tethered at power supply module or battery power supply module, save the weight in unmanned plane use.
Description
Technical field
The present invention relates to a kind of power modules, and in particular to a kind of certainly cooling power module of unmanned plane belongs to unmanned electromechanics
Source technology field.
Background technique
Unmanned plane is to develop a kind of very fast aircraft now, is applied to all trades and professions.It is wherein tethered at unmanned plane, more
Favored with the characteristics of its long endurance by many special industries, such as traffic, communication, fire-fighting and security protection.
But the existing unmanned plane that is tethered on the market is the model specially designed, has two sets of power supply modules on an airplane, both
There is battery power supply module, and be tethered at power supply module, not only increase the volume of aircraft in this way, the even more consumption of increase user is negative
Load.Battery power supply module and it being tethered at the mutually independent use of power supply module, limitation is larger, and heat is easy to produce in,
In the normal use of the internal influence power supply module of unmanned plane, service efficiency and service life are affected thermal accumlation.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned planes from cooling power module, and can solve has on existing unmanned plane
Two sets of power supply modules, existing battery power supply module, and it is tethered at power supply module, not only increase the volume of aircraft in this way, even more increases
The consumption of user is added to bear.Battery power supply module and it is tethered at the mutually independent use of power supply module, limitation is larger, and uses
In be easy to produce heat, thermal accumlation service efficiency and uses the longevity in the normal use of the internal influence power supply module of unmanned plane
The technical issues of life is affected.
The purpose of the present invention can be achieved through the following technical solutions:
A kind of unmanned plane is from cooling power module, including shell, radiator fan and cable mounting head, the radiator fan
Two groups, radiator fan described in two groups is installed in the top of the shell, and the cable mounting head is fixed on the one of the shell
End side surface, the shell are provided with outlet, the case top two far from one end bottom middle-end of the cable mounting head
Side is mounted on radiating fin, and the radiator fan two sides are fixedly connected with the radiating fin of two sides, the housing bottom
Both ends are provided with module fixing groove in the width direction.
Preferably, the outlet matches with the battery socket inside unmanned plane.
Preferably, the module fixing groove matches with the battery fixing groove inside unmanned plane.
Preferably, several fixation holes are provided at the top of the radiating fin, and the both ends of radiator fan pass through screw
It is connected and fixed hole.
Preferably, the enclosure interior is cavity setting, and cavity inside is equipped with power supply inverter.
Preferably, the radiator fan is electrically connect with power supply inverter, and power supply inverter is electrically connected electricity
Cable mounting head and outlet.
Preferably, the specific steps of the power module application method include:
Step 1: one end of power module is electrically connected by the cable mounting head and cable connection, cable with the city 220v
It connects, the other end is directly inserted into the inside of unmanned machine battery socket by the outlet of shell one end, replaces unmanned machine battery
Position, shell is connected to the inside of unmanned plane using the module fixing groove of bottom；
Step 2: in work, when power module is worked, radiator fan starts work therewith, reduces power module
Operating temperature, continue working it.
Beneficial effects of the present invention:
1, this, which is tethered at power module and can change common unmanned plane at any time, is adapted as being tethered at unmanned plane, is not needing long boat
When in the state of change back common unmanned plane.Being tethered at power supply module and battery power supply module be free to mutually replacement and makes
With, the same unmanned plane using when only installation can be tethered at power supply module or battery power supply module, saving unmanned plane makes
Weight in reduces volume.
2 and this be tethered at power module and automatic heat radiation can be carried out by the radiator fan at top in use, improve power supply
Module radiating efficiency in use, the heat generated in work are not easy to be deposited in the inside of unmanned plane, nobody is eupraxic
It uses.The service life of power module is extended, and working environment is optimized.
Detailed description of the invention
In order to facilitate the understanding of those skilled in the art, the present invention will be further described below with reference to the drawings.
Fig. 1 is overall structure of the present invention.
Fig. 2 is the main view of Fig. 1 of the present invention.
Fig. 3 is the top view of Fig. 1 of the present invention.
1, shell；2, outlet；3, cable mounting head；4, fixation hole；5, radiating fin；6, radiator fan；7, module
Fixing groove.
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with embodiment, it is clear that described reality
Applying example is only a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, this field is general
Logical technical staff all other embodiment obtained without creative efforts belongs to what the present invention protected
Range.
It please refers to shown in Fig. 1-3, a kind of certainly cooling power module of unmanned plane, including shell 1, radiator fan 6 and cable peace
Head 3 is filled, radiator fan 6 is two groups, and two groups of radiator fans 6 are installed in the top of shell 1, and cable mounting head 3 is fixed on shell 1
One end side, shell 1 is provided with outlet 2 far from one end bottom middle-end of cable mounting head 3, and 1 top two sides of shell are equal
Radiating fin 5 is installed, 6 two sides of radiator fan are fixedly connected with the radiating fin 5 of two sides, and 1 bottom both ends of shell are along width side
To module fixing groove 7 is provided with, work, and nothing can be replaced mutually with the battery module inside unmanned plane by being tethered at power module
People's eupraxic use is quickly radiated by radiator fan 6 and radiating fin 5 in use.
As a kind of technical optimization scheme of the invention, outlet 2 matches with the battery socket inside unmanned plane, electricity
Source socket 2 can be connect with the battery socket inside unmanned plane, nobody eupraxic use, can connect battery power supply module again
It can connect and be tethered at power supply module.
As a kind of technical optimization scheme of the invention, module fixing groove 7 and the battery fixing groove phase inside unmanned plane
Match, being tethered at power module can be clamped by module fixing groove 7 with the battery fixing groove inside unmanned plane, so that being tethered at power supply
Module can be in the storage of unmanned plane internal stability.
As a kind of technical optimization scheme of the invention, several fixation holes 4 are provided at the top of radiating fin 5, and radiate
The both ends of fan 6 are connected by screw to fixation hole 4, and radiator fan 6, which is fixed on 5 top of radiating fin, normally to radiate,
And radiating fin 5 can improve the efficiency of heat dissipation.
As a kind of technical optimization scheme of the invention, it is arranged inside shell 1 for cavity, and cavity inside is equipped with power supply
Inverter, power supply inverter are mounted on inside shell 1 and save space, reduce the volume of whole device, and can be by outside
Alternating current is converted to direct current and uses for unmanned plane.
As a kind of technical optimization scheme of the invention, radiator fan 6 is electrically connect with power supply inverter, and power supply
Inverter is electrically connected cable mounting head 3 and outlet 2, power supply inverter convert alternating current to direct current after can be
Unmanned plane and radiator fan 6 provide electric power.
As a kind of technical optimization scheme of the invention, the specific steps of the power module application method include:
Step 1: by one end of power module by cable mounting head 3 and cable connection, cable is electrically connected with the city 220v,
The other end is directly inserted into the inside of unmanned machine battery socket by the outlet 2 of 1 one end of shell, replaces unmanned machine battery
Position, shell 1 are connected to the inside of unmanned plane using the module fixing groove 7 of bottom；
Step 2: in work, when power module is worked, radiator fan 6 starts work therewith, reduces power module
Operating temperature, continue working it.
In the use of the present invention, the battery inside the unmanned plane for needing to use for a long time is taken out, one end of power module
By cable mounting head 3 and cable connection, cable is electrically connected with the city 220v, and the other end is straight by the outlet 2 of 1 one end of shell
The inside for being inserted into unmanned machine battery socket is connect, the position of unmanned machine battery is replaced.Shell 1 utilizes the module fixing groove 7 of bottom
It is connected to the inside of unmanned plane.In work, when power module is worked, radiator fan 6 starts work therewith, reduces power supply
The operating temperature of module, continues working it.Radiating fin 5 increases the area of heat dissipation, improves the speed of heat dissipation, improves in work
The efficiency of heat dissipation.External cable delivers power to inside the power supply inverter of model ACM16S50CF in work, passes through
It is transported to radiator fan 6 and outlet 2 after crossing inversion, provides electric power for unmanned plane.
Present invention disclosed above preferred embodiment is only intended to help to illustrate the present invention.There is no detailed for preferred embodiment
All details are described, are not limited the invention to the specific embodiments described.Obviously, according to the content of this specification,
It can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to better explain the present invention
Principle and practical application, so that skilled artisan be enable to better understand and utilize the present invention.The present invention is only
It is limited by claims and its full scope and equivalent.
Claims (7)
1. a kind of certainly cooling power module of unmanned plane, it is characterised in that: including shell (1), radiator fan (6) and cable mounting head
(3), the radiator fan (6) is two groups, and radiator fan described in two groups (6) is installed in the top of the shell (1), the electricity
Cable mounting head (3) is fixed on the one end side of the shell (1), the one end of the shell (1) far from the cable mounting head (3)
Bottom middle-end is provided with outlet (2), and two sides are mounted on radiating fin (5), the radiator fan at the top of the shell (1)
(6) two sides are fixedly connected with the radiating fin (5) of two sides, and shell (1) the bottom both ends are provided in the width direction
Module fixing groove (7).
2. a kind of certainly cooling power module of unmanned plane according to claim 1, it is characterised in that: the outlet (2)
Match with the battery socket inside unmanned plane.
3. a kind of certainly cooling power module of unmanned plane according to claim 1, it is characterised in that: the module fixing groove
(7) match with the battery fixing groove inside unmanned plane.
4. a kind of certainly cooling power module of unmanned plane according to claim 1, it is characterised in that: the radiating fin (5)
Top is provided with several fixation holes (4), and the both ends of radiator fan (6) are connected by screw to fixation hole (4).
5. a kind of certainly cooling power module of unmanned plane according to claim 1, it is characterised in that: the shell (1) is internal
It is arranged for cavity, and cavity inside is equipped with power supply inverter.
6. a kind of certainly cooling power module of unmanned plane according to claim 1, it is characterised in that: the radiator fan (6)
It is electrically connect with power supply inverter, and power supply inverter is electrically connected cable mounting head (3) and outlet (2).
7. a kind of certainly cooling power module of unmanned plane according to claim 1, which is characterized in that power module user
The specific steps of method include:
Step 1: one end of power module is electrically connected by the cable mounting head (3) and cable connection, cable with the city 220v
It connects, the other end is directly inserted into the inside of unmanned machine battery socket by the outlet (2) of shell (1) one end, replaces nobody
The position of machine battery, shell (1) are connected to the inside of unmanned plane using the module fixing groove (7) of bottom；
Step 2: in work, when power module is worked, radiator fan (6) starts work therewith, reduces power module
Operating temperature continues working it.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811236529.8A CN109301900A (en) | 2018-10-23 | 2018-10-23 | A kind of certainly cooling power module of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811236529.8A CN109301900A (en) | 2018-10-23 | 2018-10-23 | A kind of certainly cooling power module of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109301900A true CN109301900A (en) | 2019-02-01 |
Family
ID=65158473
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811236529.8A Pending CN109301900A (en) | 2018-10-23 | 2018-10-23 | A kind of certainly cooling power module of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109301900A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113964431A (en) * | 2021-11-24 | 2022-01-21 | 杭州铂科电子有限公司 | Novel AC-DC forced air cooling high-voltage unmanned aerial vehicle power supply |
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| CN205248402U (en) * | 2015-12-26 | 2016-05-18 | 武汉智能鸟无人机有限公司 | Battery heat radiation structure reaches unmanned aerial vehicle who contains it |
| CN105836153A (en) * | 2016-03-17 | 2016-08-10 | 北京大工科技有限公司 | Mooring system of unmanned aerial vehicle |
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| CN107140229A (en) * | 2017-04-27 | 2017-09-08 | 陶霖密 | One kind is tethered at unmanned plane energy supplyystem |
| WO2018053823A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Heat dispersion structure, and unmanned aerial vehicle provided with heat dispersion structure |
| US20180155022A1 (en) * | 2016-12-05 | 2018-06-07 | Kevin Hess | System for Converting a Safeguarded Free Flight Onboard Battery-Powered Drone to a Ground-Powered Tethered Drone |
| CN108516096A (en) * | 2018-05-31 | 2018-09-11 | 珠海市双捷科技有限公司 | High-low voltage switching device, unmanned plane and its switching method |
| CN208874325U (en) * | 2018-10-23 | 2019-05-17 | 安徽佳讯皖之翼科技有限公司 | A kind of certainly cooling power module of unmanned plane |
-
2018
- 2018-10-23 CN CN201811236529.8A patent/CN109301900A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205248402U (en) * | 2015-12-26 | 2016-05-18 | 武汉智能鸟无人机有限公司 | Battery heat radiation structure reaches unmanned aerial vehicle who contains it |
| CN105836153A (en) * | 2016-03-17 | 2016-08-10 | 北京大工科技有限公司 | Mooring system of unmanned aerial vehicle |
| WO2018053823A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Heat dispersion structure, and unmanned aerial vehicle provided with heat dispersion structure |
| CN106659071A (en) * | 2016-11-29 | 2017-05-10 | 合肥赛为智能有限公司 | Heat dissipation bottom plate, power source module with same and unmanned aerial vehicle |
| US20180155022A1 (en) * | 2016-12-05 | 2018-06-07 | Kevin Hess | System for Converting a Safeguarded Free Flight Onboard Battery-Powered Drone to a Ground-Powered Tethered Drone |
| CN107140229A (en) * | 2017-04-27 | 2017-09-08 | 陶霖密 | One kind is tethered at unmanned plane energy supplyystem |
| CN108516096A (en) * | 2018-05-31 | 2018-09-11 | 珠海市双捷科技有限公司 | High-low voltage switching device, unmanned plane and its switching method |
| CN208874325U (en) * | 2018-10-23 | 2019-05-17 | 安徽佳讯皖之翼科技有限公司 | A kind of certainly cooling power module of unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113964431A (en) * | 2021-11-24 | 2022-01-21 | 杭州铂科电子有限公司 | Novel AC-DC forced air cooling high-voltage unmanned aerial vehicle power supply |
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