CN106505703A - A kind of ground charger of unmanned plane - Google Patents
A kind of ground charger of unmanned plane Download PDFInfo
- Publication number
- CN106505703A CN106505703A CN201611069374.4A CN201611069374A CN106505703A CN 106505703 A CN106505703 A CN 106505703A CN 201611069374 A CN201611069374 A CN 201611069374A CN 106505703 A CN106505703 A CN 106505703A
- Authority
- CN
- China
- Prior art keywords
- charger
- unmanned plane
- ground
- charging
- temperature
- 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.)
- Pending
Links
- HEZMWWAKWCSUCB-PHDIDXHHSA-N (3R,4R)-3,4-dihydroxycyclohexa-1,5-diene-1-carboxylic acid Chemical compound O[C@@H]1C=CC(C(O)=O)=C[C@H]1O HEZMWWAKWCSUCB-PHDIDXHHSA-N 0.000 claims description 6
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 abstract description 9
- 229910052744 lithium Inorganic materials 0.000 abstract description 9
- 229920000642 polymer Polymers 0.000 abstract description 9
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Classifications
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- 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
- H02J7/02—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- H02J7/0021—
-
- H02J7/0027—
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
A kind of ground charger of unmanned plane is disclosed, which can solve the problem that high-capacity lithium polymer battery group charging interval longer problem, unmanned plane power battery pack charge efficiency is substantially improved, improve the working performance of UAS；The lithium polymer battery group (3S 6S) of compatible different size, reduces charger kind and quantity, reduces cost simultaneously.The ground charger of this unmanned plane, it include direct-flow voltage regulation source, charger, charged in parallel plate；220V alternating currents arrive charger through the unidirectional current that direct-flow voltage regulation source exports 2900W, 48V, and charger arranged using paralleling model, and charger exports the electric current of highest 70A to charged in parallel plate, and charging panel expands four charging inlets in parallel.
Description
Technical field
The invention belongs to the technical field of unmanned plane, more particularly to a kind of ground charger of unmanned plane.
Background technology
At present, UAS power is more and more from lithium polymer battery group, especially multi-rotor unmanned aerial vehicle and
Small-sized fixed-wing unmanned plane.As the capacity of power battery pack is increasing and battery kind increases, integrated charger and
Quick charge capability becomes an important indicator of unmanned plane, directly governs the working performance of UAS.
And about 3 hours one group of power battery pack charging intervals of typically electronic unmanned plane, this just directly constrains unmanned plane
Outfield working performance.Using the battery of plurality of specifications, need to be equipped with multiple chargers, high cost, portability are poor.
Content of the invention
The present invention technology solve problem be：Overcome the deficiencies in the prior art, there is provided charge and set in a kind of ground of unmanned plane
Standby, which can solve the problem that high-capacity lithium polymer battery group charging interval longer problem, unmanned plane power battery pack is substantially improved and fills
Electrical efficiency, improves the working performance of UAS；The lithium polymer battery group (3S-6S) of compatible different size, reduces simultaneously
Charger kind and quantity, reduces cost.
The present invention technical solution be：The ground charger of this unmanned plane, which includes direct-flow voltage regulation source, charging
Device, charged in parallel plate；220V alternating currents export the unidirectional current of 2900W, 48V to charger through direct-flow voltage regulation source, and charger makes
Arranged with paralleling model, to charged in parallel plate, charging panel expands four and fills the electric current of charger output highest 70A in parallel
Electrical interface.
220V alternating currents of the present invention export the unidirectional current of 2900W, 48V to charger through direct-flow voltage regulation source, and charger makes
Arranged with paralleling model, to charged in parallel plate, charging panel expands four and fills the electric current of charger output highest 70A in parallel
Electrical interface, therefore, it is possible to solve high-capacity lithium polymer battery group charging interval longer problem, is substantially improved unmanned plane power current
Pond group charge efficiency, improves the working performance of UAS；While the lithium polymer battery group (3S- of compatible different size
6S), charger kind and quantity, reduces cost are reduced.
Description of the drawings
Fig. 1 shows the structural representation of a preferred embodiment of the ground charger of the unmanned plane according to the present invention
Figure.
Fig. 2 shows the schematic diagram of the intelligent temperature control circuit of the ground charger of the unmanned plane according to the present invention.
Specific embodiment
From figure 1 it appears that the ground charger of this unmanned plane, which includes direct-flow voltage regulation source, charger, parallel connection
Charging panel；220V alternating currents export the unidirectional current of 2900W, 48V to charger through direct-flow voltage regulation source, and charger is using simultaneously gang mould
Formula is arranged, and to charged in parallel plate, charging panel expands four charging inlets to the electric current of charger output highest 70A in parallel.
220V alternating currents of the present invention export the unidirectional current of 2900W, 48V to charger through direct-flow voltage regulation source, and charger makes
Arranged with paralleling model, to charged in parallel plate, charging panel expands four and fills the electric current of charger output highest 70A in parallel
Electrical interface, therefore, it is possible to solve high-capacity lithium polymer battery group charging interval longer problem, is substantially improved unmanned plane power current
Pond group charge efficiency, improves the working performance of UAS；While the lithium polymer battery group (3S- of compatible different size
6S), charger kind and quantity, reduces cost are reduced.
In addition, the ground charger of the unmanned plane also includes some charging transit cables, its one end and charging inlet
It is connected and the other end is connected with the power battery pack of unmanned plane.By designing different types of charging transit cable, can be with compatibility
The set of cells of 3S-6S difference core numbers, successfully realizes the generalization of the ground charger of the unmanned plane.
In addition, the ground charger of the unmanned plane also includes charging case, direct-flow voltage regulation source, charger, charged in parallel plate
It is installed in charging case.Can so make the ground charger of the unmanned plane dust-proof, greatly prolong service life.
In addition, the ground charger of the unmanned plane also includes intelligent temperature control circuit, its be located at direct-flow voltage regulation source and
Between charger, intelligent temperature control circuit includes temperature sensor, temperature detect switch (TDS), DCDC modules, the first fan, the second wind
Fan, the temperature in temperature sensor senses charging case start temperature detect switch (TDS), DCDC modules, after assigned temperature is reached so as to band
Dynamic first fan, the second fan work, disconnect temperature detect switch (TDS), DCDC modules when less than assigned temperature, so that the first fan,
Second fan quits work.Ensure that the charger is used safely under the hot environment of outfield.
In addition, the assigned temperature is 65 DEG C.
Six rotor wing unmanned aerial vehicle of Hai Ying airlines model, is electrokinetic cell using this Universal high-power charging case equipment
Charge with device battery, solve the problems, such as power battery pack quick charge so that the operation effect of certain six rotor wing unmanned aerial vehicle of model
Rate is obviously improved.
The above, is only presently preferred embodiments of the present invention, not makees any pro forma restriction to the present invention, every according to
According to any simple modification, equivalent variations and modification that the technical spirit of the present invention is made to above example, still belong to the present invention
The protection domain of technical scheme.
Claims (5)
1. the ground charger of a kind of unmanned plane, it is characterised in that：Which includes direct-flow voltage regulation source, charger, charged in parallel plate；
220V alternating currents export the unidirectional current of 2900W, 48V to charger through direct-flow voltage regulation source, and charger is arranged using paralleling model,
The electric current of charger output highest 70A expands four charging inlets to charged in parallel plate, in parallel charging panel.
2. the ground charger of unmanned plane according to claim 1, it is characterised in that：Charge and set in the ground of the unmanned plane
For some charging transit cables are also included, its one end is connected with charging inlet and the other end is connected with the power battery pack of unmanned plane
Connect.
3. the ground charger of unmanned plane according to claim 2, it is characterised in that：Charge and set in the ground of the unmanned plane
Standby also include that charging case, direct-flow voltage regulation source, charger, charged in parallel plate are installed in charging case.
4. the ground charger of unmanned plane according to claim 3, it is characterised in that：Charge and set in the ground of the unmanned plane
For intelligent temperature control circuit is also included, which is located between direct-flow voltage regulation source and charger, and intelligent temperature control circuit includes temperature
Degree sensor, temperature detect switch (TDS), DCDC modules, the first fan, the second fan, the temperature in temperature sensor senses charging case, when
Start temperature detect switch (TDS), DCDC modules after reaching assigned temperature, so as to drive the first fan, the second fan work, when less than specified
Temperature detect switch (TDS), DCDC modules is disconnected during temperature, so that the first fan, the second fan quit work.
5. the ground charger of unmanned plane according to claim 3, it is characterised in that：The assigned temperature is 65 DEG C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611069374.4A CN106505703A (en) | 2016-11-29 | 2016-11-29 | A kind of ground charger of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611069374.4A CN106505703A (en) | 2016-11-29 | 2016-11-29 | A kind of ground charger of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106505703A true CN106505703A (en) | 2017-03-15 |
Family
ID=58328878
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611069374.4A Pending CN106505703A (en) | 2016-11-29 | 2016-11-29 | A kind of ground charger of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106505703A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108023394A (en) * | 2017-12-27 | 2018-05-11 | 国网福建省电力有限公司 | Patrol unmanned locomotive team calamity is for vehicle-mounted emergency charge method |
| CN108495767A (en) * | 2017-04-13 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Charger and unmanned plane portable unit |
| WO2018205166A1 (en) * | 2017-05-10 | 2018-11-15 | 深圳市大疆创新科技有限公司 | Charging control method and system for unmanned aerial vehicle, and unmanned aerial vehicle |
| WO2019178993A1 (en) * | 2018-03-22 | 2019-09-26 | 深圳市华尼电子有限公司 | Mobile terminal charger |
| CN112151888A (en) * | 2020-09-25 | 2020-12-29 | 上海航天计算机技术研究所 | Carrier rocket lithium battery intelligent management equipment |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN203552177U (en) * | 2013-11-26 | 2014-04-16 | 路瑶 | Silencing energy-saving computer power supply |
| CN104810902A (en) * | 2014-12-30 | 2015-07-29 | 北京新能源汽车股份有限公司 | Mobile charging device and mobile charging method |
| CN105186628A (en) * | 2015-10-10 | 2015-12-23 | 陶杰 | Intelligent charging pile system for electric automobile |
| CN105680554A (en) * | 2015-12-28 | 2016-06-15 | 海鹰航空通用装备有限责任公司 | Power supply and distribution control device for unmanned aerial vehicle |
| CN105743153A (en) * | 2015-05-15 | 2016-07-06 | 杭州信控科技有限公司 | Flexibly-configurable and portable electric vehicle charging device |
-
2016
- 2016-11-29 CN CN201611069374.4A patent/CN106505703A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203552177U (en) * | 2013-11-26 | 2014-04-16 | 路瑶 | Silencing energy-saving computer power supply |
| CN104810902A (en) * | 2014-12-30 | 2015-07-29 | 北京新能源汽车股份有限公司 | Mobile charging device and mobile charging method |
| CN105743153A (en) * | 2015-05-15 | 2016-07-06 | 杭州信控科技有限公司 | Flexibly-configurable and portable electric vehicle charging device |
| CN105186628A (en) * | 2015-10-10 | 2015-12-23 | 陶杰 | Intelligent charging pile system for electric automobile |
| CN105680554A (en) * | 2015-12-28 | 2016-06-15 | 海鹰航空通用装备有限责任公司 | Power supply and distribution control device for unmanned aerial vehicle |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108495767A (en) * | 2017-04-13 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Charger and unmanned plane portable unit |
| WO2018188028A1 (en) * | 2017-04-13 | 2018-10-18 | 深圳市大疆创新科技有限公司 | Charger and unmanned aerial vehicle carrying apparatus |
| CN108495767B (en) * | 2017-04-13 | 2021-11-16 | 深圳市大疆创新科技有限公司 | Charger and unmanned aerial vehicle portable equipment |
| US11332265B2 (en) | 2017-04-13 | 2022-05-17 | SZ DJI Technology Co., Ltd. | Charger and portable device for unmanned aerial vehicle |
| WO2018205166A1 (en) * | 2017-05-10 | 2018-11-15 | 深圳市大疆创新科技有限公司 | Charging control method and system for unmanned aerial vehicle, and unmanned aerial vehicle |
| CN108023394A (en) * | 2017-12-27 | 2018-05-11 | 国网福建省电力有限公司 | Patrol unmanned locomotive team calamity is for vehicle-mounted emergency charge method |
| CN108023394B (en) * | 2017-12-27 | 2019-12-27 | 国网福建省电力有限公司 | Patrol unmanned aerial vehicle fleet disaster recovery standby vehicle-mounted emergency charging method |
| WO2019178993A1 (en) * | 2018-03-22 | 2019-09-26 | 深圳市华尼电子有限公司 | Mobile terminal charger |
| CN112151888A (en) * | 2020-09-25 | 2020-12-29 | 上海航天计算机技术研究所 | Carrier rocket lithium battery intelligent management equipment |
| CN112151888B (en) * | 2020-09-25 | 2022-02-15 | 上海航天计算机技术研究所 | Carrier rocket lithium battery intelligent management equipment |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170315 |
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| RJ01 | Rejection of invention patent application after publication |