CN107069865A - A kind of aircraft charging device used for buses and method - Google Patents
A kind of aircraft charging device used for buses and method Download PDFInfo
- Publication number
- CN107069865A CN107069865A CN201710237724.1A CN201710237724A CN107069865A CN 107069865 A CN107069865 A CN 107069865A CN 201710237724 A CN201710237724 A CN 201710237724A CN 107069865 A CN107069865 A CN 107069865A
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- Prior art keywords
- aircraft
- charging
- module
- charging device
- groove
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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
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/342—The other DC source being a battery actively interacting with the first one, i.e. battery to battery charging
-
- 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
- H02J7/0047—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
Abstract
The present invention relates to a kind of aircraft charging device used for buses; including the battery inside bus, installed in the aircraft airplane parking area and aircraft bottom electromagnet of bus roof; the airplane parking area includes shutting down plate; the shutdown plate is connected by fixing device with bus roof; the shutdown plate is provided with some first grooves and the second groove and power supply processing module; in the present invention; aircraft is fixed on bus roof by the collocation using electromagnet with shutting down the first groove on plate, and electromagnet will not rock aircraft generation after coming to a complete stop；Aircraft bottom is bonded to each other provided with contact charging device and charging panel in the second groove of bus roof, and receiving charging instruction can start to charge up, and such a charging modes are convenient and swift and battery need not be installed or dismantled.
Description
Technical field
The present invention relates to aircraft charging device, more particularly to a kind of aircraft charging device used for buses.
Background technology
At present, unmanned plane during flying device is using more and more extensive, with springing up for ecommerce tide, unmanned plane during flying implements
It is increasingly faster that stream develops, and it is more and more extensive that unmanned plane during flying device is just used, but is due to that unmanned plane belongs to small aircraft,
Continuation of the journey is a unalterable topic, and during unmanned plane delivery, battery electric quantity deficiency can be run into unavoidably causes aircraft can not
Continue delivery；If unmanned plane is on the way, a problem is also that can not find charge point, unmanned plane is caused persistently to fly
OK, the conventional charging arrangements of unmanned plane during flying device are all using charging socket or battery directly are removed into charging, this charging
Mode very inconvenient and current unmanned plane during flying device during unmanned plane transport express delivery is not to popularize very much, is matched somebody with somebody therewith
It is not many to close the device of charging.
The content of the invention
The present invention is that there is provided one kind one for the shortcomings of time not long charging is inconvenient for the continuation of the journey of unmanned plane in the prior art
Plant aircraft charging device used for buses and method.
In order to solve the above-mentioned technical problem, the present invention is addressed by following technical proposals：
A kind of aircraft charging device used for buses, including battery inside bus, installed in bus roof
The aircraft airplane parking area in portion and aircraft bottom electromagnet, the airplane parking area include shutting down plate, and the shutdown plate is filled by fixed
Put and be connected with bus roof, the shutdown plate is provided with some first grooves and the second groove and power supply processing module,
Pressure sensor is provided with each first groove, the pressure sensor connects power supply processing module, the power supply control
Processing module processed includes ARM microcontroller module, unmanned plane reference power supply Voltage stabilizing module, on/off module, contactor mould
Block and wireless data transfer module, the on/off module is provided with platform charging output end, bus battery connection nothing
Charging panel is provided with man-machine reference power supply Voltage stabilizing module, second groove, the charging panel connects the pressure sensor, institute
State charging panel to be connected with battery by wire, aircraft bottom is additionally provided with contact charging device, the contact charging device connects
Aircraft power management processing module is connect, the aircraft power management processing module includes aircraft ARM microcontroller module
With power interface control module, the power interface control module is connected by contact interface and platform charging output end, institute
State aircraft ARM microcontroller module and aircraft master controller is connected by signal, the power interface control module connection flies
Row device battery, the contact charging device connects aircraft battery, and the charging panel is used in conjunction with each other with contact charging device,
Electromagnet is used in conjunction with each other with the first groove.In the present invention, charge, not only meet winged to aircraft in bus roof
The charging of row device battery facilitates this demand, and aircraft can also carry bus and be moved in specified route simultaneously, not only save
Battery electric quantity it also avoid the flight that aircraft is repeated；Aircraft is consolidated in collocation using electromagnet with shutting down the first groove on plate
It is scheduled on bus roof, electromagnet will not rock aircraft generation after coming to a complete stop；Aircraft bottom is provided with contact charging device
Bonded to each other with charging panel in the second groove of bus roof, receiving charging instruction can start to charge up, Ci Zhongchong
Electrically convenient and swift and battery need not be installed or dismantled.
Preferably, the electromagnet uniform design is on the angle of aircraft bottom four, in bus roof identical bits
Four the first grooves are installed, when aircraft rests in bus roof, electromagnet is placed into the first groove.It is low in aircraft
Four angles in end set electromagnet, during fixation, aircraft is more stablized and avoid aircraft rocking all around,
In the present invention, electromagnet is equivalent to for bulge-structure, in order to be able to which more stable is placed in the first groove, the chi of the first groove
The very little size for being greater than electromagnet.
Preferably, the length of first groove is more than the length of electromagnet, the width of first groove is more than electricity
The width of magnet.
Preferably, both sides are provided with contact charging device in the middle of the aircraft bottom, in bus roof identical bits
Two the second grooves are installed, when aircraft rests in bus roof, contact charging device is placed into the second groove.
Preferably, the length of second groove is more than the length of contact charging device, the width of second groove
More than the width of contact charging device.
Preferably, power supply processing module also includes charging indicating module and alarm module.Charge indicating module with
Alarm module is all for sending charged state indicative function.
Preferably, charging indicating module includes four kinds of color LEDs, alarm module includes buzzer.
A kind of aircraft charging method used for buses, comprises the following steps：
The first step：Aircraft master control system is positioned and visual identity feedback or aircraft power administrative office by gps system
Reason module sends landing instruction to aircraft master control system, and aircraft bottom electromagnet is fallen into the first groove, in the first groove
Pressure sensor aircraft lands signal is sent in wireless data transfer module, wireless data transfer module sends out data
It is sent in aircraft master control system, aircraft master control system confirms aircraft lands, aircraft master control system starts charging
Instruction；
Second step：Power supply processing module receives charging instruction, and charging instruction is performed；Aircraft power administrative office
Reason module is received after charging instruction, and charging instruction is performed；
3rd step：Power supply processing module carries out path to on/off module, and aircraft reference power supply Voltage stabilizing module is received
The electric current that bus battery is sent is by the mobile platform transmission line of electricity that pulls in on charging panel；Power interface control module is received
The instruction that processing module is sent is managed to aircraft power, making charging to contact charging device indicates；
4th step：Charging panel charges to contact charging device, and contact charging device directly delivers current to aircraft electrical
In pond, when aircraft battery charging 25%：First LED light is bright；When aircraft battery charging 50%：2nd LED is indicated
Lamp is bright, when aircraft battery charging 75%：3rd LED light is bright；When aircraft battery charging 100%：4th LED is indicated
Lamp is bright and buzzer rings.
The present invention is as a result of above technical scheme, with significant technique effect：
In the present invention, charged in bus roof to aircraft, not only meet aircraft battery charging and facilitate this demand
Aircraft can also carry bus and be moved in specified route simultaneously, not only save battery electric quantity and it also avoid aircraft
The flight repeated；Aircraft is fixed on bus roof by the collocation using electromagnet with shutting down the first groove on plate, electromagnet
Aircraft will not be made to produce after coming to a complete stop to rock；Second groove of the aircraft bottom provided with contact charging device with bus roof
Interior charging panel is bonded to each other, and receiving charging instruction can start to charge up, such a charging modes are convenient and swift and battery not
Need to install or dismantle.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the accompanying drawing used required in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, without having to pay creative labor, may be used also
To obtain other accompanying drawings according to these accompanying drawings.
Fig. 1 is structure chart of the invention.
Fig. 2 is flow chart of the invention.
Label declaration：Airplane parking area 1, electromagnet 2, contact charging device 3, shutdown plate 11, the first groove 12, the second groove
13rd, charging panel 14.
Embodiment
With reference to embodiment, the present invention is described in further detail, following examples be explanation of the invention and
The invention is not limited in following examples.
Embodiment 1：
A kind of aircraft charging device used for buses, including battery inside bus, installed in bus roof
The aircraft airplane parking area 1 in portion and aircraft bottom electromagnet 2, the airplane parking area 1 include shutting down plate 11, and the shutdown plate 11 passes through
Fixing device is connected with bus roof, and the shutdown plate 11 is provided with some grooves 13 of first groove 12 and second and power supply control
Processing module processed, is provided with pressure sensor, the pressure sensor connection power supply processing mould in each first groove 12
Block, the power supply processing module includes ARM microcontroller module, unmanned plane reference power supply Voltage stabilizing module, on/off mould
Block, contactor module and wireless data transfer module, the on/off module is provided with platform charging output end, bus
Battery, which is connected, is provided with charging panel 14 in unmanned plane reference power supply Voltage stabilizing module, second groove 13, the charging panel 14 connects
The pressure sensor is connect, the charging panel 14 is connected by wire with battery, aircraft bottom is additionally provided with contact charging dress
3 are put, the connection of the contact charging device 3 aircraft power management processing module, the aircraft power manages processing module bag
The module of ARM microcontroller containing aircraft and power interface control module, the power interface control module pass through contact interface
It is connected with platform charging output end, the aircraft ARM microcontroller module connects aircraft master controller by signal, described
Power interface control module connects aircraft battery, and the contact charging device 3 connects aircraft battery, the charging panel 14 with
Contact charging device 3 is used in conjunction with each other, and electromagnet 2 is used in conjunction with each other with the first groove 12.
The uniform design of electromagnet 2 is provided with four on the angle of aircraft bottom four in bus roof same position
Individual first groove 12, the length of first groove 12 is more than the length of electromagnet 2, and the width of first groove 12 is more than electricity
The width of magnet 2, when aircraft rests in bus roof, electromagnet 2 is placed into the first groove 12.
Both sides are provided with contact charging device 3 in the middle of the aircraft bottom, and two are provided with bus roof same position
Individual second groove 13, the length of second groove 13 is more than the length of contact charging device 3, the width of second groove 13
More than the width of contact charging device 3, when aircraft rests in bus roof, contact charging device 3 is placed into the second groove
In 13.
A kind of aircraft charging method used for buses that device in embodiment 1 is realized, comprises the following steps：
The first step：Aircraft master control system is positioned and visual identity feedback or aircraft power administrative office by gps system
Reason module sends landing instruction to aircraft master control system, and aircraft bottom electromagnet 2 is fallen into the first groove 12, the first groove
Aircraft lands signal is sent in wireless data transfer module by the pressure sensor in 12, and wireless data transfer module is by number
According to being sent in aircraft master control system, aircraft master control system confirms aircraft lands, and aircraft master control system starts
Charging instruction；
Second step：Power supply processing module receives charging instruction, and charging instruction is performed；Aircraft power administrative office
Reason module is received after charging instruction, and charging instruction is performed；
3rd step：Power supply processing module carries out path to on/off module, and aircraft reference power supply Voltage stabilizing module is received
The electric current that bus battery is sent is by the mobile platform transmission line of electricity that pulls in on charging panel；Power interface control module is received
The instruction that processing module is sent is managed to aircraft power, making charging to contact charging device 3 indicates；
4th step：Charging panel 14 charges to contact charging device 3, and contact charging device directly delivers current to aircraft
In battery, when aircraft battery charging 25%：First LED light is bright；When aircraft battery charging 50%：2nd LED refers to
Show that lamp is bright, when aircraft battery charging 75%：3rd LED light is bright；When aircraft battery charging 100%：4th LED refers to
Show that lamp is bright and buzzer rings.
In embodiment 1, charging indicating module and alarm module are set in power supply processing module, and charging indicates mould
Block and alarm module are indicated for making display to charged state, and four kinds of color LEDs are provided with charging indicating module, according to
Battery is made color in charging and indicated, is provided with buzzer in alarm module, sound occurs when buzzer is provided in fully charged,
Prompting can also be made in each state that charges, this will write corresponding program in control chip and can just realize.
Furthermore, it is necessary to explanation, the specific embodiment described in this specification, is named the shape of its parts and components
Title etc. can be different.The equivalent or simple change that all construction, feature and principles according to described in inventional idea of the present invention are done, is wrapped
Include in the protection domain of patent of the present invention.Those skilled in the art can be to described specific implementation
Example is made various modifications or supplement or substituted using similar mode, structure without departing from the present invention or surmounts this
Scope as defined in the claims, all should belong to protection scope of the present invention.
Claims (8)
1. a kind of aircraft charging device used for buses, it is characterised in that：Including the battery inside bus, install
In the aircraft airplane parking area of bus roof（1）With aircraft bottom electromagnet（2）, the airplane parking area（1）Including shutting down plate
（11）, the shutdown plate（11）It is connected by fixing device with bus roof, the shutdown plate（11）It is recessed provided with some first
Groove（12）With the second groove（13）And power supply processing module, in each first groove（12）It is interior to be provided with pressure sensor,
The pressure sensor connects power supply processing module, and the power supply processing module includes ARM microcontroller module, nothing
Man-machine reference power supply Voltage stabilizing module, on/off module, contactor module and wireless data transfer module, the power supply lead to
Disconnected module is provided with platform charging output end, bus battery connection unmanned plane reference power supply Voltage stabilizing module, second groove
（13）It is interior to be provided with charging panel（14）, the charging panel（14）Connect the pressure sensor, the charging panel（14）Pass through wire
It is connected with battery, aircraft bottom is additionally provided with contact charging device（3）, the contact charging device（3）Connect aircraft electrical
Source control processing module, the aircraft power management processing module includes aircraft ARM microcontroller module and power interface
Control module, the power interface control module is connected by contact interface and platform charging output end, the aircraft ARM
Micro controller module connects aircraft master controller by signal, and the power interface control module connects aircraft battery, institute
State contact charging device（3）Connect aircraft battery, the charging panel（14）With contact charging device（3）It is used in conjunction with each other,
Electromagnet（2）With the first groove（12）It is used in conjunction with each other.
2. a kind of aircraft charging device used for buses according to claim 1, it is characterised in that：The electromagnet（2）
Uniform design is on the angle of aircraft bottom four, in bus roof same position provided with four the first grooves（12）, flight
When device rests in bus roof, electromagnet（2）It is placed into the first groove（12）It is interior.
3. a kind of aircraft charging device used for buses according to claim 2, it is characterised in that：First groove
（12）Length be more than electromagnet（2）Length, first groove（12）Width be more than electromagnet（2）Width.
4. a kind of aircraft charging device used for buses according to claim 1, it is characterised in that：The aircraft bottom
Middle both sides are provided with contact charging device（3）, in bus roof same position provided with two the second grooves（13）, aircraft
When resting in bus roof, contact charging device（3）It is placed into the second groove（13）It is interior.
5. a kind of aircraft charging device used for buses according to claim 4, it is characterised in that：Second groove
（13）Length be more than contact charging device（3）Length, second groove（13）Width be more than contact charging device（3）
Width.
6. a kind of aircraft charging device used for buses according to claim 1, it is characterised in that：Power supply handles mould
Block also includes charging indicating module and alarm module.
7. a kind of aircraft charging device used for buses according to claim 1, it is characterised in that：Charge indicating module bag
Containing four kinds of color LEDs, alarm module includes buzzer.
8. one kind that a kind of aircraft charging device used for buses based on any one described in claim 1-7 is realized
Aircraft charging method used for buses, it is characterised in that comprise the following steps：
The first step：Aircraft master control system is positioned and visual identity feedback or aircraft power administrative office by gps system
Reason module sends landing instruction, aircraft bottom electromagnet to aircraft master control system（2）Fall into the first groove（12）It is interior, first
Groove（12）Aircraft lands signal is sent in wireless data transfer module by interior pressure sensor, wireless data transmission mould
Block is transmitted data in aircraft master control system, and aircraft master control system confirms aircraft lands, aircraft master control system
System starts charging instruction；
Second step：Power supply processing module receives charging instruction, and charging instruction is performed；Aircraft power administrative office
Reason module is received after charging instruction, and charging instruction is performed；
3rd step：Power supply processing module carries out path to on/off module, and aircraft reference power supply Voltage stabilizing module is received
The electric current that bus battery is sent is by the mobile platform transmission line of electricity that pulls in on charging panel；Power interface control module is received
The instruction that processing module is sent is managed to aircraft power, to contact charging device（3）Charging is made to indicate；
4th step：Charging panel（14）To contact charging device（3）Charged, contact charging device directly delivers current to winged
In row device battery, when aircraft battery charging 25%：First LED light is bright；When aircraft battery charging 50%：Second
LED light is bright, when aircraft battery charging 75%：3rd LED light is bright；When aircraft battery charging 100%：4th
LED light is bright and buzzer rings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710237724.1A CN107069865A (en) | 2017-04-12 | 2017-04-12 | A kind of aircraft charging device used for buses and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710237724.1A CN107069865A (en) | 2017-04-12 | 2017-04-12 | A kind of aircraft charging device used for buses and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107069865A true CN107069865A (en) | 2017-08-18 |
Family
ID=59602712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710237724.1A Withdrawn CN107069865A (en) | 2017-04-12 | 2017-04-12 | A kind of aircraft charging device used for buses and method |
Country Status (1)
| Country | Link |
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| CN (1) | CN107069865A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108698709A (en) * | 2017-09-30 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Shut down platform, unmanned vehicle base station, the landing method of unmanned vehicle and system |
| CN108974365A (en) * | 2018-07-31 | 2018-12-11 | 佛山市高明曦逻科技有限公司 | Brainpower insufflation pesticide system |
| CN109502023A (en) * | 2018-09-26 | 2019-03-22 | 北京理工大学 | A kind of unmanned vehicle and unmanned plane cooperative operation system |
| CN109944473A (en) * | 2019-04-10 | 2019-06-28 | 蔡乌力吉 | A kind of stereo urban traffic hinge |
| CN109972865A (en) * | 2019-04-10 | 2019-07-05 | 蔡乌力吉 | A kind of urban bus station |
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| JPH09302628A (en) * | 1996-05-16 | 1997-11-25 | Mutsuo Hamaguchi | Movable landing facility for small-sized aircraft |
| CN104875902A (en) * | 2015-05-25 | 2015-09-02 | 陶亚平 | Overhead remote control aircraft parking apron and parking device thereof |
| CN105553116A (en) * | 2016-01-19 | 2016-05-04 | 刘勇 | Landing capture device for unmanned aerial vehicle |
| CN105958656A (en) * | 2016-06-27 | 2016-09-21 | 中惠创智无线供电技术有限公司 | Wireless charging equipment and method for multi-rotor aircraft |
| CN106394382A (en) * | 2015-07-29 | 2017-02-15 | 周坤友 | Intelligent supply base for vehicle-mounted unmanned aircraft |
-
2017
- 2017-04-12 CN CN201710237724.1A patent/CN107069865A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09302628A (en) * | 1996-05-16 | 1997-11-25 | Mutsuo Hamaguchi | Movable landing facility for small-sized aircraft |
| CN104875902A (en) * | 2015-05-25 | 2015-09-02 | 陶亚平 | Overhead remote control aircraft parking apron and parking device thereof |
| CN106394382A (en) * | 2015-07-29 | 2017-02-15 | 周坤友 | Intelligent supply base for vehicle-mounted unmanned aircraft |
| CN105553116A (en) * | 2016-01-19 | 2016-05-04 | 刘勇 | Landing capture device for unmanned aerial vehicle |
| CN105958656A (en) * | 2016-06-27 | 2016-09-21 | 中惠创智无线供电技术有限公司 | Wireless charging equipment and method for multi-rotor aircraft |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108698709A (en) * | 2017-09-30 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Shut down platform, unmanned vehicle base station, the landing method of unmanned vehicle and system |
| CN108698709B (en) * | 2017-09-30 | 2022-03-22 | 深圳市大疆创新科技有限公司 | Shutdown platform, unmanned aerial vehicle base station, and landing method and system of unmanned aerial vehicle |
| CN108974365A (en) * | 2018-07-31 | 2018-12-11 | 佛山市高明曦逻科技有限公司 | Brainpower insufflation pesticide system |
| CN109502023A (en) * | 2018-09-26 | 2019-03-22 | 北京理工大学 | A kind of unmanned vehicle and unmanned plane cooperative operation system |
| CN109944473A (en) * | 2019-04-10 | 2019-06-28 | 蔡乌力吉 | A kind of stereo urban traffic hinge |
| CN109972865A (en) * | 2019-04-10 | 2019-07-05 | 蔡乌力吉 | A kind of urban bus station |
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Application publication date: 20170818 |
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