CN207557727U - Unmanned plane with intelligent battery - Google Patents
Unmanned plane with intelligent battery Download PDFInfo
- Publication number
- CN207557727U CN207557727U CN201721762203.XU CN201721762203U CN207557727U CN 207557727 U CN207557727 U CN 207557727U CN 201721762203 U CN201721762203 U CN 201721762203U CN 207557727 U CN207557727 U CN 207557727U
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- China
- Prior art keywords
- module
- unmanned plane
- intelligent battery
- battery
- fuselage
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model is related to a kind of unmanned planes with intelligent battery, and including main control module, the main control module is suitable for being communicated by CAN bus and intelligent battery module；The intelligent battery module includes：The lithium battery of several parallel connections and the battery detecting module for connecting intelligent battery module output terminal；The battery detecting module is adapted to detect for the output voltage and/or electric current of intelligent battery module, and is shown by being located at the display module on intelligent battery module, and user can intuitively check the state of battery in unmanned plane very much.
Description
Technical field
The utility model is related to unmanned plane fields, and in particular to a kind of unmanned plane with intelligent battery.
Background technology
UAV is referred to as " unmanned plane "（“UAV”）, controlled using radio robot and the program provided for oneself
The not manned vehicle that device manipulates.Unmanned plane is actually the general designation of unmanned vehicle, can be with from technical standpoint definition
It is divided into：Unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, nothing
People's parasol etc..
Since unmanned plane is generally using battery powered, the effective utilization of battery directly influences the flight endurance of unmanned plane.
Therefore, it based on above-mentioned purpose, needs to design a kind of unmanned plane with intelligent battery.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane with intelligent battery, convenient for intuitively to obtain in unmanned plane
The volt-ampere parameter of lithium battery module.
In order to solve the above-mentioned technical problem, the utility model provides a kind of unmanned plane with intelligent battery, including：
Main control module, the main control module are suitable for being communicated by CAN bus and intelligent battery module；
The intelligent battery module includes：The lithium battery of several parallel connections and the electricity for connecting intelligent battery module output terminal
Pond detection module；
The battery detecting module is adapted to detect for the output voltage and/or electric current of intelligent battery module, and by being located at intelligence
Display module in energy battery modules is shown.
Further, the battery detecting module includes：MCU module, the management of charging and discharging chip being connected with the MCU module,
The MCU module is suitable for the charge and discharge cycles number by management of charging and discharging chip minute book intelligent battery module, and passes through aobvious
Show that module is shown.
Further, the output terminal of the intelligent battery module is suitable for using double wire connection terminals.
Further, the unmanned plane further includes：
Several horn bars, and one end of each horn bar is connect with fuselage；Wherein
The horn bar is hollow structure, and air-charging lining is equipped in the hollow structure,
The gas that density is less than air is filled in the air-charging lining.
Further, the unmanned plane is multi-rotor unmanned aerial vehicle；
The fuselage is cylindrical structure, and the junction of each horn bar and fuselage is equipped with rotating mechanism；
The rotating mechanism is driven by a stepper motor；
The Hall sensor for being adapted to detect for rotor motor rotation is equipped in each rotor；
After Hall sensor detects that a rotor motor breaks down, the main control module is suitable for through the top in fuselage
The fuselage angle of inclination that spiral shell instrument obtains is to control corresponding stepper motor to adjust the distribution of horn bar, the shape so that fuselage restores balance
State.
Further, the unmanned plane further includes：The GPS module that is electrically connected with the main control module, communication module and
Photographing module.
The beneficial effects of the utility model are, the unmanned plane of the utility model is with intelligent battery, i.e., including main control module,
The main control module is suitable for being communicated by CAN bus and intelligent battery module；The intelligent battery module includes：If dry doubling
The lithium battery of connection and the battery detecting module for connecting intelligent battery module output terminal；The battery detecting module is adapted to detect for
The output voltage and/or electric current of intelligent battery module, and shown by being located at the display module on intelligent battery module, make
User can intuitively check the state of the work of battery in unmanned plane very much.
Description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is the functional block diagram of the unmanned plane of the utility model；
Fig. 2 is the structure diagram of the unmanned plane of the utility model；
Fig. 3 be the utility model unmanned plane in after a rotor motor breaks down, horn bar where remaining rotor motor
Mobile schematic diagram.
In figure：
Horn bar 100, air-charging lining 101, rotor motor 102, fuselage 200, stepper motor 201, rotating mechanism 210, fan
Shape connector 211, shaft 212.
Specific embodiment
The utility model is described in further detail presently in connection with attached drawing.These attached drawings are simplified schematic diagram,
Only illustrate the basic structure of the utility model in a schematic way, therefore it only shows the composition related with the utility model.
As shown in Figure 1, a kind of unmanned plane with intelligent battery is present embodiments provided, including：Main control module, the master
Control module is suitable for being communicated by CAN bus and intelligent battery module；The intelligent battery module includes：The lithium of several parallel connections
Battery and the battery detecting module for connecting intelligent battery module output terminal；The battery detecting module is adapted to detect for intelligent electricity
The output voltage and/or electric current of pond module, and shown by being located at the display module on intelligent battery module.
The main control module is communicated with intelligent battery module, suitable for according to the volt-ampere number for obtaining intelligent battery module
According to performing corresponding flight directive；And CAN bus communication modes are used convenient for being expanded as unit of intelligent battery module,
Increase the quantity of intelligent battery module.
As a kind of optional embodiment of battery detecting module, the battery detecting module includes：MCU module, with
The management of charging and discharging chip that the MCU module is connected, the MCU module are suitable for through management of charging and discharging chip minute book intelligent battery
The charge and discharge cycles number of module, and pass through display module and shown.
Wherein, 51 series monolithics may be used in the MCU module, and the management of charging and discharging chip can be, but not limited to adopt
With MAX8731, CN3717 or UC3096 etc..
CAN communication module is equipped between the MCU module and main control module, the CAN communication module is for example
SN65HVD230DR。
Also, the temperature sensor for detecting lithium battery temperature, the temperature are additionally provided in the intelligent battery module
Temperature data is sent to MCU module and is shown by display module by sensor.
The output terminal of the intelligent battery module is suitable for using double wire connection terminals, using Redundancy Design, in a wire connection terminal
During connecting fault, wire connection terminal can be replaced.
The unmanned plane further includes：Several horn bars 100, one end of each horn bar 100 are connect with fuselage 200；
Wherein described horn bar 100 is hollow structure, air-charging lining 101 is equipped in the hollow structure, in the air-charging lining 101
It is filled with the gas that density is less than air.
The utility model is less than sky by being put into air-charging lining 101 in the hollow structure of horn bar 100, with packing density
The gas of gas can be the lighter-than-air inert gas of the quality such as helium, and energy is reduced to reduce the dead weight of unmanned plane, and then realize
Consumption.
Fig. 2 is referred to, the unmanned plane is multi-rotor unmanned aerial vehicle, can be three rotors, quadrotor or six rotors；It is described
Fuselage 200 be cylindrical structure, in order to prevent unmanned plane in flight course rotor motor 102 break down stalling after, nobody
The easy disequilibrium of machine crashes, and therefore, the junction of each horn bar 100 and fuselage 200 is equipped with rotating machine in the present embodiment
Structure 210；The rotating mechanism 210 is driven by a stepper motor 201；It is equipped in each rotor and is adapted to detect for rotor motor 102 and rotates
Hall sensor.
The present embodiment has rotor motor A, rotor motor B, rotor motor C and rotor electricity by taking quadrotor unmanned plane as an example
Machine D, and above-mentioned rotor motor is connected to the shaft 212 of stepper motor 201 by horn bar 100, fan-shaped connector 211
On, it is driven by stepper motor 201 and rotated in a certain range, rotational angle can be by taking rotor motor B as an example, if level angle is
0, rotational angle can be, but not limited to ± 30 °, and stepper motor 201 drives rotation in a certain range as shown in F.
After Hall sensor detects that a rotor motor breaks down, the main control module in the unmanned plane is suitable for passing through
200 angle of inclination of fuselage that gyroscope in fuselage 200 obtains is to control corresponding stepper motor 201 to adjust point of horn bar 100
Cloth, the state so that fuselage 200 restores balance.
As shown in figure 3, if a rotor motor C breaks down in unmanned plane, corresponding to rotor motor B and rotor motor D
Horn bar 100 moved respectively along F1 and F2 directions so that each horn bar 100 is in 120 ° of angles, and then fuselage 200 is made to restore flat
Weighing apparatus state, and then prevent unmanned plane from remaining rotor motor being caused to cannot keep balance since a rotor motor breaks down, at present
Although there is related algorithm it can be made to restore balance by changing the rotating speed of each rotor motor, a large amount of electric energy can be consumed,
Also, the rotational speed regulation range of rotor motor is made to narrow, resists the less able of air-flow.
The unmanned plane further includes：GPS module, communication module and the camera shooting mould being electrically connected with the main control module
Block.
The main control module can be, but not limited to using ARM embeded processors, such as s3C2416 processors.
Therefore, this communication module can stablize wireless telecommunications of the transmitting-receiving unmanned plane in flight course, the communication module
WiFi communication module may be used.
Using the above-mentioned desirable embodiment according to the utility model as enlightenment, pass through above-mentioned description, related work people
Member can carry out various changes and amendments in the range of without departing from this item utility model technological thought completely.This item is real
The content being not limited to novel technical scope on specification, it is necessary to which its technology is determined according to right
Property range.
Claims (6)
1. a kind of unmanned plane with intelligent battery, which is characterized in that including：
Main control module, the main control module are suitable for being communicated by CAN bus and intelligent battery module；
The intelligent battery module includes：The lithium battery of several parallel connections and the battery inspection for connecting intelligent battery module output terminal
Survey module；
The battery detecting module is adapted to detect for the output voltage and/or electric current of intelligent battery module, and by being located at intelligent electricity
Display module on the module of pond is shown.
2. the unmanned plane according to claim 1 with intelligent battery, which is characterized in that
The battery detecting module includes：MCU module, the management of charging and discharging chip MCU module being connected with the MCU module are described
MCU module is suitable for the charge and discharge cycles number by management of charging and discharging chip minute book intelligent battery module, and passes through display mould
Block is shown.
3. the unmanned plane according to claim 2 with intelligent battery, which is characterized in that
The output terminal of the intelligent battery module is suitable for using double wire connection terminals.
4. the unmanned plane according to claim 3 with intelligent battery, which is characterized in that
The unmanned plane further includes：
Several horn bars, and one end of each horn bar is connect with fuselage；Wherein
The horn bar is hollow structure, and air-charging lining is equipped in the hollow structure,
The gas that density is less than air is filled in the air-charging lining.
5. unmanned plane according to claim 4, which is characterized in that
The unmanned plane is multi-rotor unmanned aerial vehicle；
The fuselage is cylindrical structure, and the junction of each horn bar and fuselage is equipped with rotating mechanism；
The rotating mechanism is driven by a stepper motor；
The Hall sensor for being adapted to detect for rotor motor rotation is equipped in each rotor；
After Hall sensor detects that a rotor motor breaks down, the main control module is suitable for through the gyroscope in fuselage
The fuselage angle of inclination of acquisition is to control corresponding stepper motor to adjust the distribution of horn bar, the state so that fuselage restores balance.
6. unmanned plane according to claim 5, which is characterized in that
The unmanned plane further includes：GPS module, communication module and the photographing module being electrically connected with the main control module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721762203.XU CN207557727U (en) | 2017-12-15 | 2017-12-15 | Unmanned plane with intelligent battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721762203.XU CN207557727U (en) | 2017-12-15 | 2017-12-15 | Unmanned plane with intelligent battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207557727U true CN207557727U (en) | 2018-06-29 |
Family
ID=62663398
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721762203.XU Expired - Fee Related CN207557727U (en) | 2017-12-15 | 2017-12-15 | Unmanned plane with intelligent battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207557727U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110138046A (en) * | 2019-06-05 | 2019-08-16 | 深圳市道通智能航空技术有限公司 | Battery management system, battery management method, power module and unmanned plane |
-
2017
- 2017-12-15 CN CN201721762203.XU patent/CN207557727U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110138046A (en) * | 2019-06-05 | 2019-08-16 | 深圳市道通智能航空技术有限公司 | Battery management system, battery management method, power module and unmanned plane |
| CN110138046B (en) * | 2019-06-05 | 2022-01-14 | 深圳市道通智能航空技术股份有限公司 | Battery management system, battery management method, power module and unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180629 Termination date: 20211215 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |