CN209448498U - UAV system and unmanned plane - Google Patents
UAV system and unmanned plane Download PDFInfo
- Publication number
- CN209448498U CN209448498U CN201822010200.1U CN201822010200U CN209448498U CN 209448498 U CN209448498 U CN 209448498U CN 201822010200 U CN201822010200 U CN 201822010200U CN 209448498 U CN209448498 U CN 209448498U
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- power source
- unmanned
- uav system
- backup power
- main power
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B70/00—Technologies for an efficient end-user side electric power management and consumption
- Y02B70/30—Systems integrating technologies related to power network operation and communication or information technologies for improving the carbon footprint of the management of residential or tertiary loads, i.e. smart grids as climate change mitigation technology in the buildings sector, including also the last stages of power distribution and the control, monitoring or operating management systems at local level
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
- Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
- Y04S20/00—Management or operation of end-user stationary applications or the last stages of power distribution; Controlling, monitoring or operating thereof
- Y04S20/20—End-user application control systems
Abstract
The utility model discloses a kind of UAV system and unmanned planes.Wherein, UAV system includes: unmanned thermomechanical components, and the unmanned thermomechanical components include at least one sub-component；Main power source, the main power source are connected with the unmanned thermomechanical components, for the unmanned plane assembly power supply；Backup power source, the backup power source are connected with the unmanned thermomechanical components, powered at least one sub-component in main power source power-off.The UAV system of the utility model can be when main power source turns off, being switched to backup power source is the part unmanned plane sub-component power supply in UAV system, is at working condition, in this way, it maintains the major function of unmanned plane to can be at continuing working the purpose of state, promotes the working efficiency of unmanned plane.
Description
Technical field
The utility model relates to vehicle technology field more particularly to a kind of UAV system and unmanned planes.
Background technique
In the related technology, the structure of UAV system is as shown in Figure 1, comprising: flight controller, power supply, electron speed regulator,
The functional module and communication module of propeller motor and periphery, work are original are as follows: power supply is various pieces (that is: flight control
Device processed, electron speed regulator, propeller motor and periphery functional module and communication module) power supply, flight controller control electricity
Sub- governor, to can control propeller motor.Flight controller control function module is to reach the function to be realized of unmanned plane.
Communication module is responsible for being communicated with other equipment (such as computer), achievees the purpose that transmit data.
Power supply is responsible for giving various pieces power supply, and when power supply disconnects, the various pieces of unmanned plane are closed completely because of power supply
Break and be in off position, such as: the data link of communication module is fully disconnected, and when unmanned plane re-powers, restores data
Link needs the regular hour, therefore, influences the working efficiency of unmanned plane.
Summary of the invention
The utility model aims to solve at least one of the technical problems existing in the prior art.
For this purpose, a purpose of the utility model is to propose a kind of UAV system.The UAV system can be effective
Promote the working efficiency of unmanned plane.
Another purpose of the utility model is to propose a kind of unmanned plane.
To achieve the goals above, the first aspect of the utility model discloses a kind of UAV system, comprising: unmanned plane
Component, the unmanned thermomechanical components include at least one sub-component；Main power source, the main power source are connected with the unmanned thermomechanical components,
Think the unmanned plane assembly power supply；Backup power source, the backup power source are connected with the unmanned thermomechanical components, in the main electricity
When source powers off, power at least one sub-component.
The UAV system of the utility model, can be when main power source turns off, and being switched to backup power source is UAV system
In part unmanned plane sub-component power supply, be at working condition, in this way, maintain unmanned plane major function can be at continue
The purpose of working condition promotes the working efficiency of unmanned plane.
Further, the backup power source is connected and the anode of the diode by diode with the unmanned thermomechanical components
It is connected with the backup power source, wherein the output voltage of the main power source is greater than the output voltage of the backup power source.
Further, the backup power source is connected with the main power source, to be charged by the main power source.
Further, the backup power source includes: battery core；Buck component, wherein the unmanned thermomechanical components pass through described
Buck component is connected with the battery core；Charge management component, the charge management component respectively with the battery core and the liter
Down block is connected, and is charged and discharged with controlling the battery core, and control the opening and closing of the buck component.
Further, the backup power source is removably connected with the unmanned thermomechanical components and the main power source.
Further, unmanned plane is arranged in independently of the unmanned thermomechanical components and the main power source in the backup power source
On.
Further, the unmanned thermomechanical components include flight controller, the flight controller respectively with the main power source
It is connected with the backup power source, to be powered by main power source or backup power source.
Further, the flight controller is connect with electron speed regulator, the electron speed regulator and propeller electricity
Machine is connected to control the propeller.
Further, the flight controller is connect with communication module.
The second aspect of the utility model discloses a kind of unmanned plane, comprising: according to nothing described in above-mentioned first aspect
Man-machine system.The unmanned plane can be when main power source turns off, and being switched to backup power source is the part unmanned plane in UAV system
Sub-component power supply, is at working condition, in this way, the major function of maintenance unmanned plane can be at continuing working the mesh of state
, work efficiency is high.
The additional aspect and advantage of the utility model will be set forth in part in the description, partially will be from following description
In become obvious, or recognized by the practice of the utility model.
Detailed description of the invention
The above-mentioned and/or additional aspect and advantage combination following accompanying drawings of the utility model are incited somebody to action in the description of embodiment
Become obvious and be readily appreciated that, in which:
Fig. 1 is the schematic diagram of UAV system in the related technology.
Fig. 2 is the structural block diagram according to the UAV system of the utility model one embodiment.
Fig. 3 is the schematic diagram according to the UAV system of the utility model one embodiment；
Fig. 4 is the charge and discharge electrical schematic of backup power source in the UAV system according to the utility model one embodiment；
Fig. 5 is main power source and backup power source and unmanned unit in the UAV system according to the utility model one embodiment
The schematic diagram of part connection.
Description of symbols:
UAV system 200, unmanned thermomechanical components 210, main power source 220, backup power source 230, charge management component 231 and electricity
Core 232.
Specific embodiment
The embodiments of the present invention are described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the utility model, and should not be understood as to the utility model
Limitation.
UAV system and unmanned plane according to the utility model embodiment is described with reference to the accompanying drawing.
Fig. 2 is the structural block diagram according to the UAV system of the utility model one embodiment.As shown in Fig. 2, according to this
The UAV system 200 of utility model one embodiment, comprising: unmanned thermomechanical components 210, main power source 220 and backup power source 230.
Wherein, unmanned thermomechanical components 210 include at least one sub-component.Main power source 220 is connected with unmanned thermomechanical components 210, with
For the power supply of unmanned thermomechanical components 210.Backup power source 230 is connected with unmanned thermomechanical components 210, to be at least when main power source 220 powers off
One sub- assembly power supply.
The UAV system of the utility model embodiment can be switched to backup power source when main power source turns off as nobody
Part unmanned plane sub-component power supply in machine system, is at working condition, in this way, maintaining the major function of unmanned plane can locate
In the purpose for the state that continues working.
As shown in figure 3, backup power source 230 is also connected with main power source 220, in this way, main power source 220 can be backup power source
230 charge.
As shown in figure 4, backup power source 230 includes: that charge management component 231, battery core 232 and buck component (do not have in Fig. 4
It shows).Wherein, unmanned thermomechanical components 210 are connected by buck component with battery core 231.Charge management component 231 respectively with electricity
Core 231 is connected with buck component, is charged and discharged with controlling battery core 231, and controls unlatching and the pass of buck component
It closes.
In the above description, buck component is the circuit for voltage being boosted or being depressured processing.Such as: charging valve
It manages component 231 and controls battery core when being the subassemblies power supply in unmanned thermomechanical components 210, it is assumed that discharge voltage is excessively high, then can be with
It is the subassemblies power supply in unmanned thermomechanical components 210 after being depressured by buck component.
As shown in figure 3, the unmanned thermomechanical components 210 include flight controller, the flight controller respectively with the master
Power supply 220 is connected with the backup power source 230, to be powered by main power source 220 or backup power source 230.
Further, the flight controller can be connect with electron speed regulator, the electron speed regulator and the spiral
Paddle motor is connected to control the propeller.
Further, the flight controller can be connect with communication module, to realize that flight controller and outside are mobile
Equipment or the communication for controlling equipment.
The working principle of the UAV system of the utility model embodiment is as follows:
When unmanned plane is in state of flight or main power source 220 in the closure state, the main power supply source of unmanned plane
Main power source 220, backup power source 230 may be at charged state at this time, not supplying power for outside, the electricity of backup power source 230 by
Charge management component 231 controls, and when fully charged, charge management component 231 controls main power source 220 and disconnects and backup power source 230
Connection, so that backup power source 230 be avoided to overcharge, when backup power source 230 is in it is under-voltage when, charge management component 231 can also be controlled
Connection in the disconnection of backup power source 230 processed and unmanned thermomechanical components 210 between subassemblies, at this point, will not be these subgroups
Part power supply, avoids 230 overdischarge of backup power source, promotes the service life of backup power source 230.
When main power source 220 is in an off state, the part of module of UAV system can be made by certain circuit mechanism
The power supply of (that is: subassemblies) switches seamlessly to backup power source 230 by main power source 220, disconnects in this way in main power source 220
In the case of, the part of module of unmanned plane can not work with powering off, and (communication link such as be avoided to build again to reach certain functional requirements
It is vertical) continue.
Specifically, as shown in figure 5, backup power source 230 is connected by diode D1 with unmanned thermomechanical components 210 and diode
The anode of D1 is connected with backup power source 230, and the cathode of diode D1 is connected with the supply port of unmanned thermomechanical components 210, main power source
220 are directly connected with the supply port of unmanned thermomechanical components 210.In this example, the output voltage of main power source 220 is greater than standby electricity
The output voltage in source 230.
Such as: the output voltage of backup power source 230 is 5V, and the output voltage of main power source 220 is 5.5V, at this point, working as main electricity
When source 220 is accessed, then unmanned thermomechanical components 210 are powered using main power source 220, when main power source 220 powers off or removes, then spare
The diode D1 of power supply 230 is connected, so that backup power source 230 is that unmanned thermomechanical components 210 continue to power, hereby it is achieved that seamless
Ground is switched to backup power source 230, and in the case where main power source 220 disconnects, the part of module of unmanned plane can not work with powering off.
The UAV system of the utility model embodiment can be switched to backup power source when main power source turns off as nobody
Part unmanned plane sub-component power supply in machine system, is at working condition, in this way, reaching unmanned plane can be to transmission data
It is uninterrupted, or the major function of unmanned plane is maintained to be in the state that continues working, reduced after main power source is opened such as data-link
The recovery time that road is established.
In addition, backup power source 230 is removably connected with unmanned thermomechanical components 210 and main power source 220.Further, spare
Power supply 230 is arranged on unmanned plane independently of unmanned thermomechanical components 210 and 220 ground of the main power source.That is: backup power source 230 is being tied
Independently of other modules (that is: unmanned thermomechanical components 210 and main power source 220) so that it is convenient to dismantle, replace on structure.
Specifically, since the cruising ability of the main power source of unmanned plane 220 is limited, lead to landing often, in this way, spare
Power supply 230 is usually in the case where not being full of in charging, the recurrent state discharged, due to the cycle charge-discharge of battery core
Number is limited, therefore, backup power source 230 is external, when backup power source 230 needs replacing, facilitates operation.
Further, the embodiments of the present invention disclose a kind of unmanned plane, comprising: according to any one above-mentioned implementation
UAV system described in example.
The unmanned plane can be when main power source turns off, and being switched to backup power source is the unmanned loom in part in UAV system
Assembly power supply is at working condition, in this way, reaching unmanned plane can be to the uninterrupted of transmission data, or maintains nobody
The major function of machine is in the state continued working, reduces the recovery time after main power source is opened such as data link setup.
In addition, according to other compositions of the unmanned plane of the utility model embodiment and effect for this field common skill
All be for art personnel it is known, be not repeated herein.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means specific features, structure, material or spy described in conjunction with this embodiment or example
Point is contained at least one embodiment or example of the utility model.In the present specification, to the schematic table of above-mentioned term
Stating may not refer to the same embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be
It can be combined in any suitable manner in any one or more embodiment or examples.
While there has been shown and described that the embodiments of the present invention, it will be understood by those skilled in the art that:
These embodiments can be carried out with a variety of variations, modification, replacement in the case where not departing from the principles of the present invention and objective
And modification, the scope of the utility model are defined by the claims and their equivalents.
Claims (10)
1. a kind of UAV system characterized by comprising
Unmanned thermomechanical components, the unmanned thermomechanical components include at least one sub-component；
Main power source, the main power source are connected with the unmanned thermomechanical components, for the unmanned plane assembly power supply；
Backup power source, the backup power source are connected with the unmanned thermomechanical components, to be at least one in main power source power-off
Sub-component power supply.
2. UAV system according to claim 1, which is characterized in that the backup power source passes through diode and the nothing
Man-machine component is connected and the anode of the diode is connected with the backup power source, wherein the output voltage of the main power source is big
In the output voltage of the backup power source.
3. UAV system according to claim 1, which is characterized in that the backup power source is connected with the main power source,
To be charged by the main power source.
4. UAV system according to claim 1-3, which is characterized in that the backup power source includes:
Battery core；
Buck component, wherein the unmanned thermomechanical components are connected by the buck component with the battery core；
Charge management component, the charge management component is connected with the battery core and the buck component respectively, to control
It states battery core to charge and discharge, and controls the opening and closing of the buck component.
5. UAV system according to claim 3, which is characterized in that the backup power source removably with it is described nobody
Thermomechanical components are connected with the main power source.
6. UAV system according to claim 5, which is characterized in that the backup power source is independently of the unmanned unit
It is arranged on unmanned plane to part and the main power source.
7. UAV system according to claim 1, which is characterized in that the unmanned thermomechanical components include flight controller,
The flight controller is connected with the main power source and the backup power source respectively, to be supplied by main power source or backup power source
Electricity.
8. UAV system according to claim 7, which is characterized in that the flight controller and electron speed regulator connect
It connects, the electron speed regulator is connect with propeller motor to control propeller.
9. UAV system according to claim 7, which is characterized in that the flight controller is connect with communication module.
10. a kind of unmanned plane characterized by comprising -9 described in any item UAV system according to claim 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822010200.1U CN209448498U (en) | 2018-11-30 | 2018-11-30 | UAV system and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822010200.1U CN209448498U (en) | 2018-11-30 | 2018-11-30 | UAV system and unmanned plane |
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| Publication Number | Publication Date |
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| CN209448498U true CN209448498U (en) | 2019-09-27 |
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| CN201822010200.1U Active CN209448498U (en) | 2018-11-30 | 2018-11-30 | UAV system and unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116280230A (en) * | 2023-03-17 | 2023-06-23 | 昆山亿飞航空智能科技有限公司 | Continuous energy protection device for power output interruption of unmanned aerial vehicle |
-
2018
- 2018-11-30 CN CN201822010200.1U patent/CN209448498U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116280230A (en) * | 2023-03-17 | 2023-06-23 | 昆山亿飞航空智能科技有限公司 | Continuous energy protection device for power output interruption of unmanned aerial vehicle |
| CN116280230B (en) * | 2023-03-17 | 2024-02-23 | 昆山亿飞航空智能科技有限公司 | Continuous energy protection device for power output interruption of unmanned aerial vehicle |
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Address after: 510000 Block C, 115 Gaopu Road, Tianhe District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Jifei Technology Co.,Ltd. Address before: 510000, No. 1, Cheng Cheng Road, Gaotang Software Park, Guangzhou, Guangdong, Tianhe District, 3A01 Patentee before: Guangzhou Xaircraft Technology Co.,Ltd. |