CN207257997U - The unmanned plane of plurality of voltage platforms - Google Patents
The unmanned plane of plurality of voltage platforms Download PDFInfo
- Publication number
- CN207257997U CN207257997U CN201720985639.9U CN201720985639U CN207257997U CN 207257997 U CN207257997 U CN 207257997U CN 201720985639 U CN201720985639 U CN 201720985639U CN 207257997 U CN207257997 U CN 207257997U
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- Prior art keywords
- battery pack
- unmanned plane
- voltage
- terminal
- pair
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model provides a kind of unmanned plane of plurality of voltage platforms, including the battery pack fixed to bottom part body, battery pack has a shell and accommodates inside the shell at least one connects the battery pack formed and the control circuit being connected with battery pack by multiple rechargeable batteries, housing exterior is additionally provided with one group of electric connection terminal being connected with control circuit, for being powered when battery pack is coupled to unmanned plane main body by electric connection terminal to unmanned plane；The electric connection terminal includes at least two pairs of terminals, provides first voltage to unmanned plane or second voltage exports.The unmanned plane of the utility model above-mentioned technical proposal, the battery pack that it is used is as power source, with more flexible voltage supply platform, when being connected to different unmanned planes or adapting to different battery packs, different voltage platforms may be selected to be exported and worked, so as to better conform to work and operating that battery pack is installed on unmanned plane, without individually finding unmanned plane or being adapted to new battery pack.
Description
Technical field
Unmanned plane field is the utility model is related to, in particular to a kind of unmanned plane of plurality of voltage platforms.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, or fully or intermittently independently operated by car-mounted computer.
At present, it is many that nobody company and technology are produced and sold, such as typical multi-rotor unmanned aerial vehicle, fixed-wing
Unmanned plane, the unmanned plane of electric drive, engine-driven unmanned plane, solar energy unmanned plane etc., take photo by plane, it is agricultural, plant protection, micro-
Type self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief,
The fields such as movies-making are widely applied.But application it is most be still electric drive unmanned plane, be subject to the shadow of battery
Ring, the most continuation of the journey of unmanned plane is all limited, such as the unmanned plane of great Jiang companies, and the lithium battery of its airborne platform supplies at present
Electric system, can maintain unmanned plane during flying 30-60min, also mean that its flight must make a return voyage for about 30 minutes, the electricity of early stage
Pond, encapsulation and battery combination constrain the development of unmanned plane with control system significantly.With the development of battery technology, at present
People have been developed for the battery of higher efficiency and higher energy density so that battery pack bigger, power supply it is stronger, but with it is so much
The matching for having been sold out unmanned plane in the market is still problem.
Meanwhile each family is all promoting the voltage platform of oneself, is bound to cause the waste of resource, such as the 18V of earlier-generation
Power supply platform, 36V platforms, 54V platforms to the later stage, all there is a problem in that, then how in obstructed voltage class
The problem of enabling it match different unmanned planes in battery pack, being to be solved.
Utility model content
The utility model aim is to provide a kind of unmanned plane of plurality of voltage platforms, including：
Main body；
The support arm for being connected and being disposed below with main body；
In the flight component that support arm tail end is set；
It is arranged on the landing chassis of bottom part body；
It is arranged on the positioning component of body top；
The battery pack of bottom part body is arranged on, for powering for unmanned plane；
Wherein, the support arm is 4, is centered around the uniform setting of main body surrounding, and 4 support arms correspond to four flight crews
Part, each flight component drive rotating rotor to form by a driving motor and by driving motor, and driving motor is connected to one
In a circuit control mainboard, circuit control mainboard is arranged in main body；
Main control processor and local storage and wireless network transceiver module are integrated with the circuit control mainboard；
The battery pack is fixed to the bottom of the main body, and battery pack has a shell and accommodates inside the shell extremely
Few one connects the battery pack formed and the control circuit being connected with battery pack, housing exterior are also set by multiple rechargeable batteries
One group of electric connection terminal being connected with control circuit is equipped with, for passing through electric connecting terminal when battery pack is coupled to unmanned plane main body
Son is powered to unmanned plane；
The electric connection terminal includes at least two pairs of terminals, wherein a pair of terminal is connected to the first Battery pack group both ends,
Second pair of terminal is connected to the second Battery pack group both ends, and the bottom of the main body of unmanned plane is provided with four terminals, wherein, unmanned plane
On terminal be configured to be connected with the electric connection terminal of battery pack so that in the first link position, described a pair of terminal pair
Series connection is formed between the battery pack answered battery pack corresponding with second pair of terminal in succession, and first voltage output is provided, second
Link position, formed between the corresponding battery pack of described a pair of terminal battery pack corresponding with second pair of terminal it is in parallel in succession,
And provide second voltage output.
In further embodiment, the rechargeable battery is identical, and the lithium battery that nominal voltage is 3.6V.
In further embodiment, in the first Battery pack group and the second Battery pack group, it is single that it is respectively provided with least five
The rechargeable battery series connection of body.
In further embodiment, the numerical value of the first voltage is twice of second voltage numerical value.
In further embodiment, the first voltage is 36V, second voltage 18V.
In further embodiment, described a pair of terminal and second pair of terminal are in line shape arrangement in physical space,
And second pair of terminal is located at the both sides of a pair of terminal.
In further embodiment, the landing chassis bottom is provided with Wireless charging coil, and is set by cable and one
Master control charging circuit connection in the main body, master control charging circuit are connected to main control processor.
Further, electric quantity monitoring circuit is additionally provided with the battery pack, is connected with the battery pack and control circuit, is used
In the residual charge state of monitoring battery pack.
Further, the positioning component includes at least one of GPS or Big Dipper positioning component.
Further, the control circuit has multiple field-effect transistors, is switched as charge and discharge control.
The unmanned plane of the utility model above-mentioned technical proposal, its battery pack used have cleverer as power source
Voltage supply platform living, can be by newly-designed when being connected to different unmanned planes or adapting to different battery packs
Electrode slice connection mode selects different voltage platforms to be exported and worked to realize, is installed to so as to better conform to battery pack
Work and operating on unmanned plane, without individually finding unmanned plane or being adapted to new battery pack.
It should be appreciated that as long as aforementioned concepts and all combinations additionally conceived that describe in greater detail below are at this
Sample design it is not conflicting in the case of can be viewed as the disclosure utility model theme a part.In addition, want
Ask the theme of protection all combinations be considered as the disclosure utility model theme a part.
The foregoing and other side of the utility model teaching can be more fully appreciated from the following description with reference to attached drawing
Face, embodiment and feature.The feature and/or beneficial effect of other additional aspects such as illustrative embodiments of the utility model
To be obvious in the following description, or learnt in the practice by the embodiment instructed according to the utility model.
Brief description of the drawings
Attached drawing is not intended to drawn to scale.In the accompanying drawings, each identical or approximately uniform group shown in each figure
It can be indicated by the same numeral into part.For clarity, in each figure, it is not that each part is labeled.
Now, by example and the embodiment of the various aspects of the utility model will be described in reference to the drawings, wherein：
Fig. 1 is the structure diagram of the unmanned plane of the utility model plurality of voltage platforms.
Fig. 2 is the battery structure schematic diagram inside the battery pack of the unmanned plane of the utility model plurality of voltage platforms.
Fig. 3 is the connection signal of the first voltage output of the unmanned plane main body and battery pack of the utility model plurality of voltage platforms
Figure.
Fig. 4 is the connection signal of the second voltage output of the unmanned plane main body and battery pack of the utility model plurality of voltage platforms
Figure.
Embodiment
In order to know more about the technology contents of the utility model, especially exemplified by specific embodiment and institute's accompanying drawings are coordinated to be described as follows.
The each side of the utility model is described with reference in the disclosure, shown in the drawings of the implementation of many explanations
Example.All aspects of the embodiment of the disclosure it is not intended to cover the utility model.It should be appreciated that a variety of structures presented hereinbefore
Think and embodiment, and describe in more detail below those design and embodiment can in many ways in any one
To implement, this is because design disclosed in the utility model and embodiment are not limited to any embodiment.In addition, this practicality
New disclosed some aspects can be used alone, or with the utility model disclosed in it is otherwise it is any it is appropriately combined come
Use.
With reference to shown in Fig. 1-Fig. 4, the utility model proposes a kind of unmanned plane for power circuit automatic detecting, for
Flight inspection is carried out on power circuit, the collecting device carried using it gathers information, to have found that it is likely that presence early
Risk and problem.
The unmanned plane 100 for power circuit automatic detecting of the utility model is multi-rotor unmanned aerial vehicle, including main body
101st, the support arm 102 that is connected with main body 101, the flight component (103,104) set in support arm tail end, be arranged on main body
Symmetrically arranged a pair of of landing chassis 105 of 101 bottoms, camera assembly 106, battery pack 109 and it is arranged on determining for body top
Hyte part 108.
In the embodiment of the utility model, the support arm 102 is 4, and 4 support arms correspond to four flight components, often
A flight component drives rotating rotor 104 to form by a driving motor 103 and by driving motor 103, and driving motor 103 connects
It is connected in a circuit control mainboard.
Circuit control mainboard is arranged in main body, is integrated with flight controller, motor-drive circuit, wireless network thereon and is received
Send out module, 6 axis gyroscopes, acceleration transducer, local storage, Temperature Humidity Sensor, camera assembly image-forming assembly and
Main control processor.Foregoing flight controller, motor-drive circuit, wireless network transceiver module, 6 axis gyroscopes, acceleration sensing
Device, local storage, Temperature Humidity Sensor, the image-forming assembly of camera assembly are all connected to main control processor.
6 axis gyroscopes, acceleration transducer are respectively used to the flight attitude data of collection unmanned plane in real time, and are transferred to master
Control processor.
Flight controller is used to control motor-drive circuit according to flight attitude data, with the flight of control adjustment unmanned plane
Posture.Flight controller can use the drive circuit and type of drive of existing unmanned plane.
Temperature Humidity Sensor is used to gather the data of the Temperature and Humidity module of unmanned plane location in real time and is transferred to main control processor.
Positioning component 108, such as Big Dipper positioning component or GPS positioning component etc., for obtaining the ground of unmanned plane in real time
Position data is managed, and is transferred to main control processor.
Battery pack 109, positioned at the lower section of main body 101, using rechargeable battery pack, such as lithium battery pack, have it is multiple can
Charged lithium cells, for powering to unmanned plane.Battery pack is also connected with wireless charging circuit, for by wireless charging circuit to
Battery pack charges.
Camera assembly, is arranged on the front of battery pack 109, including lens assembly 107 and the imaging positioned at camera lens rear
Component, image-forming assembly are connected with main control processor, and image-forming assembly is used for the image that reception is gathered from lens assembly 107 and will
Video conversion is into electric signal output to main control processor.
Wireless charging circuit, has multiple micro radio charge coils, and multiple micro radio charge coils are separately mounted to
In foregoing 2 landing chassis, by charging with extraneous magnetic coupling.Multiple micro radio charge coils pass through wired line
Road such as cable are connected to the master control charging circuit being integrated in circuit control mainboard, and main control processor connects more than master control charging circuit
Connect.
Wireless network transceiver module, such as including 4G or 5G wireless communication modules, for unmanned plane to be accessed network, make
Unmanned plane is able to carry out data interaction with remote monitoring center.
Battery pack 109 is fixed on the bottom of main body 101, such as is fixed by buckle, or the component such as card slot.
Be additionally provided with battery pack 109 it is at least one set of by multiple rechargeable batteries 1092 battery pack 1093 in series,
As shown in the figure, there is battery pack as three groups, and the control circuit being connected with battery pack, control circuit have multiple effects
Transistor is answered, is switched as charge and discharge control, for controlling the discharge and recharge of battery pack.
Electric quantity monitoring circuit is additionally provided with battery pack, is connected with the battery pack and control circuit, for monitoring battery
The residual charge state of bag.
Connected to form series connection on the whole, gone here and there by alloying metal piece before the positive and negative anodes of multiple rechargeable batteries 1092
The control circuit is connected to after connection.
With reference to Fig. 2-Fig. 4, battery pack 109 is fixed to the bottom of the main body 101 of unmanned plane by we, and especially, bottom is set
A shoulder with radian is equipped with, there is a shell and receiving for fixing and installing 109. battery pack 109 of battery pack
Inside the shell at least one connects the battery pack formed and the control circuit being connected with battery pack by multiple rechargeable batteries,
Housing exterior is additionally provided with one group of electric connection terminal being connected with control circuit, for when battery pack is coupled to unmanned plane main body
Powered by electric connection terminal to unmanned plane.
The electric connection terminal includes at least two pairs of terminals (plus end and negative terminal), wherein a pair of terminal 1095 connects
At the first Battery pack group both ends, second pair of terminal 1096 is connected to the second Battery pack group both ends.
The bottom of the main body of unmanned plane is provided with four terminals 1011.
When the terminal 1011 on unmanned plane is configured to be connected with the electric connection terminal of battery pack so that in the first connection
Position, forms series connection in succession between the corresponding battery pack of described a pair of terminal battery pack corresponding with second pair of terminal, and carries
(such as Fig. 3) is exported for first voltage, in the second link position, the corresponding battery pack of a pair of terminal and second pair of terminal pair
Parallel connection is formed between the battery pack answered in succession, and second voltage output, such as Fig. 4 are provided.
In the embodiment of the utility model, rechargeable battery 1092 is identical, and the lithium electricity that nominal voltage is 3.6V
Pond.
In the first Battery pack group and the second Battery pack group, it is respectively provided with the rechargeable battery string of at least five monomers
Connection, the nominal voltage of formation is 18V.
With reference to Fig. 3,4, the numerical value of first voltage is twice of second voltage numerical value.The first voltage is 36V, and second is electric
Press as 18V.
Certainly, do not have to represent in Fig. 3, Fig. 4 of indication circuit signal, a pair of terminal and second pair of terminal are in thing
The shape arrangement that is spatially in line is managed, and second pair of terminal is located at the both sides of a pair of terminal.
Although the utility model has been disclosed with preferred embodiment as above, so it is not limited to the utility model.This reality
It is without departing from the spirit and scope of the utility model, each when that can make with new those of ordinary skill in the art
Kind changes and retouches.Therefore, the scope of protection of the utility model is when subject to those as defined in claim.
Claims (10)
- A kind of 1. unmanned plane of plurality of voltage platforms, it is characterised in that including：Main body；The support arm for being connected and being disposed below with main body；In the flight component that support arm tail end is set；It is arranged on the landing chassis of bottom part body；It is arranged on the positioning component of body top；The battery pack of bottom part body is arranged on, for powering for unmanned plane；Wherein, the support arm is 4, is centered around the uniform setting of main body surrounding, and 4 support arms correspond to four flight components, Each flight component drives rotating rotor to form by a driving motor and by driving motor, and driving motor is connected to an electricity In the control mainboard of road, circuit control mainboard is arranged in main body；Main control processor and local storage and wireless network transceiver module are integrated with the circuit control mainboard；The battery pack be fixed to the main body bottom, battery pack have a shell and accommodate inside the shell at least one It is a to connect the battery pack formed by multiple rechargeable batteries and the control circuit being connected with battery pack, housing exterior are additionally provided with One group of electric connection terminal being connected with control circuit, for when battery pack is coupled to unmanned plane main body by electric connection terminal to Unmanned plane is powered；The electric connection terminal includes at least two pairs of terminals, wherein a pair of terminal is connected to the first Battery pack group both ends, second The second Battery pack group both ends are connected to terminal, the bottom of the main body of unmanned plane is provided with four terminals, wherein, on unmanned plane Terminal is configured to be connected with the electric connection terminal of battery pack so that corresponding in the first link position, described a pair of terminal Series connection is formed between battery pack battery pack corresponding with second pair of terminal in succession, and first voltage output is provided, in the second connection Position, formed between the corresponding battery pack of described a pair of terminal battery pack corresponding with second pair of terminal it is in parallel in succession, and carry Exported for second voltage.
- 2. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the rechargeable battery is identical , and the lithium battery that nominal voltage is 3.6V.
- 3. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the first Battery pack group and second In Battery pack group, it is respectively provided with the rechargeable battery series connection of at least five monomers.
- 4. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the numerical value of the first voltage is Twice of two voltage values.
- 5. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the first voltage is 36V, second Voltage is 18V.
- 6. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that described a pair of terminal and second pair Terminal is in line shape arrangement in physical space, and second pair of terminal is located at the both sides of a pair of terminal.
- 7. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the landing chassis bottom is provided with nothing Micro USB electric coil, and be connected by cable with the master control charging circuit that one is arranged in the main body, the connection of master control charging circuit To main control processor.
- 8. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that be additionally provided with electricity in the battery pack Observation circuit is measured, is connected with the battery pack and control circuit, for monitoring the residual charge state of battery pack.
- 9. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the positioning component include GPS or At least one of person's Big Dipper positioning component.
- 10. the unmanned plane of plurality of voltage platforms according to claim 1, it is characterised in that the control circuit has multiple Field-effect transistor, switchs as charge and discharge control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720985639.9U CN207257997U (en) | 2017-08-09 | 2017-08-09 | The unmanned plane of plurality of voltage platforms |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720985639.9U CN207257997U (en) | 2017-08-09 | 2017-08-09 | The unmanned plane of plurality of voltage platforms |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207257997U true CN207257997U (en) | 2018-04-20 |
Family
ID=61924370
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720985639.9U Expired - Fee Related CN207257997U (en) | 2017-08-09 | 2017-08-09 | The unmanned plane of plurality of voltage platforms |
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| Country | Link |
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| CN (1) | CN207257997U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108944497A (en) * | 2018-05-30 | 2018-12-07 | 合肥市春华起重机械有限公司 | A kind of AGV trolley wireless charging system |
| CN109515726A (en) * | 2018-12-25 | 2019-03-26 | 汇星海科技（天津）有限公司 | A kind of unmanned plane electrical source of power switching circuit plate and its switching method |
| CN109861464A (en) * | 2019-03-27 | 2019-06-07 | 江苏金丰机电有限公司 | A kind of integrated motor system of integrated manipulator and charger |
-
2017
- 2017-08-09 CN CN201720985639.9U patent/CN207257997U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108944497A (en) * | 2018-05-30 | 2018-12-07 | 合肥市春华起重机械有限公司 | A kind of AGV trolley wireless charging system |
| CN109515726A (en) * | 2018-12-25 | 2019-03-26 | 汇星海科技（天津）有限公司 | A kind of unmanned plane electrical source of power switching circuit plate and its switching method |
| CN109861464A (en) * | 2019-03-27 | 2019-06-07 | 江苏金丰机电有限公司 | A kind of integrated motor system of integrated manipulator and charger |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180420 Termination date: 20190809 |