CN207173949U - A kind of long endurance multi-rotor unmanned aerial vehicle - Google Patents
A kind of long endurance multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN207173949U CN207173949U CN201720835177.2U CN201720835177U CN207173949U CN 207173949 U CN207173949 U CN 207173949U CN 201720835177 U CN201720835177 U CN 201720835177U CN 207173949 U CN207173949 U CN 207173949U
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Abstract
The utility model discloses a kind of long endurance multi-rotor unmanned aerial vehicle, including：Upper and lower laminate, horn, foot stool, dynamical system, miniature head, camera, mapping head, number blit transmission module, battery plug, battery, power management module, power cathode hub, positive source hub, LED, USB module and unmanned plane fly control；Corner part screw fixes top plate and lower plywood, one end of horn is connected with corner part, dynamical system is arranged on the other end of horn by chuck, foot stool is arranged on lower plywood, battery plug, positive source, negative pole hub are arranged on lower plywood by screw, number blit transmission module, unmanned plane fly control and power management module is bonded on lower plywood, LED and USB module are fixed on the downside of top plate, miniature head and mapping head are fixed on the lower end of lower plywood, and battery is arranged on lower plywood.The utility model extends the cruising time of unmanned plane, realizes the replacing of each task module.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, more particularly to a kind of long endurance multi-rotor unmanned aerial vehicle.
Background technology
In recent years, more rotor flying machines are quickly grown, and are not only also planted in the field of taking photo by plane, more rotor flying machines in agricultural
The fields such as guarantor, power-line patrolling, geological prospecting, traffic administration, express transportation equally have considerable development prospect.It is existing
In multi-rotor unmanned aerial vehicle, wheelbase below 500mm type due to size limit, typically using integrated design, i.e., more rotors
The task module and fuselage of unmanned plane are directly bound, and task module is non-exchange, cruising time between 20-30 minutes,
It is easy to carry；Wheelbase is in the task module of 500mm to the 1000m replaceable multi-rotor unmanned aerial vehicle of type, but the weight of task module
Measure larger so that its cruising time shortens, it is more difficult to carries, i.e., multi-rotor unmanned aerial vehicle of the prior art can not take into account continuation of the journey simultaneously
Time is grown and the two features of replaceable task module.
The content of the invention
In view of this, the utility model provides a kind of long endurance multi-rotor unmanned aerial vehicle, when it extends the continuation of the journey of unmanned plane
Between, and realize the replacing of each task module.
The utility model is solved the above problems by following technological means：
A kind of long endurance multi-rotor unmanned aerial vehicle of the present utility model, including：Top plate, lower plywood, horn, foot stool, power
System, miniature head, camera, mapping head, number blit transmission module, battery plug, battery, power management module, power cathode
Hub, positive source hub, LED, USB module and unmanned plane fly control；The capacity of the battery is more than or equal to
16000mAH；The corner part is fixed the top plate and the lower plywood by screw, one end of the horn and institute
The connection of corner part is stated, the dynamical system is arranged on the other end of the horn, and the spiral shell of the dynamical system by chuck
The angle revolved between oar plane and ground level is 2 degree, and the foot stool is arranged on the lower plywood by corner part connecting pieces,
The battery plug, the positive source hub and the power cathode hub are arranged on the lower plywood by screw
On, and the positive source hub is located at the outside of the lower plywood, several blit transmission modules, the unmanned plane fly control and
For the power management module by 3M adhesive tape bondings on the lower plywood, the LED and the USB module are fixed on institute
State on the downside of top plate, the miniature head and the mapping head are fixed under the lower plywood by rubber shock-absorbing ball
End, the battery are arranged on the lower plywood by screw or magic band；The battery is plugged on the battery plug
On, the battery plug is connected with the positive source hub and the power cathode hub respectively, the power management
The input of module is connected with the positive source hub and the power cathode hub respectively, the power management module
Output end and the unmanned plane fly control connection, several blit transmission modules, the dynamical system, the LED and the USB
Module flies control connection with the unmanned plane.
Further, in addition to the GNSS locating modules and compass module that are arranged on the top plate, the GNSS determine
Position module and compass module fly control connection with the unmanned plane.
Further, in addition to multiple bay, the multiple bay are hinged on the upper surface of the top plate.
Further, the dynamical system is set with for E1200 specialties power.
Further, the model microhard n920 of several blit transmission modules.
Further, the unmanned plane flies the model micropilot MP2128heli2 of control.
A kind of long endurance multi-rotor unmanned aerial vehicle of the present utility model has the advantages that：
The utility model provides a kind of long endurance multi-rotor unmanned aerial vehicle, including top plate, lower plywood, horn, foot stool, dynamic
Force system, miniature head, camera, mapping head, number blit transmission module, battery plug, battery, power management module, power supply are born
Pole hub, positive source hub, LED, USB module and unmanned plane fly control, wherein, the capacity of battery is more than or equal to
16000mAH；The utility model by miniature head, camera, mapping head, number blit transmission module, LED, USB module and nobody
Machine flies the task modules such as control, and by screw, either 3M adhesive tape bondings are on top plate or lower plywood, convenient disassembly so that use
Family respectively changes each task module according to the function of being actually needed and realize, realizes the replacing of task module；In addition, this practicality
The new capacity that battery can be changed according to load, to extend the cruising time of unmanned plane.
Brief description of the drawings
The utility model is further described with reference to the accompanying drawings and examples.
Fig. 1 is a kind of structural representation of long endurance multi-rotor unmanned aerial vehicle of the present utility model；
Fig. 2 is the structural representation of the long endurance multi-rotor unmanned aerial vehicle of another kind of the present utility model；
Fig. 3 is the structural representation of the long endurance multi-rotor unmanned aerial vehicle of another kind of the present utility model；
Fig. 4 is a kind of front view of corner part of the present utility model；
Fig. 5 is a kind of top view of corner part of the present utility model；
Fig. 6 is a kind of side view of corner part of the present utility model；
Fig. 7 is a kind of front view of chuck of the present utility model；
Fig. 8 is a kind of top view of chuck of the present utility model；
Fig. 9 is a kind of side view of chuck of the present utility model；
Figure 10 is a kind of structural representation of top plate of the present utility model；
Figure 11 is a kind of structural representation of lower plywood of the present utility model；
Figure 12 is a kind of front view of multiple bay of the present utility model；
Figure 13 is a kind of top view of multiple bay of the present utility model.
Embodiment
The utility model is described in detail below with reference to accompanying drawing, as shown in figure 1 to figure 13：One kind of the present embodiment
Long endurance multi-rotor unmanned aerial vehicle includes：Top plate 1, lower plywood 2, horn 3, foot stool 4, dynamical system 5, miniature head 6, camera 7,
Survey and draw head 8, number blit transmission module 9, battery plug 10, battery 11, power management module 12, power cathode hub 13, electricity
Source positive pole hub 14, LED 16, USB module 17 and unmanned plane fly control 18；The capacity of the battery 11 is more than or equal to
16000mAH。
The corner part is fixed the top plate 1 and the lower plywood 2 by screw, one end of the horn 3 with
The corner part connection, the dynamical system 5 are arranged on the other end of the horn 3, and the dynamical system 5 by chuck
Propeller plan and ground level between angle be 2 degree, the foot stool 4 is arranged on the lower floor by corner part connecting pieces
On plate 2, the battery plug 10, the positive source hub 14 and the power cathode hub 13 are installed by screw
On the lower plywood 2, and the positive source hub 14 is located at the outside of the lower plywood 2, several blit transmission modules
9th, the unmanned plane flies control 18 and the power management module 12 by 3M adhesive tape bondings on the lower plywood 2, the LED
Lamp 16 and the USB module 17 are fixed on the downside of top plate 1, and the miniature head 6 and the mapping head 8 pass through rubber
Glue shock-absorbing ball is fixed on the lower end of the lower plywood 2, and the camera 7 is arranged on the miniature head 6, and the battery 11 passes through
Screw or magic band are arranged on the lower plywood 2.
The battery 11 is plugged on the battery plug 10, the battery plug 10 respectively with the positive source line concentration
Device 14 and the power cathode hub 13 connect, the input of the power management module 12 respectively with the positive source collection
Line device 14 and the power cathode hub 13 connect, and output end and the unmanned plane of the power management module 12 fly control 18
Connection, several blit transmission modules 9, the dynamical system 5, the LED 16 and the USB module 17 with the unmanned plane
Fly the connection of control 18.
Wherein, it is in order that unmanned plane the angle between the propeller plan and ground level of dynamical system 5 to be arranged into 2 degree
It can be offset in flight course with less inclination correction unmanned aerial vehicle body position, there is provided extra unmanned plane stability；Institute
State positive source hub 14 and be arranged on the outside of the lower plywood 2 and avoid high current on top plate 1 or lower plywood 2
Other electronic components produce interference.
Specifically, battery 11 provides power supply by battery plug 10 for unmanned plane, the wire that battery plug 10 is drawn passes through
4mm bananas head access power cathode hub 13 and positive source hub 14, it is dynamical system 5, power management module 12, miniature
The power supply of head 6, camera 7 and mapping head 8 passes through 3.5mm bananas head and accesses power cathode hub 13 and positive source line concentration
Device 14, to realize power supply；Miniature head 6, camera 7 and mapping head 8 also fly control by 2.54mm Du Pont's terminal and unmanned plane
18 connections, unmanned plane fly control 18 and are used to control miniature head 6 and survey and draw the direction of head 8 and the shooting of camera 7；Power supply pipe
Reason module 12 flies control 18 with unmanned plane by data wire and is connected, and flying control 18 for unmanned plane provides stable voltage and cell voltage letter
Breath；Unmanned plane flies control 18 and is powered for number blit transmission modules 9 and provide flight parameter；Number blit transmission module 9 is that unmanned plane flies control 18
Ground remote control data are provided；Dynamical system 5 flies control 18 with unmanned plane and is connected by 2.54mm Du Pont's terminal, and unmanned plane flies control 18
Control the motor speed of dynamical system 5；LED is used to show the current state of unmanned plane；USB module 17 is believed for data storage
Breath.
It should be noted that the quantity of horn 3 of the present utility model is four, the quantity of corresponding corner part is also four
Individual, four corner parts are symmetricly set between top plate 1 and lower plywood 2, and the quantity of dynamical system 5 is also four, Mei Gedong
Force system 5 is arranged on the other end of each horn 3；The quantity of foot stool 4 and corresponding corner part is also four, each corner zero
Part is separately positioned on one end away from top plate 1 on each horn 3.
As the further improvement of above-mentioned technical proposal, the long endurance multi-rotor unmanned aerial vehicle also includes being arranged on described
GNSS locating modules and compass module 19 on laminate, the GNSS locating modules and compass module 19 with it is described nobody
Machine flies the connection of control 18.
As the further improvement of above-mentioned technical proposal, the long endurance multi-rotor unmanned aerial vehicle also includes multiple bay
20, the multiple bay 20 is hinged on the upper surface of the top plate 1.
Wherein, multiple bay 20 is used to install the components such as the battery subsequently expanded, head.
In the present embodiment, the dynamical system 5 is set with for E1200 specialties power.
In the present embodiment, the model microhard n920 of several blit transmission modules 9.
In the present embodiment, the unmanned plane flies the model micropilot MP2128heli2 of control 18.
The utility model provides a kind of long endurance multi-rotor unmanned aerial vehicle, including top plate 1, lower plywood 2, horn 3, foot stool
4th, dynamical system 5, miniature head 6, camera 7, mapping head 8, number blit transmission module 9, battery plug 10, battery 11, power supply pipe
Manage module 12, power cathode hub 13, positive source hub 14, LED 16, USB module 17 and unmanned plane and fly control 18, its
In, the capacity of battery 11 is more than or equal to 16000mAH；The utility model by miniature head 6, camera 7, mapping head 8, number blit
Transmission module 9, LED 16, USB module 17 and unmanned plane fly the control task modules such as 18 by screw or 3M adhesive tape bondings upper
On laminate 1 or lower plywood 2, convenient disassembly so that user respectively changes each task mould according to the function of being actually needed and realize
Block, realize the replacing of task module；In addition, the utility model can change the capacity of battery 11 according to load, to prolong
The cruising time of long unmanned plane.
Finally illustrate, above example is only unrestricted to illustrate the technical solution of the utility model, although ginseng
The utility model is described in detail according to preferred embodiment, it will be understood by those within the art that, can be to this
The technical scheme of utility model is modified or equivalent substitution, without departing from the objective and model of technical solutions of the utility model
Enclose, it all should cover among right of the present utility model.
Claims (6)
- A kind of 1. long endurance multi-rotor unmanned aerial vehicle, it is characterised in that：Including：Top plate, lower plywood, horn, foot stool, dynamical system System, miniature head, camera, mapping head, number blit transmission module, battery plug, battery, power management module, power cathode collection Line device, positive source hub, LED, USB module and unmanned plane fly control；The capacity of the battery is more than or equal to 16000mAH；Corner part is fixed the top plate and the lower plywood by screw, and one end and the corner part of the horn connect Connect, the dynamical system is arranged on the other end of the horn, and the propeller plan of the dynamical system and ground by chuck Angle between plane is 2 degree, and the foot stool is arranged on the lower plywood by corner part connecting pieces, and the battery is inserted Head, the positive source hub and the power cathode hub are arranged on the lower plywood by screw, and described Positive source hub is located at the outside of the lower plywood, and several blit transmission modules, the unmanned plane fly control and the power supply For management module by 3M adhesive tape bondings on the lower plywood, the LED and the USB module are fixed on the top plate Downside, the miniature head and the mapping head are fixed on the lower end of the lower plywood, the electricity by rubber shock-absorbing ball Pond is arranged on the lower plywood by screw or magic band；The battery is plugged on the battery plug, the battery plug respectively with the positive source hub and the electricity Source negative pole hub connection, the input of the power management module are born with the positive source hub and the power supply respectively Pole hub connection, the output end of the power management module fly control connection, several blit transmission modules, institute with the unmanned plane State dynamical system, the LED and the USB module and fly control connection with the unmanned plane.
- A kind of 2. long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：Also include being arranged on described GNSS locating modules and compass module on laminate, the GNSS locating modules and compass module fly with the unmanned plane Control connection.
- A kind of 3. long endurance multi-rotor unmanned aerial vehicle according to claim 2, it is characterised in that：Also include multiple bay, The multiple bay is hinged on the upper surface of the top plate.
- A kind of 4. long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The dynamical system is E1200 specialties power is set with.
- A kind of 5. long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：Several blit transmission modules Model microhard n920.
- A kind of 6. long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The unmanned plane flies the type of control Number it is micropilot MP2128heli2.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720835177.2U CN207173949U (en) | 2017-07-11 | 2017-07-11 | A kind of long endurance multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720835177.2U CN207173949U (en) | 2017-07-11 | 2017-07-11 | A kind of long endurance multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207173949U true CN207173949U (en) | 2018-04-03 |
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ID=61734402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720835177.2U Active CN207173949U (en) | 2017-07-11 | 2017-07-11 | A kind of long endurance multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207173949U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110800280A (en) * | 2018-11-29 | 2020-02-14 | 深圳市大疆创新科技有限公司 | Image transmission device, assembly method thereof and movable platform |
| CN116812184A (en) * | 2023-07-04 | 2023-09-29 | 深圳技术大学 | Six-axis unmanned aerial vehicle for radar mapping |
-
2017
- 2017-07-11 CN CN201720835177.2U patent/CN207173949U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110800280A (en) * | 2018-11-29 | 2020-02-14 | 深圳市大疆创新科技有限公司 | Image transmission device, assembly method thereof and movable platform |
| WO2020107338A1 (en) * | 2018-11-29 | 2020-06-04 | 深圳市大疆创新科技有限公司 | Image transmission apparatus, and assembly method and movable platform thereof |
| CN116812184A (en) * | 2023-07-04 | 2023-09-29 | 深圳技术大学 | Six-axis unmanned aerial vehicle for radar mapping |
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