CN109229349A - A kind of long endurance multi-rotor unmanned aerial vehicle - Google Patents
A kind of long endurance multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN109229349A CN109229349A CN201710561671.9A CN201710561671A CN109229349A CN 109229349 A CN109229349 A CN 109229349A CN 201710561671 A CN201710561671 A CN 201710561671A CN 109229349 A CN109229349 A CN 109229349A
- Authority
- CN
- China
- Prior art keywords
- module
- lower plywood
- battery
- unmanned plane
- hub
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a kind of long endurance multi-rotor unmanned aerial vehicles, comprising: upper and lower laminate, horn, foot prop, dynamical system, miniature holder, camera, mapping holder, number blit transmission module, battery plug, battery, power management module, power cathode hub, positive pole hub, LED light, USB module and unmanned plane fly control；Corner part screw fixes top plate and lower plywood, one end of horn is connect with corner part, dynamical system is mounted on the other end of horn by collet, foot prop is mounted on lower plywood, battery plug, positive pole, cathode hub are mounted on lower plywood by screw, number blit transmission module, unmanned plane fly control and power management module is bonded on lower plywood, LED light and USB module are fixed on the downside of top plate, miniature holder and mapping holder are fixed on the lower end of lower plywood, and battery is mounted on lower plywood.The present invention extends the cruise duration of unmanned plane, realizes the replacement of each task module.
Description
Technical field
The present invention relates to air vehicle technique field, in particular to a kind of long endurance multi-rotor unmanned aerial vehicle.
Background technique
In recent years, more rotor flying machines are quickly grown, and not only in the field of taking photo by plane, more rotor flying machines are also planted 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, since size limits, generally uses integrated design, i.e., more rotors in 500mm type below
The task module of unmanned plane is directly bound with fuselage, and task module is non-exchange, cruise duration between 20-30 minutes,
It is easy to carry；Task module of the wheelbase in the replaceable multi-rotor unmanned aerial vehicle of type of 500mm to 1000m, but the weight of task module
Measure it is larger so that its cruise duration shorten, it is more difficult to carry, i.e., multi-rotor unmanned aerial vehicle in the prior art cannot combine continuation of the journey
Time length and the two features of replaceable task module.
Summary of the invention
In view of this, the present invention provides a kind of long endurance multi-rotor unmanned aerial vehicle, the cruise duration of unmanned plane is extended, and
Realize the replacement of each task module.
The present invention is solved the above problems by following technological means:
A kind of long endurance multi-rotor unmanned aerial vehicle of the invention, comprising: top plate, lower plywood, horn, foot prop, dynamical system,
Miniature holder, camera, mapping holder, number blit transmission module, battery plug, battery, power management module, power cathode line concentration
Device, positive pole hub, LED light, USB module and unmanned plane fly control；The capacity of the battery is more than or equal to 16000mAH；Institute
It states corner part and is fixed the top plate and the lower plywood by screw, one end of the horn and the corner part connect
It connects, the dynamical system is mounted on the other end of the horn, and the propeller plan of the dynamical system and ground by collet
Angle between plane is 2 degree, and the foot prop is mounted on the lower plywood by corner part connecting pieces, and the battery is inserted
Head, the positive pole hub and the power cathode hub pass through screw and are mounted on the lower plywood, and described
Positive pole hub is located at the outside of the lower plywood, and several blit transmission modules, the unmanned plane fly control and the power supply
Management module passes through 3M adhesive tape bonding on the lower plywood, and the LED light and the USB module are fixed on the top plate
Downside, the miniature holder and the mapping holder pass through the lower end that rubber shock-absorbing ball is fixed on the lower plywood, the electricity
Pond is mounted on the lower plywood by screw or magic band；The battery is plugged on the battery plug, the electricity
Pond plug is connect with the positive pole hub and the power cathode hub respectively, the input of the power management module
End connect respectively with the positive pole hub and the power cathode hub, the output end of the power management module and
The unmanned plane flies control connection, and several blit transmission modules, the dynamical system, the LED light and the USB module are and institute
It states unmanned plane and flies control connection.
It further, further include the GNSS locating module being arranged on the top plate and compass module, the GNSS is fixed
Position module and compass module fly control connection with the unmanned plane.
It further, further include multi-purpose stand, the multi-purpose stand is hinged on the upper surface of the top plate.
Further, the dynamical system is E1200 profession power suit.
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 invention has the advantages that
The present invention provides a kind of long endurance multi-rotor unmanned aerial vehicles, including top plate, lower plywood, horn, foot prop, dynamical system
System, miniature holder, camera, mapping holder, number blit transmission module, battery plug, battery, power management module, power cathode collection
Line device, positive pole hub, LED light, USB module and unmanned plane fly control, wherein the capacity of battery is more than or equal to
16000mAH；The present invention flies miniature holder, camera, mapping holder, number blit transmission module, LED light, USB module and unmanned plane
The task modules such as control pass through screw or 3M adhesive tape bonding on top plate or lower plywood, convenient disassembly, so that user is each
Each task module is replaced with the function of realization according to actual needs, realizes the replacement of task module；In addition, the present invention can root
The capacity of battery is replaced, according to payload size to extend the cruise duration of unmanned plane.
Detailed description of the invention
The invention will be further described with reference to the accompanying drawings and examples.
Fig. 1 is a kind of structural schematic diagram of long endurance multi-rotor unmanned aerial vehicle of the invention；
Fig. 2 is the structural schematic diagram of the long endurance multi-rotor unmanned aerial vehicle of another kind of the invention；
Fig. 3 is the structural schematic diagram of the long endurance multi-rotor unmanned aerial vehicle of another kind of the invention；
Fig. 4 is a kind of front view of corner part of the invention；
Fig. 5 is a kind of top view of corner part of the invention；
Fig. 6 is a kind of side view of corner part of the invention；
Fig. 7 is a kind of front view of collet of the invention；
Fig. 8 is a kind of top view of collet of the invention；
Fig. 9 is a kind of side view of collet of the invention；
Figure 10 is a kind of structural schematic diagram of top plate of the invention；
Figure 11 is a kind of structural schematic diagram of lower plywood of the invention；
Figure 12 is a kind of main view of multi-purpose stand of the invention；
Figure 13 is a kind of top view of multi-purpose stand of the invention.
Specific embodiment
Below with reference to attached drawing, the present invention is described in detail, as shown in figure 1 to figure 13: a kind of long boat of the present embodiment
When multi-rotor unmanned aerial vehicle include: top plate 1, lower plywood 2, horn 3, foot prop 4, dynamical system 5, miniature holder 6, camera 7, survey
Draw holder 8, number blit transmission module 9, battery plug 10, battery 11, power management module 12, power cathode hub 13, power supply
Positive hub 14, LED light 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 by 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 mounted on the other end of the horn 3, and the dynamical system 5 by collet
Propeller plan and ground level between angle be 2 degree, the foot prop 4 is mounted on the lower layer by corner part connecting pieces
On plate 2, the battery plug 10, the positive pole hub 14 and the power cathode hub 13 are installed by screw
On the lower plywood 2, and the positive pole hub 14 is located at the outside of the lower plywood 2, several blit transmission modules
9, the unmanned plane flies control 18 and the power management module 12 and passes through 3M adhesive tape bonding on the lower plywood 2, described
LED light 16 and the USB module 17 are fixed on 1 downside of top plate, and the miniature holder 6 and the mapping holder 8 are logical
The lower end that rubber shock-absorbing ball is fixed on the lower plywood 2 is crossed, the camera 7 is arranged on the miniature holder 6, the battery 11
It is mounted on the lower plywood 2 by screw or magic band.
The battery 11 is plugged on the battery plug 10, the battery plug 10 respectively with the positive pole line concentration
Device 14 and the power cathode hub 13 connection, the input terminal of the power management module 12 respectively with the positive pole collection
Line device 14 and the power cathode hub 13 connection, the 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 light 16 and the USB module 17 with it is described nobody
Machine flies 18 connection of control.
Wherein, setting 2 degree for the angle between the propeller plan and ground level of dynamical system 5 is to make unmanned plane
In flight course additional unmanned plane stability can be provided with lesser inclination correction unmanned aerial vehicle body positional shift；Institute
It states positive pole hub 14 outside of the lower plywood 2 is set and avoid high current on top plate 1 or lower plywood 2
Other electronic components generate interference.
Specifically, battery 11 provides power supply by battery plug 10 for unmanned plane, the conducting wire that battery plug 10 is drawn passes through
4mm banana head accesses power cathode hub 13 and positive pole hub 14, dynamical system 5, power management module 12, miniature
The power supply of holder 6, camera 7 and mapping holder 8 accesses power cathode hub 13 and positive pole line concentration by 3.5mm banana head
Device 14, to realize power supply；Miniature holder 6, camera 7 and mapping holder 8 also fly control by Du Pont's terminal of 2.54mm and unmanned plane
18 connections, unmanned plane fly control 18 for controlling the direction of miniature holder 6 and mapping holder 8 and the shooting of camera 7；Power supply pipe
Reason module 12 flies control 18 with unmanned plane by data line and connect, and flies control 18 for unmanned plane and provides stable voltage and cell voltage
Information；Unmanned plane flies control 18 and powers for number blit transmission module 9 and provide flight parameter；Number blit transmission module 9 is that unmanned plane flies control
18 provide ground remote control data；Dynamical system 5 flies control 18 with unmanned plane and is connect by Du Pont's terminal of 2.54mm, and unmanned plane flies
The motor speed of 18 control dynamical system 5 of control；LED light is for showing the current state of unmanned plane；USB module 17 is for storing number
It is believed that breath.
It should be noted that the quantity of horn 3 of the invention is four, the quantity of corresponding corner part is also four,
Four corner parts are symmetricly set between top plate 1 and lower plywood 2, and the quantity of dynamical system 5 is also four, each dynamical system
The other end of each horn 3 is arranged in system 5；The quantity of foot prop 4 and corresponding corner part is also four, each corner part point
One end on each horn 3 far from top plate 1 is not set.
As a further improvement of the above technical scheme, the long endurance multi-rotor unmanned aerial vehicle further includes being arranged on described
GNSS locating module and compass module 19 on laminate, the GNSS locating module and compass module 19 with it is described nobody
Machine flies 18 connection of control.
As a further improvement of the above technical scheme, the long endurance multi-rotor unmanned aerial vehicle further includes multi-purpose stand
20, the multi-purpose stand 20 is hinged on the upper surface of the top plate 1.
Wherein, multi-purpose stand 20 is for installing the components such as battery, the holder of subsequent expansion.
In the present embodiment, the dynamical system 5 is E1200 profession power suit.
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 present invention provides a kind of long endurance multi-rotor unmanned aerial vehicle, including it is top plate 1, lower plywood 2, horn 3, foot prop 4, dynamic
Force system 5, miniature holder 6, camera 7, mapping holder 8, number blit transmission module 9, battery plug 10, battery 11, power management mould
Block 12, power cathode hub 13, positive pole hub 14, LED light 16, USB module 17 and unmanned plane fly control 18, wherein
The capacity of battery 11 is more than or equal to 16000mAH；The present invention by miniature holder 6, camera 7, mapping holder 8, number blit transmission module 9,
LED light 16, USB module 17 and unmanned plane fly the task modules such as control 18 pass through screw or 3M adhesive tape bonding in top plate 1 or
On person's lower plywood 2, convenient disassembly is realized so that user respectively replaces each task module with the function of realization according to actual needs
The replacement of task module；In addition, the present invention can replace the capacity of battery 11 according to payload size, to extend the continuous of unmanned plane
ETS estimated time of sailing.
Finally, it is stated that the above examples are only used to illustrate the technical scheme of the present invention and are not limiting, although referring to compared with
Good embodiment describes the invention in detail, those skilled in the art should understand that, it can be to skill of the invention
Art scheme is modified or replaced equivalently, and without departing from the objective and range of technical solution of the present invention, should all be covered at this
In the scope of the claims of invention.
Claims (6)
1. a kind of long endurance multi-rotor unmanned aerial vehicle, it is characterised in that: include: top plate, lower plywood, horn, foot prop, dynamical system
System, miniature holder, camera, mapping holder, number blit transmission module, battery plug, battery, power management module, power cathode collection
Line device, positive pole hub, LED light, 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 the corner
Part connection, the dynamical system is mounted on the other end of the horn by collet, and the propeller of the dynamical system is flat
Angle between face and ground level is 2 degree, and the foot prop is mounted on the lower plywood by corner part connecting pieces, the electricity
Pond plug, the positive pole hub and the power cathode hub pass through screw and are mounted on the lower plywood, and
The positive pole hub is located at the outside of the lower plywood, and several blit transmission modules, the unmanned plane fly control and described
Power management module passes through 3M adhesive tape bonding on the lower plywood, and the LED light and the USB module are fixed on described
On the downside of laminate, the miniature holder and the mapping holder pass through the lower end that rubber shock-absorbing ball is fixed on the lower plywood, institute
Battery is stated to be mounted on the lower plywood by screw or magic band；
The battery is plugged on the battery plug, the battery plug respectively with the positive pole hub and the electricity
The connection of source cathode hub, the input terminal of the power management module are negative with the positive pole hub and the power supply respectively
The connection of pole hub, the output end of the power management module and the unmanned plane fly control connection, several blit transmission modules, institute
It states dynamical system, the LED light and the USB module and flies control connection with the unmanned plane.
2. a kind of long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that: further include being arranged on described
GNSS locating module and compass module on laminate, the GNSS locating module and compass module fly with the unmanned plane
Control connection.
3. a kind of long endurance multi-rotor unmanned aerial vehicle according to claim 2, it is characterised in that: it further include multi-purpose stand,
The multi-purpose stand is hinged on the upper surface of the top plate.
4. a kind of long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that: the dynamical system is
E1200 profession power suit.
5. a kind of long endurance multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that: several blit transmission modules
Model microhard n920.
6. a kind of 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 be micropilot MP2128heli2.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710561671.9A CN109229349A (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 |
|---|---|---|---|
| CN201710561671.9A CN109229349A (en) | 2017-07-11 | 2017-07-11 | A kind of long endurance multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109229349A true CN109229349A (en) | 2019-01-18 |
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ID=65083397
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710561671.9A Pending CN109229349A (en) | 2017-07-11 | 2017-07-11 | A kind of long endurance multi-rotor unmanned aerial vehicle |
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