CN104627361B - A kind of Modularized unmanned aircraft - Google Patents
A kind of Modularized unmanned aircraft Download PDFInfo
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- CN104627361B CN104627361B CN201510060890.XA CN201510060890A CN104627361B CN 104627361 B CN104627361 B CN 104627361B CN 201510060890 A CN201510060890 A CN 201510060890A CN 104627361 B CN104627361 B CN 104627361B
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- Prior art keywords
- control box
- driving lever
- axis motor
- unmanned vehicle
- output shaft
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- 238000009434 installation Methods 0.000 claims description 17
- 230000005389 magnetism Effects 0.000 claims description 11
- 230000005611 electricity Effects 0.000 claims description 9
- 230000007480 spreading Effects 0.000 claims description 5
- 229920000742 Cotton Polymers 0.000 claims description 3
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 230000001771 impaired effect Effects 0.000 abstract description 4
- 238000012423 maintenance Methods 0.000 abstract description 2
- 238000012360 testing method Methods 0.000 abstract description 2
- 239000002360 explosive Substances 0.000 description 5
- 238000012937 correction Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
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- 238000000034 method Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
The present invention relates to a kind of Modularized unmanned aircraft.The unmanned vehicle includes fuselage device, fuselage device includes shell, propeller and the motor of unmanned vehicle, aircraft also includes control box, for shooting and transmitting photographed data to the filming apparatus of external equipment and the supply unit for being powered for unmanned vehicle, filming apparatus and supply unit are fixed on below control box, the main control board of unmanned vehicle is provided with control box, supply unit electrically connects with filming apparatus, main control board and motor respectively.The part of unmanned vehicle is divided into several independent devices by the present invention, in assembling, first can distinguish assembling test by each device, then refill and be made into unmanned vehicle, cost is reduced, and the quality of aircraft also gets a promotion；And when unmanned vehicle is by hitting impaired, can be directed to impaired device is repaired or is changed, and other devices not being damaged can retain, and maintenance cost and time are all reduced.
Description
Technical field
The present invention relates to aircraft, more particularly to a kind of Modularized unmanned aircraft.
Background technology
At present small-sized unmanned aircraft widely apply take photo by plane, agricultural, fire, the field such as natural calamity early warning, with skill
The maturation of art and the reduction of cost, it will there is increasing field to use.
The small-sized unmanned aircraft of commercial type, is generally designed using upper and lower covers, motor, flight required for aircraft
Indicator lamp, flight control system, GPS system, magnetic system etc. be all put into aircraft upper and lower covers, production and assembly are very tired
Difficulty, it is not easy to repair.Aircraft is in high-speed flight, the easy misoperation of manipulator, and aircraft knocks building or big in high-altitude
Tree, or even, so as to cause aircraft to be damaged, can not directly be repaired from falling from high altitude.Manipulator can only buy new product, but fly
The current price of row device is a no small loss for consumers all costly.
The content of the invention
The defects of it is an object of the invention to overcome prior art, and a kind of Modularized unmanned aircraft is provided, with drop
Low-dimensional is repaiied and assembly cost.
To achieve the above object, the present invention uses following technical scheme：
A kind of Modularized unmanned aircraft, including fuselage device, fuselage device include the shell of unmanned vehicle and set
The motor of propeller and driving propeller rotational on shell；Unmanned vehicle also includes being embedded at the control among shell
Box, for shoot and photographed data is transmitted to the filming apparatus of external equipment and the power supply for being powered for unmanned vehicle
Device, filming apparatus and supply unit are fixed below control box, and the main control board of unmanned vehicle, power supply are provided with control box
Device electrically connects with filming apparatus, main control board and motor respectively.
Further, shell is provided with four spreading arms extended outward, and shell is in cross, and motor is fixed on spreading arm
Outer end, upward, propeller is located on motor output shaft and rotated coaxially with motor output shaft motor output shaft.
Further, shell is provided with the installation position for being used for fixing control box, and installation position is provided with upper shed and under shed, controls
Box processed loads in installation position under shed, the upper shed of the top insertion installation position of control box.
Further, main control board is provided with RF modules, is additionally provided with GPS circuitry plate in control box, GPS circuitry plate is fixed
It is provided with above main control board and between the two shielding cotton.
Further, control box is provided with the driving lever being rotatably connected with control box, and main control board is provided with power switch,
Power switch is provided with the elastic pressuring plate for being used for controlling power switch break-make, and driving lever includes main part and for extruding elastic pressure
The afterbody of piece, driving lever are rotatably connected with control box in main part with the junction of afterbody.
Further, when driving lever is located at de-energized, the main part of driving lever is placed within control box, and the afterbody of driving lever is remote
From elastic pressuring plate, power switch power-off；When driving lever is allocated to on-position, the main part of driving lever is exposed to outside control box,
The afterbody of driving lever pushes elastic pressuring plate, and power switch is powered.
Further, when driving lever is located at de-energized, driving lever is horizontal positioned；When driving lever is allocated to on-position, dial
Bar is placed vertically.
Further, it is provided with earth magnetism circuit board in the main part of driving lever.
Further, filming apparatus includes video camera, head and three spindle motors, is provided with head wiring board in head, and three
Spindle motor is divided into Z axis motor, y-axis motor and X-axis motor, and Z axis motor is located in head, and down, Y-axis is electric for Z axis motor output shaft
Machine is fixedly connected on Z axis motor output shaft by a lower swing arm, and X-axis motor is fixedly connected on y-axis motor by a horizontal arm
On output shaft, video camera is fixed on X-axis motor output shaft.
Further, supply unit includes battery case, the battery core being located in battery case and is located on battery outer box wall
Electricity shows bar, and electricity shows that bar electrically connects with battery core.
Compared with the prior art, the invention has the advantages that：
The part of unmanned vehicle is divided into several independent devices by the present invention, can first each device in assembling
Assembling test respectively, then refills and is made into unmanned vehicle, cost is reduced, and the quality of aircraft also gets a promotion；And
When unmanned vehicle is by hitting impaired, impaired device can be directed to and repaired or changed, other dresses not being damaged
Putting to retain, and maintenance cost and time are all reduced.
Brief description of the drawings
Fig. 1 is the explosive view of unmanned vehicle；
Fig. 2 is the explosive view of fuselage device；
Fig. 3 is the explosive view of control box；
Fig. 4 is main control board stereogram；
Fig. 5 is the sectional arrangement drawing (driving lever closure) of control box；
Fig. 6 is the sectional arrangement drawing (driving lever opening procedure) of control box；
Fig. 7 is the sectional arrangement drawing of control box (driving lever is opened completely)；
Fig. 8 is Fig. 7 partial enlarged drawing；
Fig. 9 is the top view of control box；
Figure 10 is the explosive view of filming apparatus；
Figure 11 is the assembling stereogram of filming apparatus；
Figure 12 is the explosive view of supply unit.
Embodiment
In order to more fully understand the technology contents of the present invention, technical scheme is made with reference to specific embodiment
It is further described and illustrates.
The concrete structure of the embodiment of the present invention is as shown in Figures 1 to 12.
The Modularized unmanned aircraft of the present embodiment includes fuselage device, control box 20, for shooting and by photographed data
Transmit to the filming apparatus 30 of external equipment and the supply unit 40 for being powered for unmanned vehicle.
The propeller 14 and driving propeller that fuselage device includes the shell 10 of unmanned vehicle and is located on shell 10
14 motors 13 rotated.Control box 20 is embedded at the centre of shell 10.Main control board 24, the GPS circuitry plate of unmanned vehicle
22nd, RF modules and earth magnetism circuit board 27 are fixed in control box 20.
Specifically, shell 10 is provided with four spreading arms 12 extended outward, and shell 10 is in cross, and motor 13, which is fixed on, to be prolonged
The outer end of swing arm 12, upward, propeller 14 is located on the output shaft of motor 13 and coaxial with the output shaft of motor 13 output shaft of motor 13
Rotate.Shell 10 includes the upper lid 101 and lower cover 102 to interfix.Upper lid 101 is provided with the through hole 121 for being used for accommodating motor 13.
The lower section of lower cover 102 is hinged with retractable foot stool 15.
Control box 20 is fixed in shell 10.Specifically, shell 10 is provided with the installation position 11 for being used for fixing control box 20,
Installation position 11 is provided with upper shed and under shed, and control box 20 loads in installation position 11 under shed, the top insertion of control box 20
The upper shed of installation position 11.In the present embodiment, control box 20 loads installation position 11 from the bottom up, and in other embodiments, can
Load installation position from top to bottom to be arranged to control box.
Control box 20 includes the upper casing 201 to interfix and lower casing 202.In the present embodiment, the upper shed of installation position 11 is in
Corner is starlike, and the upper casing 201 of control box 20 is also starlike in corresponding corner.The outer wall of upper casing 201 and lower casing 202 is equipped with scattered
Hot hole.Main control board 24 is fixed on lower casing 202, and RF modules are located on main control board 24, and GPS circuitry plate 22 is fixed on master
Control the top of circuit board 24 and be provided with shielding cotton 23 between the two.
Main control board 24 is provided with power switch 25.Power switch 25, which is provided with, to be used to control the break-make of power switch 25
Elastic pressuring plate 26.Elastic pressuring plate 26 is fixed on the top of power switch 25 and forms acute angle with the top surface of power switch 25.Power supply is opened
The top surface for closing 25 is provided with shift knob 251, and shift knob 251 is located at the lower section of elastic pressuring plate 26.
Upper casing 201 is provided with the driving lever 21 being rotatably connected with upper casing 201.Driving lever 21 includes main part 211 and for squeezing
The afterbody 212 of compression elasticity tabletting 26.Driving lever 21 connects with junction bearing pin rotation of the upper casing 201 in main part 211 and afterbody 212
Connect.Upper casing 201 is provided with the groove 201a for accommodating the main part 211 of driving lever 21.
When driving lever 21 is horizontal positioned, driving lever 21 is located at de-energized, and the main part 211 of driving lever 21 is placed within upper casing 201
(i.e. the main part 211 of driving lever 21 is placed in groove 201a), the afterbody 212 of driving lever 21 is away from elastic pressuring plate 26, elastic pressuring plate 26
Also do not contacted with shift knob 251, power switch 25 powers off.
Driving lever 21 from it is horizontal positioned be changed into placing vertically when, driving lever 21 is allocated to on-position, the main part 211 of driving lever 21
Expose to outside upper casing 201, the afterbody 212 of driving lever 21 pushes elastic pressuring plate 26, and elastic pressuring plate 26 is by under shift knob 251
Pressure, power switch 25 are powered.
Earth magnetism circuit board 27 is located in the main part 211 of driving lever 21, and it is used to carry out earth magnetism when in vertical position
Correction.Therefore when driving lever 21 is horizontal positioned, earth magnetism circuit board 27 also is located on horizontal plane, and earth magnetism circuit board 27 is without earth magnetism
Correction.And when driving lever 21 is placed vertically, earth magnetism circuit board 27 is on vertical plane, while power switch 25 is also powered, this
When earth magnetism circuit board 27 can be to carry out earth magnetism correction to ensure unmanned vehicle normal flight.
Filming apparatus 30 is fixed on the lower section of control box 20.Specifically, as shown in Figure 10 and Figure 11, filming apparatus 30 includes taking the photograph
Camera 36, the spindle motor of head 31 and three.Head wiring board 32 is provided with head 31, carries and is wirelessly transferred on head wiring board 32
Module.Three spindle motors are divided into Z axis motor 33, y-axis motor 34 and X-axis motor 35.Z axis motor 33 is located in head 31, Z axis motor
Down, y-axis motor 34 is fixedly connected on the output shaft of Z axis motor 33 33 output shafts by lower swing arm 37, and X-axis motor 35 passes through water
Flat arm 38 is fixedly connected on the output shaft of y-axis motor 34, and video camera 36 is fixed on the output shaft of X-axis motor 35.
Supply unit 40 is fixed on the lower section of control box 20.As shown in figure 12, supply unit 40 includes battery case 41, is located at electricity
Battery core 42 in pond box 41 and the electricity being located on the outer wall of battery case 41 show bar 43.Electricity shows that bar 43 is electrically connected with battery core 42
Connect.Supply unit 40 electrically connects with filming apparatus 30, main control board 24 and motor 13 respectively.
The technology contents set forth above that the present invention is only further illustrated with embodiment, in order to which reader is easier to understand,
But embodiments of the present invention are not represented and are only limitted to this, any technology done according to the present invention extends or recreation, is sent out by this
Bright protection.
Claims (4)
1. a kind of Modularized unmanned aircraft, including fuselage device, fuselage device includes the shell of unmanned vehicle and is located at
The motor of propeller on shell and driving propeller rotational, it is characterised in that also include being embedded at control box among shell,
For shooting and transmitting photographed data to the filming apparatus of external equipment and the dress of the power supply for being powered for unmanned vehicle
Put, the filming apparatus and supply unit are fixed on below control box, the master control electricity provided with unmanned vehicle in the control box
Road plate, supply unit electrically connect with filming apparatus, main control board and motor respectively；Shell is provided with four extensions extended outward
Arm, shell are in cross, and motor is fixed on the outer end of spreading arm, and upward, propeller is located on motor output shaft motor output shaft
And rotated coaxially with motor output shaft；The shell is provided with the installation position for being used for fixing control box, and installation position is provided with upper shed
And under shed, control box load in installation position under shed, the upper shed of the top insertion installation position of control box；Described control
Box includes the upper casing and lower casing to interfix；The upper shed of installation position is starlike in corner, and the upper casing of control box is also in and installation
The corner that the upper shed of position is corresponding is starlike；The outer wall of upper casing and lower casing is equipped with heat emission hole；The corner of the upper shed is starlike
Wedge angle alignment spreading arm center；The control box is provided with the driving lever being rotatably connected with control box, the main control board
Power switch is provided with, the power switch is provided with the elastic pressuring plate for being used for controlling power switch break-make, and driving lever includes main body
Portion and the afterbody for extruding elastic pressuring plate, driving lever are rotatably connected with control box in main part with the junction of afterbody；When dial
When bar is located at de-energized, the main part of driving lever is placed within control box, and the afterbody of driving lever breaks away from elastic pressuring plate, power switch
Electricity；When driving lever is allocated to on-position, the main part of driving lever is exposed to outside control box, and the afterbody of driving lever is by under elastic pressuring plate
Pressure, power switch are powered；When driving lever is located at de-energized, driving lever is horizontal positioned；When driving lever is allocated to on-position, driving lever
It is vertical to place；Earth magnetism circuit board is provided with the main part of the driving lever.
2. Modularized unmanned aircraft as claimed in claim 1, it is characterised in that the main control board is provided with RF moulds
Block, GPS circuitry plate is additionally provided with control box, and GPS circuitry plate is fixed on above main control board and is provided with shielding between the two
Cotton.
3. Modularized unmanned aircraft as claimed in claim 1, it is characterised in that the filming apparatus includes video camera, cloud
Platform and three spindle motors, head is interior to be provided with head wiring board, and three spindle motors are divided into Z axis motor, y-axis motor and X-axis motor, Z axis
Motor is located in head, and down, y-axis motor is fixedly connected on Z axis motor output shaft to Z axis motor output shaft by a lower swing arm
On, X-axis motor is fixedly connected on y-axis motor output shaft by a horizontal arm, and the video camera is fixed on X-axis motor output shaft
On.
4. Modularized unmanned aircraft as claimed in claim 1, it is characterised in that the supply unit includes battery case, set
Battery core in battery case and the electricity being located on battery outer box wall show bar, and the electricity shows that bar electrically connects with battery core.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510060890.XA CN104627361B (en) | 2015-02-05 | 2015-02-05 | A kind of Modularized unmanned aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510060890.XA CN104627361B (en) | 2015-02-05 | 2015-02-05 | A kind of Modularized unmanned aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104627361A CN104627361A (en) | 2015-05-20 |
| CN104627361B true CN104627361B (en) | 2018-01-05 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510060890.XA Expired - Fee Related CN104627361B (en) | 2015-02-05 | 2015-02-05 | A kind of Modularized unmanned aircraft |
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| Country | Link |
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Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107614378B (en) * | 2015-06-01 | 2021-06-25 | 深圳市大疆创新科技有限公司 | Method, apparatus and kit for assembling a mobile platform |
| WO2017070911A1 (en) * | 2015-10-30 | 2017-05-04 | 深圳市大疆创新科技有限公司 | Flight control device and unmanned aerial vehicle having same |
| CN205244760U (en) * | 2015-11-20 | 2016-05-18 | 深圳市道通智能航空技术有限公司 | Both arms cloud platform |
| CN105573333B (en) * | 2016-01-22 | 2018-05-08 | 青岛大学 | A kind of modular control method for quadrotor |
| CN105700535B (en) * | 2016-01-22 | 2018-05-08 | 青岛大学 | A kind of modular control panel for quadrotor |
| USD806606S1 (en) | 2016-02-03 | 2018-01-02 | Morrison Innovations, Llc | Nano camera drone |
| CN111591456B (en) * | 2016-09-23 | 2022-04-01 | 深圳市大疆创新科技有限公司 | Shock attenuation board and have unmanned vehicles of this shock attenuation board |
| CN206118300U (en) * | 2016-10-25 | 2017-04-19 | 深圳市大疆创新科技有限公司 | Shield assembly and unmanned vehicles |
| CN108064209B (en) * | 2017-04-26 | 2021-05-18 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN107567821A (en) * | 2017-07-27 | 2018-01-12 | 杭州电子科技大学 | A kind of tea picker |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201007964Y (en) * | 2006-11-01 | 2008-01-16 | 姜天恩 | Changeable switch |
| EP3828086A1 (en) * | 2011-09-09 | 2021-06-02 | SZ DJI Osmo Technology Co., Ltd. | Dual-axis platform for use in a small unmanned aerial vehicle and tri-axis platform for use in a small unmanned aerial vehicle |
| KR101350291B1 (en) * | 2012-04-24 | 2014-01-10 | 유콘시스템 주식회사 | Unmanned aerial vehicle system with cable connection equipment |
| CN103350752A (en) * | 2012-10-29 | 2013-10-16 | 深圳市哈博森科技有限公司 | Four-rotor aircraft |
| CN203064201U (en) * | 2012-12-28 | 2013-07-17 | 贵州斯凯威科技有限公司 | Aerial photo aircraft |
| CN203996886U (en) * | 2014-06-30 | 2014-12-10 | 上海汇联皆景信息科技有限公司 | A kind of four axle eight oars aircraft of taking photo by plane |
| CN204078068U (en) * | 2014-07-31 | 2015-01-07 | 西安非凡士机器人科技有限公司 | A kind of four-axle aircraft of overlength flying power |
| CN104401486B (en) * | 2014-11-21 | 2016-04-20 | 吉林大学 | Helios |
| CN204568055U (en) * | 2015-02-05 | 2015-08-19 | 深圳雷柏科技股份有限公司 | A kind of Modularized unmanned aircraft |
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2015
- 2015-02-05 CN CN201510060890.XA patent/CN104627361B/en not_active Expired - Fee Related
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| CN104627361A (en) | 2015-05-20 |
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Granted publication date: 20180105 Termination date: 20190205 |