CN104627361A - Modularized unmanned aerial vehicle - Google Patents
Modularized unmanned aerial vehicle Download PDFInfo
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- CN104627361A CN104627361A CN201510060890.XA CN201510060890A CN104627361A CN 104627361 A CN104627361 A CN 104627361A CN 201510060890 A CN201510060890 A CN 201510060890A CN 104627361 A CN104627361 A CN 104627361A
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- aerial vehicle
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Abstract
The invention relates to a modularized unmanned aerial vehicle. The modularized unmanned aerial vehicle comprises a vehicle body device, wherein the vehicle body device comprises a housing of an unmanned aerial vehicle, a propeller and a motor, wherein the unmanned aerial vehicle further comprises a control box, a shooting device used for performing shooting and transmitting shooting data to external equipment and a power supply device used for supplying power to the unmanned aerial vehicle, the shooting device and the power supply device are fixed below the control box, a main control circuit board of the unmanned aerial vehicle is arranged in the control box, and the power supply device is respectively electrically connected with the shooting device, the main control circuit board and the motor. Components of the unmanned aerial vehicle are divided into a plurality of independent devices, during assembly, each device can be respectively assembled and tested, and then assembled into the unmanned aerial vehicle, so that the cost is lowered, the quality of the unmanned aerial vehicle is improved; when the unmanned aerial vehicle is damaged by impaction, the damaged device can be maintained or replaced, and other un-damaged devices can be reserved, and the maintenance cost and time can be reduced.
Description
Technical field
The present invention relates to aircraft, particularly relate to a kind of Modularized unmanned aircraft.
Background technology
The fields such as current small-sized unmanned aircraft is widely applied taking photo by plane, agricultural, fire, disaster early warning, along with the maturation of technology and the reduction of cost, will have the use of increasing field.
The small-sized unmanned aircraft of commercial type, generally adopt upper and lower covers design, motor required for aircraft, flight indicator lamp, flight control system, gps system, magnetic system etc. be all put in aircraft upper and lower covers, production and assembly are very difficult, be not easy to maintenance.Aircraft is when high-speed flight, and the easy misoperation of manipulator, aircraft knocks building or sets greatly in high-altitude, even direct from falling from high altitude, thus causes aircraft to be damaged, and cannot keep in repair.Manipulator can only buy new product, but the current price of aircraft all costly, is a no small loss for consumers.
Summary of the invention
The object of the invention is to the defect for overcoming prior art, and a kind of Modularized unmanned aircraft is provided, to reduce maintenance and assembly cost.
For achieving the above object, the present invention is by the following technical solutions:
A kind of Modularized unmanned aircraft, comprises fuselage device, and fuselage device comprises the shell of unmanned vehicle and the motor of the screw propeller be located on shell and driving propeller rotational; Unmanned vehicle also comprises and is embedded at control capsule in the middle of shell, for taking and the filming apparatus and being used for photographed data the being transferred to external device supply unit of powering for unmanned vehicle, filming apparatus and supply unit are fixed below control capsule, be provided with the main control board of unmanned vehicle in control capsule, supply unit is electrically connected with filming apparatus, main control board and motor respectively.
Further, shell is provided with four spreading arms toward extensions, and shell is cross, and motor is fixed on the outer end of spreading arm, motor output shaft upward, screw propeller to be located on motor output shaft and with motor output shaft coaxial rotation.
Further, shell is provided with the installation position for fixing control capsule, and installation position is provided with upper shed and under shed, and control capsule loads in installation position under shed, the upper shed of the insertion installation position, top of control capsule.
Further, main control board is provided with RF module, is also provided with GPS circuit card in control capsule, and GPS circuit card is fixed on above main control board and to be provided with shielding between the two cotton.
Further, control capsule is provided with the driving lever of rotarying connection with control capsule, main control board is provided with source switch, source switch is provided with the elastic pressuring plate for controlling source switch break-make, driving lever comprises main part and the afterbody for extruding elastic pressuring plate, and driving lever is rotaryed connection with the junction of afterbody at main part with control capsule.
Further, when driving lever is positioned at de-energized, the main part of driving lever is placed within control capsule, the afterbody of driving lever away from elastic pressuring plate, source switch power-off; When driving lever is allocated to on-position, the main part of driving lever exposes to outside control capsule, and elastic pressuring plate presses down by the afterbody of driving lever, and source switch is energized.
Further, when driving lever is positioned at de-energized, driving lever horizontal positioned; When driving lever is allocated to on-position, driving lever is vertically placed.
Further, earth magnetism circuit card is provided with in the main part of driving lever.
Further, filming apparatus comprises pick up camera, The Cloud Terrace and three spindle motors, The Cloud Terrace wiring board is provided with in The Cloud Terrace, three spindle motors are divided into Z axis motor, y-axis motor and X-axis motor, Z axis motor is located in The Cloud Terrace, and down, y-axis motor is fixedly connected on Z axis motor output shaft by a lower swing arm Z axis motor output shaft, X-axis motor is fixedly connected on y-axis motor output shaft by a horizontal arm, and pick up camera is fixed on X-axis motor output shaft.
Further, supply unit comprises battery case, is located at the battery core in battery case and is located at the electricity show bar on battery case outer wall, and electricity show bar is electrically connected with battery core.
The present invention's beneficial effect is compared with prior art:
The parts of unmanned vehicle are divided into independently several devices by the present invention, and when assembling, can distinguish assembling test by first each device, and then be assembled into unmanned vehicle, cost is reduced, and the quality of aircraft also gets a promotion; And when unmanned vehicle is subject to clashing into impaired, can carry out keeping in repair or changing for impaired device, other do not have impaired device to retain, and maintenance cost and time are all reduced.
Accompanying drawing explanation
Fig. 1 is the exploded view of unmanned vehicle;
Fig. 2 is the exploded view of fuselage device;
Fig. 3 is the exploded view of control capsule;
Fig. 4 is main control board block diagram;
Fig. 5 is the sectional arrangement drawing (driving lever closes) of control capsule;
Fig. 6 is the sectional arrangement drawing (driving lever opening procedure) of control capsule;
Fig. 7 is the sectional arrangement drawing (driving lever is opened completely) of control capsule;
Fig. 8 is the partial enlarged drawing of Fig. 7;
Fig. 9 is the birds-eye view of control capsule;
Figure 10 is the exploded view of filming apparatus;
Figure 11 is the assembling stereogram of filming apparatus;
Figure 12 is the exploded view of supply unit.
Detailed description of the invention
In order to more fully understand technology contents of the present invention, below in conjunction with specific embodiment, technical scheme of the present invention being described further and being illustrated.
The concrete structure of the embodiment of the present invention as shown in Figures 1 to 12.
The Modularized unmanned aircraft of the present embodiment comprise fuselage device, control capsule 20, for taking and the filming apparatus 30 and being used for photographed data the being transferred to external device supply unit 40 of powering for unmanned vehicle.
Fuselage device comprises the shell 10 of unmanned vehicle and the motor 13 of the screw propeller 14 be located on shell 10 and the rotation of driving screw propeller 14.Control capsule 20 is embedded at the centre of shell 10.The main control board 24 of unmanned vehicle, GPS circuit card 22, RF module and earth magnetism circuit card 27 are fixed in control capsule 20.
Particularly, shell 10 is provided with four spreading arms 12 toward extensions, and shell 10 is in cross, and motor 13 is fixed on the outer end of spreading arm 12, motor 13 output shaft upward, screw propeller 14 to be located on motor 13 output shaft and with motor 13 output shaft coaxial rotation.Shell 10 comprises the upper cover 101 and lower cover 102 that interfix.Upper cover 101 is provided with the through hole 121 for holding motor 13.Being hinged with below lower cover 102 can the foot rest 15 of folding.
Control capsule 20 is fixed in shell 10.Particularly, shell 10 is provided with the installation position 11 for fixing control capsule 20, and installation position 11 is provided with upper shed and under shed, and control capsule 20 loads in installation position 11 under shed, the upper shed of the insertion installation position, top 11 of control capsule 20.In the present embodiment, control capsule 20 loads installation position 11 from the bottom up, and in other embodiments, can be arranged to control capsule and load installation position from top to bottom.
Control capsule 20 comprises the upper casing 201 and lower casing 202 that interfix.In the present embodiment, the upper shed of installation position 11 is that corner is starlike, and the corner of the upper casing 201 of control capsule 20 also in corresponding is starlike.Upper casing 201 is equipped with louvre with the outer wall of lower casing 202.Main control board 24 is fixed on lower casing 202, and RF module is located on main control board 24, and GPS circuit card 22 to be fixed on above main control board 24 and to be provided with shielding cotton 23 between the two.
Main control board 24 is provided with source switch 25.Source switch 25 is provided with the elastic pressuring plate 26 for controlling source switch 25 break-make.Elastic pressuring plate 26 is fixed on above source switch 25 and with the end face of source switch 25 and forms acute angle.The end face of source switch 25 is provided with shift knob 251, and shift knob 251 is positioned at below elastic pressuring plate 26.
Upper casing 201 is provided with the driving lever 21 of rotarying connection with upper casing 201.Driving lever 21 comprises main part 211 and the afterbody 212 for extruding elastic pressuring plate 26.Driving lever 21 is rotaryed connection with the junction bearing pin of afterbody 212 at main part 211 with upper casing 201.Upper casing 201 is provided with the groove 201a holding driving lever 21 main part 211.
During driving lever 21 horizontal positioned, driving lever 21 is positioned at de-energized, the main part 211 of driving lever 21 is placed in (namely the main part 211 of driving lever 21 is placed in groove 201a) within upper casing 201, the afterbody 212 of driving lever 21 is away from elastic pressuring plate 26, elastic pressuring plate 26 does not also contact with shift knob 251, source switch 25 power-off.
Driving lever 21 from horizontal positioned become vertically place time, driving lever 21 is allocated to on-position, and the main part 211 of driving lever 21 exposes to outside upper casing 201, and elastic pressuring plate 26 presses down by the afterbody 212 of driving lever 21, and shift knob 251 presses down by elastic pressuring plate 26, source switch 25 is energized.
Earth magnetism circuit card 27 is located in the main part 211 of driving lever 21, and it is for correcting earth magnetism when being in vertical position.Therefore when driving lever 21 horizontal positioned, earth magnetism circuit card 27 is also positioned on horizontal surface, and earth magnetism circuit card 27 does not carry out earth magnetism correction.And when driving lever 21 is vertically placed, earth magnetism circuit card 27 is on vertical plane, source switch 25 has also been energized simultaneously, and now earth magnetism circuit card 27 just can carry out earth magnetism correction to ensure unmanned vehicle normal flight.
Filming apparatus 30 is fixed on below control capsule 20.Particularly, as shown in Figure 10 and Figure 11, filming apparatus 30 comprises pick up camera 36, The Cloud Terrace 31 and three spindle motors.The Cloud Terrace wiring board 32 is provided with, with wireless transport module on The Cloud Terrace wiring board 32 in The Cloud Terrace 31.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 The Cloud Terrace 31, Z axis motor 33 output shaft down, y-axis motor 34 is fixedly connected on Z axis motor 33 output shaft by lower swing arm 37, and X-axis motor 35 is fixedly connected on y-axis motor 34 output shaft by horizontal arm 38, and pick up camera 36 is fixed on X-axis motor 35 output shaft.
Supply unit 40 is fixed on below control capsule 20.As shown in figure 12, the supply unit 40 electricity show bar 43 that comprises battery case 41, be located at the battery core 42 in battery case 41 and be located on battery case 41 outer wall.Electricity show bar 43 is electrically connected with battery core 42.Supply unit 40 is electrically connected with filming apparatus 30, main control board 24 and motor 13 respectively.
More than state only with embodiment to further illustrate technology contents of the present invention so that reader is easier to understand, but does not represent embodiments of the present invention and be only limitted to this, any technology done according to the present invention extends or recreation, all by protection of the present invention.
Claims (10)
1. a Modularized unmanned aircraft, comprise fuselage device, fuselage device comprises the shell of unmanned vehicle and the motor of the screw propeller be located on shell and driving propeller rotational, it is characterized in that, also comprise the control capsule be embedded in the middle of shell, for taking and the filming apparatus and being used for photographed data the being transferred to external device supply unit of powering for unmanned vehicle, described filming apparatus and supply unit are fixed on below control capsule, the main control board of unmanned vehicle is provided with in described control capsule, supply unit respectively with filming apparatus, main control board and motor electrical connection.
2. Modularized unmanned aircraft as claimed in claim 1, is characterized in that, described shell is provided with four spreading arms toward extension, shell is cross, motor is fixed on the outer end of spreading arm, motor output shaft upward, screw propeller to be located on motor output shaft and with motor output shaft coaxial rotation.
3. Modularized unmanned aircraft as claimed in claim 1, it is characterized in that, described shell is provided with the installation position for fixing control capsule, and installation position is provided with upper shed and under shed, control capsule loads in installation position under shed, the upper shed of the insertion installation position, top of control capsule.
4. Modularized unmanned aircraft as claimed in claim 1, it is characterized in that, described main control board is provided with RF module, is also provided with GPS circuit card in control capsule, and GPS circuit card is fixed on above main control board and to be provided with shielding between the two cotton.
5. Modularized unmanned aircraft as claimed in claim 1, it is characterized in that, described control capsule is provided with the driving lever of rotarying connection with control capsule, described main control board is provided with source switch, described source switch is provided with the elastic pressuring plate for controlling source switch break-make, driving lever comprises main part and the afterbody for extruding elastic pressuring plate, and driving lever is rotaryed connection with the junction of afterbody at main part with control capsule.
6. Modularized unmanned aircraft as claimed in claim 5, it is characterized in that, when driving lever is positioned at de-energized, the main part of driving lever is placed within control capsule, the afterbody of driving lever away from elastic pressuring plate, source switch power-off; When driving lever is allocated to on-position, the main part of driving lever exposes to outside control capsule, and elastic pressuring plate presses down by the afterbody of driving lever, and source switch is energized.
7. Modularized unmanned aircraft as claimed in claim 6, is characterized in that, when driving lever is positioned at de-energized, and driving lever horizontal positioned; When driving lever is allocated to on-position, driving lever is vertically placed.
8. Modularized unmanned aircraft as claimed in claim 6, is characterized in that, be provided with earth magnetism circuit card in the main part of described driving lever.
9. Modularized unmanned aircraft as claimed in claim 1, it is characterized in that, described filming apparatus comprises pick up camera, The Cloud Terrace and three spindle motors, The Cloud Terrace wiring board is provided with in The Cloud Terrace, three spindle motors are divided into Z axis motor, y-axis motor and X-axis motor, Z axis motor is located in The Cloud Terrace, Z axis motor output shaft down, y-axis motor is fixedly connected on Z axis motor output shaft by a lower swing arm, X-axis motor is fixedly connected on y-axis motor output shaft by a horizontal arm, and described pick up camera is fixed on X-axis motor output shaft.
10. Modularized unmanned aircraft as claimed in claim 1, it is characterized in that, described supply unit comprises battery case, is located at the battery core in battery case and is located at the electricity show bar on battery case outer wall, and described electricity show bar is electrically connected 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 |
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| CN104627361A true CN104627361A (en) | 2015-05-20 |
| CN104627361B CN104627361B (en) | 2018-01-05 |
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| CN201510060890.XA Expired - Fee Related CN104627361B (en) | 2015-02-05 | 2015-02-05 | A kind of Modularized unmanned aircraft |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105573333A (en) * | 2016-01-22 | 2016-05-11 | 青岛大学 | Modular control method for four-rotor aircraft |
| CN105700535A (en) * | 2016-01-22 | 2016-06-22 | 青岛大学 | Modular type control panel for four-rotor aircraft |
| WO2017084471A1 (en) * | 2015-11-20 | 2017-05-26 | 深圳市道通智能航空技术有限公司 | Dual-arm camera mount |
| CN106794903A (en) * | 2016-09-23 | 2017-05-31 | 深圳市大疆创新科技有限公司 | Vibration damper plate and the unmanned vehicle with the vibration damper plate |
| CN107000828A (en) * | 2015-10-30 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Flight control assemblies and the unmanned plane with the flight control assemblies |
| USD806606S1 (en) | 2016-02-03 | 2018-01-02 | Morrison Innovations, Llc | Nano camera drone |
| CN107567821A (en) * | 2017-07-27 | 2018-01-12 | 杭州电子科技大学 | A kind of tea picker |
| CN107614378A (en) * | 2015-06-01 | 2018-01-19 | 深圳市大疆创新科技有限公司 | For assembling the method, equipment and external member of mobile platform |
| WO2018076468A1 (en) * | 2016-10-25 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Shielding apparatus and unmanned aerial vehicle |
| WO2018195786A1 (en) * | 2017-04-26 | 2018-11-01 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201007964Y (en) * | 2006-11-01 | 2008-01-16 | 姜天恩 | Changeable switch |
| CN202392374U (en) * | 2011-09-09 | 2012-08-22 | 深圳市大疆创新科技有限公司 | Gyroscopic dynamic self-balancing pan/tilt/zoom (PTZ) |
| CN203064201U (en) * | 2012-12-28 | 2013-07-17 | 贵州斯凯威科技有限公司 | Aerial photo aircraft |
| CN103350752A (en) * | 2012-10-29 | 2013-10-16 | 深圳市哈博森科技有限公司 | Four-rotor aircraft |
| KR20130119633A (en) * | 2012-04-24 | 2013-11-01 | 유콘시스템 주식회사 | Unmanned aerial vehicle system with cable connection equipment |
| 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 |
| CN104401486A (en) * | 2014-11-21 | 2015-03-11 | 吉林大学 | Solar aircraft |
| 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 |
-
2015
- 2015-02-05 CN CN201510060890.XA patent/CN104627361B/en not_active Expired - Fee Related
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201007964Y (en) * | 2006-11-01 | 2008-01-16 | 姜天恩 | Changeable switch |
| CN202392374U (en) * | 2011-09-09 | 2012-08-22 | 深圳市大疆创新科技有限公司 | Gyroscopic dynamic self-balancing pan/tilt/zoom (PTZ) |
| EP2759480A1 (en) * | 2011-09-09 | 2014-07-30 | SZ DJI Technology Co., Ltd. | Dual-axis ball head for use in small unmanned aerial vehicle and triple-axis ball head for use in small unmanned aerial vehicle |
| KR20130119633A (en) * | 2012-04-24 | 2013-11-01 | 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 |
| CN104401486A (en) * | 2014-11-21 | 2015-03-11 | 吉林大学 | Solar aircraft |
| 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 |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107614378A (en) * | 2015-06-01 | 2018-01-19 | 深圳市大疆创新科技有限公司 | For assembling the method, equipment and external member of mobile platform |
| 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 |
| US10661900B2 (en) | 2015-06-01 | 2020-05-26 | SZ DJI Technology Co., Ltd. | Method, apparatus, and kit for assembling a mobile platform |
| CN107000828B (en) * | 2015-10-30 | 2019-06-18 | 深圳市大疆创新科技有限公司 | Flight control assemblies and unmanned plane with the flight control assemblies |
| US11142313B2 (en) | 2015-10-30 | 2021-10-12 | SZ DJI Technology Co., Ltd. | Flight control device and unmanned aerial vehicle having the same |
| CN107000828A (en) * | 2015-10-30 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Flight control assemblies and the unmanned plane with the flight control assemblies |
| WO2017084471A1 (en) * | 2015-11-20 | 2017-05-26 | 深圳市道通智能航空技术有限公司 | Dual-arm camera mount |
| CN105573333B (en) * | 2016-01-22 | 2018-05-08 | 青岛大学 | A kind of modular control method for quadrotor |
| CN105700535A (en) * | 2016-01-22 | 2016-06-22 | 青岛大学 | Modular type control panel for four-rotor aircraft |
| CN105573333A (en) * | 2016-01-22 | 2016-05-11 | 青岛大学 | Modular control method for four-rotor aircraft |
| 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 |
| CN106794903A (en) * | 2016-09-23 | 2017-05-31 | 深圳市大疆创新科技有限公司 | Vibration damper plate and the unmanned vehicle with the vibration damper plate |
| CN111591456A (en) * | 2016-09-23 | 2020-08-28 | 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 |
| CN109644581B (en) * | 2016-10-25 | 2020-05-22 | 深圳市大疆创新科技有限公司 | Shielding device and unmanned vehicles |
| CN109644581A (en) * | 2016-10-25 | 2019-04-16 | 深圳市大疆创新科技有限公司 | Screening arrangement and unmanned vehicle |
| WO2018076468A1 (en) * | 2016-10-25 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Shielding apparatus and unmanned aerial vehicle |
| WO2018195786A1 (en) * | 2017-04-26 | 2018-11-01 | 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 |
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