CN208429235U - It is a kind of can VTOL and long continuation of the journey unmanned plane - Google Patents
It is a kind of can VTOL and long continuation of the journey unmanned plane Download PDFInfo
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- CN208429235U CN208429235U CN201821102803.8U CN201821102803U CN208429235U CN 208429235 U CN208429235 U CN 208429235U CN 201821102803 U CN201821102803 U CN 201821102803U CN 208429235 U CN208429235 U CN 208429235U
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model relates to air vehicle technique fields, more particularly to it is a kind of can VTOL and long continuation of the journey unmanned plane, including fuselage, wing and tail, two wings are symmetrically distributed in the two sides of front end in fuselage, two empennages are symmetrically distributed in the two sides of back body, form accommodating chamber in the fuselage；It is characterized in that, being mounted on vertical lifting mechanism and parallel moving mechanism on each wing；The front end of the fuselage has been removably secured infrared rotation high-definition camera, and the upper end of the fuselage is provided with solar panel；Controller, battery and signal transceiver are provided in the accommodating chamber, the controller is connected with battery, infrared rotation high-definition camera, signal transceiver, vertical lifting mechanism and parallel moving mechanism respectively, and the battery is connected with solar panel.The utility model structure is simple, easy to use and practical, increases the ability of unmanned plane vertical lift and effectively extends the cruising ability of product.
Description
Technical field
The utility model relates to air vehicle technique fields, and in particular to one kind can VTOL and the long unmanned plane continued a journey.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.With someone
It drives an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses application field,
Can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane industrial application are nothings
It is man-machine really just to have needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal,
The application in infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field is monitored, greatly
The purposes of unmanned plane itself is expanded, developed country also in actively extension industrial application and develops unmanned air vehicle technique.
Unmanned plane has very important effect in mapping, can be with airborne sensory equipment, such as high resolution CCD number
Camera, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain information, with computer to image information into
Row processing, and image is fabricated to according to certain required precision.For the total demand for adapting to town development, comprehensive geographic, money are provided
Source information.Correctly, completely information material be science decision basis.Unmanned plane can not achieve free hang down in mapping at present
Straight landing, it is complicated for operation, it is inconvenient to use.
Summary of the invention
The purpose of the utility model is to overcome defects in the prior art, and providing one kind can VTOL and long continuation of the journey
Unmanned plane, structure is simple, easy to use and practical, increases the ability of unmanned plane vertical lift and effectively extends production
The cruising ability of product.
In order to achieve the above object, the technical solution adopted in the utility model is:
The a kind of of the utility model can VTOL and the long unmanned plane continued a journey, including fuselage, wing and tail, two machines
The wing is symmetrically distributed in the two sides of front end in fuselage, and two empennages are symmetrically distributed in the two sides of back body, are formed in the fuselage
Accommodating chamber；It is characterized in that, being mounted on vertical lifting mechanism and parallel moving mechanism on each wing；The fuselage
Front end has been removably secured infrared rotation high-definition camera, and the upper end of the fuselage is provided with solar panel；The appearance
Receive it is intracavitary be provided with controller, battery and signal transceiver, the controller respectively with battery, infrared rotation high-definition camera
Head, signal transceiver, vertical lifting mechanism are connected with parallel moving mechanism, and the battery is connected with solar panel
It connects.
Further, the vertical lifting mechanism includes support rod, lifting motor and elevating screw, and the support rod hangs down
It is directly fixed on the bottom of wing, the shape of the support rod is concave character type, is fixed on the anterior-posterior horizontal end face of the support rod
The output axis connection of lifting motor, the elevating screw and lifting motor, the lifting motor is connected with controller, described
Elevating screw is arranged in parallel with wing.
Further, the parallel moving mechanism includes support base, traversing motor and traversing propeller, and the support base hangs down
It is directly fixed on the front end of wing, the traversing motor is fixed in the preceding vertical end face of support base, the traversing propeller and cross
The output axis connection of motor is moved, the traversing motor is connected with controller, and the traversing propeller is mutually perpendicular to set with wing
It sets.
Further, temperature sensor and processor are additionally provided in the accommodating chamber, the temperature sensor is at
Reason device is connected with controller.
Further, radiator fan is additionally provided in the accommodating chamber, the radiator fan is connected with controller.
Compared with prior art, the positive beneficial effect of the utility model is:
1, the utility model passes through the vertical lifting mechanism and parallel moving mechanism being arranged on wing, may be implemented vertical
It goes up and down and moves in parallel.
2, the utility model it is a kind of can VTOL and long continuation of the journey unmanned plane, pass through four elevating screws of setting
Paddle is conducive to unmanned plane vertical lift, while increasing the ability of unmanned plane vertical lift, unmanned plane raising speed in vertical direction
Degree faster, improves mapping efficiency.
3, the upper end of fuselage is equipped with solar panel, can carry out electricity supplement during the work time, effectively extend
The cruising ability of product.
4, the front end of fuselage has been removably secured infrared rotation high-definition camera, and the camera signals acquisition capacity is strong,
High-precision picture can be obtained, the precision of mapping is improved.
Detailed description of the invention
Fig. 1 be the utility model it is a kind of can VTOL and long continuation of the journey unmanned plane structural schematic diagram；
Fig. 2 be the utility model it is a kind of can VTOL and long continuation of the journey unmanned plane control principle drawing.
Meaning representated by serial number in figure are as follows: 1. fuselages, 2. wings, 3. support rods, 4. elevating screws, 5. lifting electricity
Machine, 6. support bases, 7. traversing propellers, 8. traversing motors, 9. empennages, 10. infrared rotation high-definition cameras, 11. solar-electricities
Pond plate, 12. batteries, 13. controllers, 14. processors, 15. temperature sensors, 16. signal transceivers, 17. radiator fans.
Specific embodiment
Embodiment one, as shown in Figure 1, a kind of can VTOL and the long unmanned plane continued a journey, including fuselage 1, wing 2 and tail
The wing 9, two wings 2 are symmetrically distributed in the two sides of front end in fuselage 1, and two empennages 9 are symmetrically distributed in the two sides of 1 rear end of fuselage,
Wing 2 and empennage 9 play the role of balancing fuselage, form accommodating chamber in the fuselage 1；It is mounted on each wing 2
Vertical lifting mechanism and parallel moving mechanism, the vertical lifting mechanism can be realized the vertical lift of unmanned plane, move in parallel
Mechanism can be realized moving in parallel for unmanned plane；The front end of the fuselage 1 is removably inlaid with infrared rotation high-definition camera
10, easy to disassemble, infrared rotation high-definition camera 10 is used to shoot high definition picture, and the upper end of the fuselage 1 is provided with solar energy
Solar panel 11, solar panel 11 absorb sunlight, convert solar energy into electrical energy；Controller is provided in the accommodating chamber
13, battery 12 and signal transceiver 16, the controller 13 respectively with battery 12, infrared rotation high-definition camera 10, letter
Number transceiver 16, vertical lifting mechanism are connected with parallel moving mechanism, and the signal transceiver 16 is for sending and receiving letter
Number, it is preferable that the model SPC-STW-26A1 that the controller 13 uses, the model SD-8P that signal transceiver 16 uses,
The battery 12 is connected with solar panel 11, and power storage is entire in battery 12 by solar panel 11
Equipment power supply, extends the working time of integral device, energy conservation and environmental protection using solar panel 11.
Further, the vertical lifting mechanism includes support rod 3, lifting motor 5 and elevating screw 4, elevating screws
Paddle 4 is used to go up and down, and lifting motor 5 provides power, and the support rod 3 is vertically fixed on the bottom of wing 2, and support rod 3 plays branch
Support effect, the shape of the support rod 3 are concave character type, are fixed with lifting motor 5 on the anterior-posterior horizontal end face of the support rod 3,
The output axis connection of the elevating screw 4 and lifting motor 5, the lifting motor 5 are connected with controller 13, the lifting
Propeller 4 and wing 2 are arranged in parallel.
As another embodiment, the support rod 3 is welded to connect fastening, leakproofness with wing 2 by being welded and fixed
By force；The lifting motor 5 is bolted with support rod 3, and the lifting motor 5 is bolted with elevating screw 4,
It is bolted easy to use, easy to disassemble, 4 rotates effe of elevating screw is good.
Further, the parallel moving mechanism includes support base 6, traversing motor 8 and traversing propeller 7, traversing spiral
Paddle 7 is used to transverse shifting, and traversing motor 8 provides power, and the support base 6 is vertically fixed on the front end of wing 2, and support base 6 rises
To supporting role, the traversing motor 8 is fixed in the preceding vertical end face of support base 6, the traversing propeller 7 and traversing motor
8 output axis connection, the traversing motor 8 are connected with controller 13, and the traversing propeller 7 is mutually perpendicular to set with wing 2
It sets.
As another embodiment, the support base 6 is welded to connect fastening, leakproofness with wing 2 by being welded and fixed
By force；The traversing motor 8 is bolted with support base 6, and the traversing motor 8 is bolted with traversing propeller 7,
It is bolted easy to use, easy to disassemble, traversing 7 rotates effe of propeller is good.
In addition to above structure, this can VTOL and long continuation of the journey unmanned plane accommodating chamber in be additionally provided with temperature sensor
15, processor 14 and radiator fan 17；The temperature sensor 15 is connected by processor 14 with controller 13, temperature sensing
Temperature when device 15 works for real-time detection unmanned plane in accommodating chamber, the model PT100 that temperature sensor 15 uses here,
Processor 14 sends controller 13 to for the analog signal of temperature sensor 15 to be converted to digital signal, here processor 14
The model MT6516 used；The radiator fan 17 is connected with controller 13, and radiator fan 17 is conducive to unmanned plane work
As when the heat that generates distribute.
Specifically, the wing 2 and empennage 9 are fixed on fuselage by welding manner；The controller 13, processor
14, temperature sensor 15, radiator fan 17, solar panel 11 and signal transceiver 16 pass through the receiving of screw and fuselage
Cavity wall is fixed；The battery 12 is buckled on the card slot in 1 accommodating chamber of fuselage.
Working principle is as follows:
As shown in Fig. 2, operator sends control signal by remote control, signal transceiver 16 receives control letter
Number, under the action of controller 13, lifting motor 5 and traversing motor 8 drive elevating screw 4 and traversing propeller 7 to rotate, from
And realize can VTOL and long continuation of the journey unmanned plane vertically move and transverse shifting, when being surveyed and drawn, infrared rotation is high
The image information of acquisition is transferred to controller 13 and handled by clear camera 10, is then transferred to control by signal transceiver 16
End, when temperature sensor 15 detect can the temperature of unmanned plane of VTOL and long continuation of the journey be more than preset temperature when, radiation air
Fan 17 will start automatically, carry out radiating treatment, highly-safe.
The above-mentioned description to embodiment is for that can understand and apply this practical convenient for those skilled in the art
It is novel.Person skilled in the art obviously easily can make various modifications to these embodiments, and illustrating herein
General Principle be applied in other embodiments without having to go through creative labor.Therefore, those skilled in the art are according to this
The announcement of utility model, does not depart from improvement that the utility model scope is made and modification all should be in the protection of the utility model
Within the scope of.
Claims (5)
1. one kind can VTOL and long continuation of the journey unmanned plane, including fuselage, wing and tail, two wings are symmetrically distributed in machine
The two sides of front end in body, two empennages are symmetrically distributed in the two sides of back body, form accommodating chamber in the fuselage；Its feature exists
In being mounted on vertical lifting mechanism and parallel moving mechanism on each wing；The front end of the fuselage is removably solid
Surely there is infrared rotation high-definition camera, the upper end of the fuselage is provided with solar panel；Control is provided in the accommodating chamber
Device, battery and signal transceiver processed, the controller respectively with battery, infrared rotation high-definition camera, signal transceiver,
Vertical lifting mechanism is connected with parallel moving mechanism, and the battery is connected with solar panel.
2. it is according to claim 1 can VTOL and long continuation of the journey unmanned plane, which is characterized in that the vertical conveyor
Structure includes support rod, lifting motor and elevating screw, and the support rod is vertically fixed on the bottom of wing, the support rod
Shape is concave character type, and lifting motor, the elevating screw and lifting electricity are fixed on the anterior-posterior horizontal end face of the support rod
The output axis connection of machine, the lifting motor are connected with controller, and the elevating screw and wing are arranged in parallel.
3. it is according to claim 1 can VTOL and long continuation of the journey unmanned plane, which is characterized in that it is described to move in parallel machine
Structure includes support base, traversing motor and traversing propeller, and the support base is vertically fixed on the front end of wing, the traversing motor
It is fixed in the preceding vertical end face of support base, the output axis connection of the traversing propeller and traversing motor, the traversing motor
It is connected with controller, the traversing propeller is arranged in a mutually vertical manner with wing.
4. it is according to claim 1 can VTOL and long continuation of the journey unmanned plane, which is characterized in that in the accommodating chamber also
It is provided with temperature sensor and processor, the temperature sensor is connected by processor with controller.
5. it is according to claim 1 can VTOL and long continuation of the journey unmanned plane, which is characterized in that in the accommodating chamber also
It is provided with radiator fan, the radiator fan is connected with controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821102803.8U CN208429235U (en) | 2018-07-12 | 2018-07-12 | It is a kind of can VTOL and long continuation of the journey unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821102803.8U CN208429235U (en) | 2018-07-12 | 2018-07-12 | It is a kind of can VTOL and long continuation of the journey unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN208429235U true CN208429235U (en) | 2019-01-25 |
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| CN201821102803.8U Active CN208429235U (en) | 2018-07-12 | 2018-07-12 | It is a kind of can VTOL and long continuation of the journey unmanned plane |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2726391C1 (en) * | 2019-11-22 | 2020-07-13 | Федор Александрович Рябков | Aircraft |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| CN112407310A (en) * | 2020-11-03 | 2021-02-26 | 国网浙江省电力有限公司衢州供电公司 | Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof |
| CN113148188A (en) * | 2021-06-10 | 2021-07-23 | 宁波阿瑞斯自动化技术有限公司 | Dual-power vertical take-off and landing fixed-wing unmanned aerial vehicle |
-
2018
- 2018-07-12 CN CN201821102803.8U patent/CN208429235U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2726391C1 (en) * | 2019-11-22 | 2020-07-13 | Федор Александрович Рябков | Aircraft |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| CN112027075B (en) * | 2020-09-15 | 2022-04-29 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| CN112407310A (en) * | 2020-11-03 | 2021-02-26 | 国网浙江省电力有限公司衢州供电公司 | Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof |
| CN113148188A (en) * | 2021-06-10 | 2021-07-23 | 宁波阿瑞斯自动化技术有限公司 | Dual-power vertical take-off and landing fixed-wing unmanned aerial vehicle |
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