CN206437208U - The high unmanned plane steadily monitored can be determined - Google Patents
The high unmanned plane steadily monitored can be determined Download PDFInfo
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- CN206437208U CN206437208U CN201621041588.6U CN201621041588U CN206437208U CN 206437208 U CN206437208 U CN 206437208U CN 201621041588 U CN201621041588 U CN 201621041588U CN 206437208 U CN206437208 U CN 206437208U
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- fuselage
- unmanned plane
- high unmanned
- monitored
- protecting frame
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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
Determine the high unmanned plane steadily monitored the utility model discloses a kind of, including fuselage, the side of the fuselage is circumferentially uniformly provided with four elastic links, the end of elastic link is provided with circular protecting frame, the internal engagement of protecting frame is provided with mounting bracket, rotor motor is installed in the middle part of mounting bracket, the output shaft of rotor motor is provided with rotor, the reverse side of fuselage, which coordinates, is provided with photovoltaic solar cell plate, the inside of fuselage is additionally provided with the battery for being powered to device, the positive outer ring of fuselage is provided with multiple support feets, the positive Middle face of fuselage is provided with fillet camera, the front of fuselage further respectively has altimeter and storage device, the outer ring of protecting frame is additionally provided with multiple LED lamp beads.The utility model drop resistant ability is good, and monitoring effect is good, is highly susceptible to control, and observation, and long operational time are easy in ground.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, specifically a kind of to determine the high unmanned plane steadily monitored.
Background technology
With the development of China's science and technology building, unmanned plane has been obtained extensively at transformer, circuit and agricultural business aspect
Application.Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.It is civilian
Aspect, unmanned plane+sector application is that unmanned plane has really just been needed；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, calamity
Hardly possible rescue, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture are romantic
Etc. field application, greatly expanded the purposes of unmanned plane in itself, developed country is also in actively extension sector application and hair
Open up unmanned air vehicle technique.Existing investigation of taking photo by plane has drop resistant ability with unmanned plane, and monitoring effect is not good, and height is not easily-controllable
System, ground is difficult observation, and the shorter deficiency of run time, hinders the application and development of unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of calmly high unmanned plane steadily monitored, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the utility model provides following technical scheme：
The high unmanned plane steadily monitored, including fuselage can be determined, the side of the fuselage is circumferentially uniformly provided with four elasticity even
Bar, the end of elastic link is provided with circular protecting frame, and the internal engagement of the protecting frame is provided with mounting bracket, mounting bracket
Middle part rotor motor is installed, the output shaft of rotor motor is provided with rotor, and the reverse side of the fuselage coordinates provided with photovoltaic too
Positive energy cell panel, the inside of fuselage is additionally provided with the battery for being powered to device, and battery is automatically controlled by solar charging
Device processed is electrically connected with photovoltaic solar cell plate, and the positive outer ring of the fuselage is provided with multiple support feets, and the fuselage is just
Middle face is provided with fillet camera, and the front of the fuselage further respectively has altimeter and storage device, the storage device and
Fillet camera is electrically connected with, and the outer ring of the protecting frame is additionally provided with multiple LED lamp beads.
It is used as further program of the utility model：The fuselage is disc-shaped structure.
It is used as further program of the utility model：Each described protecting frame and fuselage are in the same plane.
It is used as further program of the utility model：The mounting bracket is cross bracket.
It is used as further program of the utility model：The support feet is made up of elastic light metal material, and support feet is provided with 4
It is individual, and support feet and connecting rod are to be staggered.
It is used as further program of the utility model：The height is calculated as radio altimeter or ultrasonic height meter.
It is used as further program of the utility model：The storage device is provided with external equipment jack.
It is used as further program of the utility model：The LED lamp bead is provided with 6~8, and LED lamp bead is imaged with fillet
Head is located at the same side.
Compared with prior art, the beneficial effects of the utility model are：By being uniformly arranged four rotors in fuselage outer side
Motor, operation stability is higher, and rotor and rotor motor can be protected by protecting frame, lifts its drop resistant ability, passes through
Control LED lamp bead light, be easy to operator's night observe the running status of unmanned plane, by elastic link connect protecting frame with
Fuselage, the stability of further lifting device, stable support when can be landed by support feet to device passes through altimeter
The height of unmanned plane can be detected, it is convenient to carry out fixed high control, monitored picture can be shot by fillet camera, and store
In storage device, ground staff is facilitated to be copied, in addition, can also be stored up by photovoltaic solar cell plate to battery
Can, energy-conserving and environment-protective can extend the flight time of unmanned plane.To sum up, the unmanned plane drop resistant ability is good, and monitoring effect is good, and height is easily
In control, observation, and long operational time are easy in ground.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the reverse structure schematic of the utility model middle fuselage.
In figure：1-LED lamp beads, 2- protecting frames, 3- rotors, 4- mounting brackets, 5- rotor motors, 6- altimeters, 7- fillets
Camera, 8- elastic links, 9- storage devices, 10- fuselages, 11- support feets, 12- batteries, 13- photovoltaic solar cell plates.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
Refer in Fig. 1~2, the utility model embodiment, it is a kind of to determine the high unmanned plane steadily monitored, including fuselage
10, the fuselage 10 is disc-shaped structure, and the side of fuselage 10 is circumferentially uniformly provided with four elastic links 8, the end of elastic link 8
Portion is provided with circular protecting frame 2, and each described protecting frame 2 and fuselage 10 are in the same plane, the protecting frame 2 it is interior
Portion, which coordinates, is provided with mounting bracket 4, and mounting bracket 4 is cross bracket, and the middle part of mounting bracket 4 is provided with rotor motor 5, rotor
The output shaft of motor 5 is provided with rotor 3, drives rotor 3 to rotate by rotor motor 5, to produce downward thrust, passes through protection
Frame 2 can be protected to rotor motor 5 and rotor 3, to lift its drop resistant ability.
The reverse side of the fuselage 10, which coordinates, is provided with photovoltaic solar cell plate 13, and the inside of fuselage 10 is additionally provided with for dress
The battery 12 being powered is put, battery 12 is electrically connected by solar charging controller with photovoltaic solar cell plate 13
Connect, when sunshine is sufficient, energy storage can be carried out to battery 12 by photovoltaic solar cell plate 13, energy-conserving and environment-protective can extend
The flight time of unmanned plane, the positive outer ring of the fuselage 10 is provided with multiple support feets 11, and support feet 11 is by elastomeric light metal material
Material is made, and support feet 11 is provided with 4, and support feet 11 and connecting rod 8 can be fallen to be staggered by support feet 11 to device
Ground is supported, and the positive Middle face of the fuselage 10 is provided with fillet camera 7, and monitoring of taking photo by plane can be carried out by fillet camera 7, described
The front of fuselage 10 further respectively has altimeter 6 and storage device 9, and the altimeter 6 is radio altimeter or ultrasonic wave height
Degree meter, can be detected to the height of unmanned plane by altimeter 6, be conveniently controlled, storage device 9 and the fillet shooting
First 7 are electrically connected with, and storage device 9 is provided with external equipment jack（It is not shown）, can be to fillet camera by storage device 9
7 monitor video is stored, and is easy to get off the copy content of shooting by external equipment jack.
In the utility model, the outer ring of the protecting frame 2 is additionally provided with multiple LED lamp beads 1, and LED lamp bead 1 is provided with 6~8,
And LED lamp bead 1 is located at the same side with fillet camera 7, by controlling LED lamp bead 1 to light, is easy to operator's night to observe nothing
Man-machine running status.
In addition, the control method of unmanned plane is the known content of this area, repeat no more.
Using when, by being uniformly arranged four rotor motors 5 in the outside of fuselage 10, operation stability is higher, passes through protection
Frame 2 can be protected to rotor 3 and rotor motor 5, lift its drop resistant ability, by controlling LED lamp bead 1 to light, and be easy to manipulation
Personnel's night observes the running status of unmanned plane, and protecting frame 2 and fuselage 10, further lifting device are connected by elastic link 8
Stability, stable support when can be landed by support feet 11 to device can be to the height of unmanned plane by altimeter 6
Detected, it is convenient to carry out fixed high control, monitored picture can be shot by fillet camera 7, and be stored in storage device 9,
Ground staff is facilitated to be copied, in addition, by photovoltaic solar cell plate 13 also energy storage, energy-saving ring can be carried out to battery 12
Protect, the flight time of unmanned plane can be extended.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that for clarity, those skilled in the art should
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It may be appreciated other embodiment.
Claims (8)
1. the high unmanned plane steadily monitored can be determined, including fuselage, it is characterised in that the side of the fuselage is circumferentially uniformly provided with four
Individual elastic link, the end of elastic link is provided with circular protecting frame, and the internal engagement of the protecting frame is provided with mounting bracket,
Rotor motor is installed, the output shaft of rotor motor is provided with rotor, and the reverse side of the fuselage, which coordinates, to be set in the middle part of mounting bracket
There is photovoltaic solar cell plate, the inside of fuselage is additionally provided with the battery for being powered to device, and battery passes through the sun
Energy charge controller is electrically connected with photovoltaic solar cell plate, and the positive outer ring of the fuselage is provided with multiple support feets, described
The positive Middle face of fuselage is provided with fillet camera, and the front of the fuselage further respectively has altimeter and storage device, the storage
Cryopreservation device and fillet camera are electrically connected with, and the outer ring of the protecting frame is additionally provided with multiple LED lamp beads.
2. according to claim 1 determine the high unmanned plane steadily monitored, it is characterised in that the fuselage is discoid knot
Structure.
3. according to claim 1 or 2 determine the high unmanned plane steadily monitored, it is characterised in that each described protection
Frame and fuselage are in the same plane.
4. according to claim 1 determine the high unmanned plane steadily monitored, it is characterised in that the mounting bracket is cross
Shape support.
5. according to claim 1 determine the high unmanned plane steadily monitored, it is characterised in that the support feet is by elastomeric light
Metal material is made, and support feet is provided with 4, and support feet and connecting rod are to be staggered.
6. according to claim 1 determine the high unmanned plane steadily monitored, it is characterised in that the height is calculated as radio
Altimeter or ultrasonic height meter.
7. according to claim 1 determine the high unmanned plane steadily monitored, it is characterised in that the storage device is provided with
External equipment jack.
8. according to claim 1 determine the high unmanned plane steadily monitored, it is characterised in that the LED lamp bead provided with 6~
8, and LED lamp bead is located at the same side with fillet camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621041588.6U CN206437208U (en) | 2016-09-08 | 2016-09-08 | The high unmanned plane steadily monitored can be determined |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621041588.6U CN206437208U (en) | 2016-09-08 | 2016-09-08 | The high unmanned plane steadily monitored can be determined |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206437208U true CN206437208U (en) | 2017-08-25 |
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ID=59644091
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621041588.6U Active CN206437208U (en) | 2016-09-08 | 2016-09-08 | The high unmanned plane steadily monitored can be determined |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108557097A (en) * | 2018-04-26 | 2018-09-21 | 广州市科锐达光电技术有限公司 | A kind of performance formation unmanned plane equipped with the illumination of LED wheel exterior feature |
-
2016
- 2016-09-08 CN CN201621041588.6U patent/CN206437208U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108557097A (en) * | 2018-04-26 | 2018-09-21 | 广州市科锐达光电技术有限公司 | A kind of performance formation unmanned plane equipped with the illumination of LED wheel exterior feature |
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