CN205801528U - Solar energy aerial device - Google Patents
Solar energy aerial device Download PDFInfo
- Publication number
- CN205801528U CN205801528U CN201620525940.7U CN201620525940U CN205801528U CN 205801528 U CN205801528 U CN 205801528U CN 201620525940 U CN201620525940 U CN 201620525940U CN 205801528 U CN205801528 U CN 205801528U
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- CN
- China
- Prior art keywords
- solar energy
- aircraft
- connecting tube
- aerial device
- encapsulating structure
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
A kind of solar energy aerial device, including solar energy electroplax encapsulating structure, aircraft, fixed frame, camera head, first connecting tube and the second connecting tube, described solar energy electroplax encapsulating structure is airfoil, the upper and lower surface of described aircraft is equipped with connecting hole, the connecting hole of described aircraft upper surface is connected with described solar energy electroplax encapsulating structure by described first connecting tube, the connecting hole of described aircraft lower surface is connected with described fixed frame by described second connecting tube, described camera head is fixed on described fixed frame, it is provided with accumulator in described aircraft, described solar energy electroplax encapsulating structure is connected with described accumulator by described first connecting tube.Solar energy electroplax encapsulating structure in this utility model constantly receives luminous energy and is converted into the accumulator that electric energy is supplied in aircraft, and solar energy electroplax encapsulating structure is airfoil, can increase the lift in flight course, reduce the power consumption of flight, thus the purpose of the work that reaches to take photo by plane for a long time.
Description
Technical field
This utility model relates to aerial photography aircraft technical field, particularly relates to a kind of solar energy aerial device.
Background technology
Aerial photography aircraft shoots, because having high-altitude, the function that this traditional cameras cannot realize, and increasingly by people
Like, in addition to as photography art, aerial photography aircraft is also widely used in military affairs, transport development, hydraulic engineering, life
The aspects such as state research, urban planning.
Existing aerial photography aircraft is generally rotor and solid two kinds of the wing, all by frame, dynamical system, control sensor-based system,
Camera head forms, and realizes high-altitude shooting by being loaded on aircraft by camera head.
But existing aerial photography aircraft has an obvious deficiency to be exactly that flying power is excessively poor, it is impossible to flying for long time, needs
Often charging, can not meet the demand that user need to carry out shooting for a long time.
Utility model content
In view of above-mentioned condition, it is necessary to provide a kind of flying power long, the solar energy worked long hours can be met and take photo by plane dress
Put.
A kind of solar energy aerial device, including solar energy electroplax encapsulating structure, aircraft, fixed frame, camera head, the
One connecting tube and the second connecting tube, described solar energy electroplax encapsulating structure is airfoil, and the upper and lower surface of described aircraft is all provided with
Having connecting hole, the connecting hole of described aircraft upper surface is by described first connecting tube with described solar energy electroplax encapsulating structure even
Connecing, the connecting hole of described aircraft lower surface is connected with described fixed frame by described second connecting tube, described camera head
Being fixed on described fixed frame, be provided with accumulator in described aircraft, described solar energy electroplax encapsulating structure is by described the
One connecting tube is connected with described accumulator.
The solar energy aerial device that the utility model proposes, passes through connecting tube by solar energy electroplax encapsulating structure and aircraft
Connecting, and access the accumulator in aircraft, during taking photo by plane, solar energy electroplax encapsulating structure constantly receives luminous energy and converts
The accumulator being supplied in aircraft for electric energy, and solar energy electroplax encapsulating structure is airfoil, by increasing capacitance it is possible to increase in flight course
Lift, reduce the power consumption of flight, thus the purpose of the work that reaches to take photo by plane for a long time.
Above-mentioned solar energy aerial device, wherein, is provided with for regulating between described fixed frame and described second connecting tube
The moving machine of described camera head camera angle includes.
Above-mentioned solar energy aerial device, wherein, the connecting hole of described aircraft upper surface and described aircraft lower surface
Connecting hole is coaxial, and is positioned at the center of described aircraft.
Above-mentioned solar energy aerial device, wherein, described solar energy electroplax encapsulating structure, described first connecting tube, described
The axis of two connecting tubes and described fixed frame is same axis.
Above-mentioned solar energy aerial device, wherein, described first connecting tube and described second connecting tube are boring
Tubular structure.
Above-mentioned solar energy aerial device, wherein, described solar energy electroplax encapsulating structure and described aircraft use detachable
Formula connects.
Above-mentioned solar energy aerial device, wherein, described fixed frame uses detachable connection with described aircraft.
Above-mentioned solar energy aerial device, wherein, described aircraft includes aircraft frame, horn and propeller, described machine
One end of arm connects described aircraft frame, and the other end connects described propeller, and described propeller is near one end of described horn
It is provided with motor.
Above-mentioned solar energy aerial device, wherein, the quantity of described horn, described propeller and described motor is at least 4.
Above-mentioned solar energy aerial device, wherein, described aircraft frame is square or circular.
Accompanying drawing explanation
Fig. 1 is the structural representation of the solar energy aerial device that this utility model first embodiment proposes；
Fig. 2 is the structural representation of solar energy electroplax encapsulating structure in Fig. 1；
Fig. 3 is the partial structurtes signal that in the solar energy aerial device that this utility model the second embodiment proposes, moving machine includes
Figure.
Main element symbol description
Solar energy electroplax encapsulating structure 10；Aircraft 20
Fixed frame 30；Camera head 40
First connecting tube 50；Second connecting tube 60
Moving machine includes 70；Aircraft frame 201
Horn 202；Propeller 203
Motor 204；
Following detailed description of the invention will further illustrate this utility model in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
For the ease of understanding this utility model, below with reference to relevant drawings, this utility model is more fully retouched
State.Accompanying drawing gives some embodiments of the present utility model.But, this utility model can come real in many different forms
Existing, however it is not limited to embodiment described herein.On the contrary, providing the purpose of these embodiments is to make public affairs of the present utility model
Open content more thorough comprehensively.
It should be noted that when element is referred to as " being fixedly arranged on " another element, and it can be directly on another element
Or element placed in the middle can also be there is.When an element is considered as " connection " another element, and it can be to be directly connected to
To another element or may be simultaneously present centering elements.Term as used herein " vertical ", " level ", " left ",
" right " and similar statement are for illustrative purposes only.
Unless otherwise defined, all of technology used herein and scientific terminology are led with belonging to technology of the present utility model
The implication that the technical staff in territory is generally understood that is identical.At term used in the description of the present utility model it is simply herein
The purpose of specific embodiment is described, it is not intended that in limiting this utility model.Term as used herein " and/or " include
Arbitrary and all of combination of one or more relevant Listed Items.
Embodiment 1:
Referring to Fig. 1 and Fig. 2, the solar energy aerial device that this utility model first embodiment proposes, it includes solar energy
Electroplax encapsulating structure 10, aircraft 20, fixed frame 30, camera head the 40, first connecting tube 50 and the second connecting tube 60, described
Solar energy electroplax encapsulating structure 10 by multiple solar panels encapsulation formed, described solar energy electroplax encapsulating structure 10 in
Airfoil, can effectively increase the lift of aerial device in flight course, and the upper and lower surface of described aircraft 20 is equipped with even
Connecing hole, the connecting hole of described aircraft 20 upper surface is by described first connecting tube 50 and described solar energy electroplax encapsulating structure 10
Connecting, the connecting hole of described aircraft 20 lower surface is connected with described fixed frame 30 by described second connecting tube 60, described
Camera head 40 is fixed on described fixed frame 30, is provided with accumulator in described aircraft 20, and described solar energy electroplax encapsulates
Structure 10 is connected with described accumulator by described first connecting tube 50.
In the present embodiment, the connecting hole of described aircraft 20 upper surface is same with the connecting hole of described aircraft 20 lower surface
Axle, and be positioned at the center of described aircraft 20, described solar energy electroplax encapsulating structure 10, described first connecting tube 50, described
The axis of two connecting tubes 60 and described fixed frame 30 is same axis, described first connecting tube 50 and described second connecting tube 60
Wire, the described sun is accommodated in being the tubular structure of boring, described first connecting tube 50 and described second connecting tube 60
Electric power system, institute can be formed by wire with the accumulator within aircraft 20 by encapsulating structure 10 by described first connecting tube 50
State solar energy electroplax encapsulating structure 10 and use detachable connection, described fixed frame 30 and described flight with described aircraft 20
Device 20 is also adopted by detachable connection, it is simple to assembles and keeps in repair.Described aircraft 20 includes aircraft frame 201, horn 202 and
Propeller 203, one end of described horn 202 connects described aircraft frame 201, and the other end connects described propeller 203, described
Propeller 203 is provided with motor 204, described horn 202, described propeller 203 and described motor near one end of described horn 202
The quantity of 204 is at least 4, the most in the present embodiment, and described horn 202, described propeller 203 and described motor 204
Quantity is 4, and is symmetrical arranged, and described aircraft frame 201 is square or circular, the most in the present embodiment, and described flight
Device frame 201 uses square.
Embodiment 2:
Referring to Fig. 3, the solar energy aerial device that this utility model the second embodiment proposes, as this utility model first
A kind of improvement of embodiment, is provided with for regulating described camera head between described fixed frame 30 and described second connecting tube 60
The moving machine of 40 camera angle includes 70, thus realizes the shooting of different angles.
The solar energy aerial device that the utility model proposes, passes through connecting tube by solar energy electroplax encapsulating structure and aircraft
Connecting, and access the accumulator in aircraft, during taking photo by plane, solar energy electroplax encapsulating structure constantly receives luminous energy and converts
The accumulator being supplied in aircraft for electric energy, and solar energy electroplax encapsulating structure is airfoil, by increasing capacitance it is possible to increase in flight course
Lift, reduce the power consumption of flight, thus the purpose of the work that reaches to take photo by plane for a long time.
Embodiment described above only have expressed several embodiments of the present utility model, and it describes more concrete and detailed,
But therefore can not be interpreted as the restriction to this utility model the scope of the claims.It should be pointed out that, common for this area
For technical staff, without departing from the concept of the premise utility, it is also possible to make some deformation and improvement, these are all
Belong to protection domain of the present utility model.Therefore, the protection domain of this utility model patent should be as the criterion with claims.
Claims (10)
1. a solar energy aerial device, it is characterised in that include solar energy electroplax encapsulating structure, aircraft, fixed frame, take the photograph
As device, the first connecting tube and the second connecting tube, described solar energy electroplax encapsulating structure is airfoil, described aircraft upper and lower
Surface is equipped with connecting hole, and the connecting hole of described aircraft upper surface is sealed with described solar energy electroplax by described first connecting tube
Assembling structure connects, and the connecting hole of described aircraft lower surface is connected with described fixed frame by described second connecting tube, described
Camera head is fixed on described fixed frame, is provided with accumulator in described aircraft, and described solar energy electroplax encapsulating structure leads to
Cross described first connecting tube to be connected with described accumulator.
Solar energy aerial device the most according to claim 1, it is characterised in that described fixed frame is connected with described second
It is provided with between pipe and includes for the moving machine regulating described camera head camera angle.
Solar energy aerial device the most according to claim 1, it is characterised in that the connecting hole of described aircraft upper surface with
The connecting hole of described aircraft lower surface is coaxial, and is positioned at the center of described aircraft.
Solar energy aerial device the most according to claim 3, it is characterised in that described solar energy electroplax encapsulating structure, institute
The axis stating the first connecting tube, described second connecting tube and described fixed frame is same axis.
Solar energy aerial device the most according to claim 4, it is characterised in that described first connecting tube and described second is even
Adapter is the tubular structure of boring.
Solar energy aerial device the most according to claim 1, it is characterised in that described solar energy electroplax encapsulating structure and institute
State aircraft and use detachable connection.
Solar energy aerial device the most according to claim 1, it is characterised in that described fixed frame is adopted with described aircraft
Use detachable connection.
8. according to the solar energy aerial device described in claim 1 to 7 any one, it is characterised in that described aircraft includes
Aircraft frame, horn and propeller, one end of described horn connects described aircraft frame, and the other end connects described spiral
Oar, described propeller is provided with motor near one end of described horn.
Solar energy aerial device the most according to claim 8, it is characterised in that described horn, described propeller and described
The quantity of motor is at least 4.
Solar energy aerial device the most according to claim 8, it is characterised in that described aircraft frame is square or circle
Shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620525940.7U CN205801528U (en) | 2016-05-31 | 2016-05-31 | Solar energy aerial device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620525940.7U CN205801528U (en) | 2016-05-31 | 2016-05-31 | Solar energy aerial device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205801528U true CN205801528U (en) | 2016-12-14 |
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ID=57501681
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620525940.7U Active CN205801528U (en) | 2016-05-31 | 2016-05-31 | Solar energy aerial device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205801528U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108928479A (en) * | 2018-06-28 | 2018-12-04 | 山东浩坤安全技术咨询有限公司 | A kind of rotor wing unmanned aerial vehicle with solar recharging |
-
2016
- 2016-05-31 CN CN201620525940.7U patent/CN205801528U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108928479A (en) * | 2018-06-28 | 2018-12-04 | 山东浩坤安全技术咨询有限公司 | A kind of rotor wing unmanned aerial vehicle with solar recharging |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Solar aerial photography device Effective date of registration: 20230808 Granted publication date: 20161214 Pledgee: Yunongshang Financial Leasing Co.,Ltd. Pledgor: NANCHANG INSTITUTE OF TECHNOLOGY Registration number: Y2023980051441 |