CN108860615A - Solar energy unmanned plane towed solar battery strut - Google Patents
Solar energy unmanned plane towed solar battery strut Download PDFInfo
- Publication number
- CN108860615A CN108860615A CN201810612269.3A CN201810612269A CN108860615A CN 108860615 A CN108860615 A CN 108860615A CN 201810612269 A CN201810612269 A CN 201810612269A CN 108860615 A CN108860615 A CN 108860615A
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- China
- Prior art keywords
- solar battery
- unmanned plane
- towed
- strut
- solar energy
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000007246 mechanism Effects 0.000 claims abstract description 60
- 238000006243 chemical reaction Methods 0.000 claims abstract description 9
- 238000004891 communication Methods 0.000 claims description 8
- 206010063385 Intellectualisation Diseases 0.000 abstract description 2
- 241000127225 Enceliopsis nudicaulis Species 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 6
- 230000006872 improvement Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 241001424688 Enceliopsis Species 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000005693 optoelectronics Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000004886 process control Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D3/00—Aircraft adaptations to facilitate towing or being towed
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses solar energy unmanned plane towed solar battery struts, towed solar battery strut is set in the rear end accommodating groove of solar energy unmanned plane, towed solar battery strut includes for telescoping mechanism flexible up and down, and the rotating mechanism for horizontal rotation, and the swing mechanism for wallowing motion, and for controlling telescoping mechanism, rotating mechanism and the control mechanism of swing mechanism；The signal output end of control mechanism and the control terminal of telescoping mechanism, rotating mechanism and swing mechanism are separately connected.Towed solar battery is connected to solar energy unmanned plane rear end by the towed solar battery strut that the present invention introduces, improve the connective stability of solar battery, remotely controlled by controller's intellectualization strut rotate horizontally, shrink up and down, tilt swing etc., realize the expansion and storage of towed solar battery, it is convenient and efficient, and the adjustable alignment sunray of solar battery, improve photoelectric conversion efficiency.
Description
Technical field
The present invention relates to solar energy air vehicle technique fields, and in particular to solar energy unmanned plane towed solar battery branch
Bar.
Background technique
Solar energy unmanned plane is a kind of course of new aircraft with development potential.It is not necessarily to using solar energy as power resources
Any fuel is carried, permanent airflight theoretically may be implemented.Daytime, by the photovoltaic cell for being layed in aircraft and showing,
Solar energy unmanned plane converts solar energy into electrical energy, and a part of electric energy is directly used for propeller and airborne electrical equipment, maintains
The normal flight of unmanned plane, another part electric energy is stored in energy-storage battery, for night use.Energy power system was with one day
One circulation is not required to consume any fuel, therefore solar energy unmanned plane has the overlength endurance of several weeks to several months.Compared to conventional nothing
Man-machine, solar energy unmanned plane is with the obvious advantage, and application prospect is boundless, it might even be possible to serve as the role of " atmosphere satellite ".
But since intensity of solar radiation is weaker, the optoelectronic transformation efficiency of photovoltaic cell is relatively low, leads to solar energy unmanned plane
Nominal power is small, flying speed is low.In order to maintain normal flight and work, solar energy unmanned plane one under limited nominal power
As use high aspect ratio lightweight wing, this also brings the disadvantages of wind loading rating is weaker.
For this purpose, Recent study has gone out the towed solar cell for solar energy unmanned plane, pass through rope or company
Extension bar pulls at the rear of body, can effectively solve the problems, such as above-mentioned electricity shortage in this way.For example, as shown in Figure 1, show
It is a kind of structure of the towed solar cell of traditional solar energy unmanned plane, is directly to tie up to unmanned plane rear end by rope,
There are some drawbacks, such as solar cell to be easy with air-flow inverting for this pulling mode, and stability is not high；And it is unable to control the sun
The tilt angle of battery is unfavorable for being directed at sunray；In addition, also need manually to arrange when storage, it is more inconvenient.
Summary of the invention
Technical problem to be solved by the present invention lies in provide solar energy unmanned plane towed solar battery strut, solution
Having determined, the stability that traditional solar cell connects is not high, be unable to control the tilt angle of solar cell and storage is inconvenient asks
Topic.
The technical problems to be solved by the invention are realized using following technical scheme：
Solar energy unmanned plane towed solar battery strut, the towed solar battery strut be set to solar energy without
In man-machine rear end accommodating groove, the towed solar battery strut includes for telescoping mechanism flexible up and down, Yi Jiyong
In the rotating mechanism of horizontal rotation, and for the swing mechanism of wallowing motion, and for controlling telescoping mechanism, whirler
The control mechanism of structure and swing mechanism；
The signal output end of the control mechanism and the control terminal of telescoping mechanism, rotating mechanism and swing mechanism connect respectively
It connects.
Further improvement lies in that the telescoping mechanism includes hydraulic cylinder and telescopic rod, the rotating mechanism includes the first electricity
Turn axis, the swing mechanism include horizon bar and the second electric rotation shaft；
The hydraulic cylinder is set to inside the solar energy unmanned plane on accommodating groove top, and the telescopic rod is connected to hydraulic cylinder
On output end, and telescopic rod is vertically arranged, and first electric rotation shaft is set to the centre of telescopic rod, and telescopic rod is divided into upper and lower two
Part, and the telescopic rod of lower part is rotated as the first electric rotation shaft rotates, the centre of the horizon bar is provided with loose slot, institute
The second electric rotation shaft is stated in loose slot, the lower end of the telescopic rod is connected on the second electric rotation shaft.
Further improvement lies in that the control mechanism is controller, the controller includes single-chip microcontroller, and and single-chip microcontroller
The wireless communication module and signal conversion module of connection.
Further improvement lies in that the single-chip microcontroller model STC12C5A60S2, the model of the wireless communication module
UTC-4432-T2000；The model C2000MDI8 of the signal conversion module.
The beneficial effects of the invention are as follows：Towed solar battery is connected to solar energy by towed solar battery strut
Unmanned plane rear end improves the connective stability of solar battery, remotely controlled by controller's intellectualization strut rotate horizontally,
It shrinks up and down, tilt swing etc., realizes the expansion and storage of towed solar battery, convenient and efficient, and solar-electricity
The adjustable alignment sunray in pond, improves photoelectric conversion efficiency.
Detailed description of the invention
Fig. 1 is the towed solar battery structure schematic diagram of traditional solar energy unmanned plane；
Fig. 2 is the structural schematic diagram of towed solar battery strut；
Fig. 3 is the use installation diagram of towed solar battery strut on solar energy unmanned plane；
Fig. 4 be towed solar battery strut in horizon bar be rotated by 90 ° after structural schematic diagram；
Fig. 5 is structural schematic diagram when towed solar battery strut is accommodated in accommodating groove；
Wherein, 1- solar energy unmanned plane, 2- accommodating groove, 3- hydraulic cylinder, 4- telescopic rod, the first electric rotation shaft of 5-, 6- are horizontal
Bar, the second electric rotation shaft of 7-, 8- loose slot.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, tie below
Specific embodiment and diagram are closed, the present invention is further explained.
In conjunction with shown in Fig. 2 and Fig. 3, solar energy unmanned plane towed solar battery strut, towed solar battery branch
Bar is set in the rear end accommodating groove 2 of solar energy unmanned plane 1, and towed solar battery strut includes flexible for what is stretched up and down
Mechanism, and it is flexible for the rotating mechanism of horizontal rotation, and for the swing mechanism of wallowing motion, and for controlling
The control mechanism of mechanism, rotating mechanism and swing mechanism.The signal output end and telescoping mechanism, rotating mechanism and pendulum of control mechanism
The control terminal of motivation structure is separately connected.
Wherein, telescoping mechanism includes hydraulic cylinder 3 and telescopic rod 4, and rotating mechanism includes the first electric rotation shaft 5, swing mechanism
Including horizon bar 6 and the second electric rotation shaft 7；Hydraulic cylinder 3 is set to inside the solar energy unmanned plane 1 on 2 top of accommodating groove, telescopic rod
4 are connected on the output end of hydraulic cylinder 3, and telescopic rod 4 is vertically arranged, and the first electric rotation shaft 5 is set to the centre of telescopic rod 4, will
Telescopic rod 4 is divided into two parts up and down, and the telescopic rod 4 of lower part is rotated as the first electric rotation shaft 5 rotates, horizon bar 6
Centre is provided with loose slot 8, and the second electric rotation shaft 7 is set in loose slot 8, and the lower end of telescopic rod 4 is connected to the second electric rotation shaft 7
On.
In addition, control mechanism is controller, controller includes single-chip microcontroller, and the wireless communication module connecting with single-chip microcontroller
And signal conversion module.Single-chip microcontroller model STC12C5A60S2, the model UTC-4432-T2000 of wireless communication module, letter
The model C2000MDI8 of number conversion module, for the digital-to-analogue between single-chip microcontroller and telescoping mechanism, rotating mechanism and swing mechanism
Conversion.Wireless communication module be used for computer or other ground controlling terminal interconnected communications, it is remote by ground controlling terminal
The functions such as storage, expansion, tilt adjustment are realized in the movement of process control above-mentioned telescoping mechanism, rotating mechanism and swing mechanism.
In conjunction with shown in Fig. 4 and Fig. 5, solar cell is pulled by strut in the rear end of solar energy unmanned plane 1 under original state,
It is spread out for one word of level.It in the tilt angle for needing to adjust solar cell, can be rotated by the second electric rotation shaft 7, drive water
Flat bar 6 is rotated relative to telescopic rod 4, and then drives the biased of entire solar cell, it is made to be directed at sunray.In the storage sun
When battery, first solar cell is folded, is closed up with horizon bar 6, then controls the first electric rotation shaft 5 and rotates 90 °, then control is flexible
Bar 4 is shunk, and moves up horizon bar 6 and solar cell, 6 a part of horizon bar is accommodated in accommodating groove 2, and a part extends in
Folding storage is completed in 2 rear end of accommodating groove.
It should be noted that the method that above-mentioned solar cell folding process can use folding electromagnetic, this method are being applied
Number for CN201810328814.6 Chinese invention patent in be discussed in detail.
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the above embodiments and description only describe originals of the invention
Reason, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these changes and improvements
It all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent circle
It is fixed.
Claims (4)
1. solar energy unmanned plane towed solar battery strut, the towed solar battery strut be set to solar energy nobody
In the rear end accommodating groove (2) of machine (1), it is characterised in that：The towed solar battery strut includes for flexible up and down
Telescoping mechanism, and for the rotating mechanism of horizontal rotation, and for the swing mechanism of wallowing motion, and for controlling
The control mechanism of telescoping mechanism, rotating mechanism and swing mechanism；
The signal output end of the control mechanism and the control terminal of telescoping mechanism, rotating mechanism and swing mechanism are separately connected.
2. solar energy unmanned plane towed solar battery strut according to claim 1, it is characterised in that：It is described flexible
Mechanism includes hydraulic cylinder (3) and telescopic rod (4), and the rotating mechanism includes the first electric rotation shaft (5), and the swing mechanism includes
Horizon bar (6) and the second electric rotation shaft (7)；
The solar energy unmanned plane (1) that the hydraulic cylinder (3) is set to accommodating groove (2) top is internal, and the telescopic rod (4) is connected to
On the output end of hydraulic cylinder (3), and telescopic rod (4) is vertically arranged, and first electric rotation shaft (5) is set in telescopic rod (4)
Between, telescopic rod (4) is divided into two parts up and down, and the telescopic rod (4) of lower part turns as the first electric rotation shaft (5) rotate
Dynamic, the centre of the horizon bar (6) is provided with loose slot (8), and second electric rotation shaft (7) is set in loose slot (8), described to stretch
The lower end of contracting bar (4) is connected on the second electric rotation shaft (7).
3. solar energy unmanned plane towed solar battery strut according to claim 1, it is characterised in that：The control
Mechanism is controller, and the controller includes single-chip microcontroller, and the wireless communication module and signal modulus of conversion that connect with single-chip microcontroller
Block.
4. solar energy unmanned plane towed solar battery strut according to claim 3, it is characterised in that：The monolithic
Machine model STC12C5A60S2, the model UTC-4432-T2000 of the wireless communication module, the signal conversion module
Model C2000MDI8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810612269.3A CN108860615A (en) | 2018-06-14 | 2018-06-14 | Solar energy unmanned plane towed solar battery strut |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810612269.3A CN108860615A (en) | 2018-06-14 | 2018-06-14 | Solar energy unmanned plane towed solar battery strut |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108860615A true CN108860615A (en) | 2018-11-23 |
Family
ID=64338280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810612269.3A Pending CN108860615A (en) | 2018-06-14 | 2018-06-14 | Solar energy unmanned plane towed solar battery strut |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108860615A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113955121A (en) * | 2021-12-01 | 2022-01-21 | 北京航空航天大学 | Unmanned aerial vehicle empty base recovery device and method |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080030884A1 (en) * | 2006-04-24 | 2008-02-07 | Bruno Hershkovitz | Device and method for affecting local climatic parameters |
| CN105383645A (en) * | 2014-06-30 | 2016-03-09 | 王云章 | Dragging floating type solar power station used for boat |
| CN106143925A (en) * | 2015-04-12 | 2016-11-23 | 况厚波 | A kind of new type solar energy aircraft |
| CN206041896U (en) * | 2016-08-30 | 2017-03-22 | 江苏康博光伏电力科技有限公司 | Solar photovoltaic board support with automatically, receive and release function |
-
2018
- 2018-06-14 CN CN201810612269.3A patent/CN108860615A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080030884A1 (en) * | 2006-04-24 | 2008-02-07 | Bruno Hershkovitz | Device and method for affecting local climatic parameters |
| CN105383645A (en) * | 2014-06-30 | 2016-03-09 | 王云章 | Dragging floating type solar power station used for boat |
| CN106143925A (en) * | 2015-04-12 | 2016-11-23 | 况厚波 | A kind of new type solar energy aircraft |
| CN206041896U (en) * | 2016-08-30 | 2017-03-22 | 江苏康博光伏电力科技有限公司 | Solar photovoltaic board support with automatically, receive and release function |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113955121A (en) * | 2021-12-01 | 2022-01-21 | 北京航空航天大学 | Unmanned aerial vehicle empty base recovery device and method |
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| PB01 | Publication | ||
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| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20181123 |
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| RJ01 | Rejection of invention patent application after publication |