CN113035984A - Photovoltaic module laying method of monocoque solar unmanned aerial vehicle - Google Patents
Photovoltaic module laying method of monocoque solar unmanned aerial vehicle Download PDFInfo
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- CN113035984A CN113035984A CN201911332898.1A CN201911332898A CN113035984A CN 113035984 A CN113035984 A CN 113035984A CN 201911332898 A CN201911332898 A CN 201911332898A CN 113035984 A CN113035984 A CN 113035984A
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/042—PV modules or arrays of single PV cells
- H01L31/048—Encapsulation of modules
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Abstract
The invention provides a method for laying photovoltaic modules of a monocoque solar unmanned aerial vehicle, which comprises the following steps: pasting a preset number of photovoltaic modules in a preset area on the surface of a wing of a solar unmanned aerial vehicle; and applying pressure to the photovoltaic modules in the preset number so that the photovoltaic modules are firmly bonded with the surface of the wing. According to the photovoltaic module laying method of the monocoque type solar unmanned aerial vehicle, provided by the embodiment of the invention, the convenience of laying the photovoltaic module of the monocoque type solar unmanned aerial vehicle is improved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a photovoltaic module laying method of a monocoque solar unmanned aerial vehicle.
Background
The solar unmanned aerial vehicle takes solar energy as energy, can fly permanently in theory, has no pollution to the environment, is flexible to use, has low cost and has wide application prospect.
At present, solar unmanned aerial vehicle mainly divide into flexible solar unmanned aerial vehicle of light and monocoque solar unmanned aerial vehicle, and two kinds of unmanned aerial vehicle respectively have characteristics. In consideration of application of the solar unmanned aerial vehicle, the photovoltaic module not only needs to have higher photoelectric conversion efficiency, but also has the characteristics of light weight, flexibility, adaptability to application of wing airfoil curved surfaces and the like. Among the prior art, the flexible solar energy unmanned aerial vehicle of light mostly adopts covering integration photovoltaic module, and this type of photovoltaic module all lays the unmanned aerial vehicle surface through complicated frock to the form of splicing. The skin integrated photovoltaic module laying method has the defects of poor pneumatic appearance dimension, complex operation steps, low laying efficiency and the like, and is not suitable for laying the photovoltaic module of the monocoque solar unmanned aerial vehicle. For the monocoque solar unmanned aerial vehicle, laying the photovoltaic module of the monocoque solar unmanned aerial vehicle is a problem to be solved urgently in the industry at present.
Disclosure of Invention
Aiming at the problems in the prior art, the embodiment of the invention provides a method for laying a photovoltaic module of a monocoque solar unmanned aerial vehicle.
The invention provides a method for laying photovoltaic modules of a monocoque solar unmanned aerial vehicle, which comprises the following steps:
pasting a preset number of photovoltaic modules in a preset area on the surface of a wing of a solar unmanned aerial vehicle;
and applying pressure to the photovoltaic modules in the preset number so that the photovoltaic modules are firmly bonded with the surface of the wing.
Before a preset number of photovoltaic modules are pasted on a preset area of the wing surface of the solar unmanned aerial vehicle, the method for laying the photovoltaic modules of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
cleaning a preset area of the surface of the wing, and spraying insulating paint on the preset area of the surface of the wing.
Before a preset number of photovoltaic modules are pasted on a preset area of the wing surface of the solar unmanned aerial vehicle, the method for laying the photovoltaic modules of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and adhering insulating adhesive tapes to the preset areas on the surface of the wing and the areas corresponding to the preset number of electrodes of the photovoltaic modules.
Before a preset number of photovoltaic modules are pasted on a preset area of the wing surface of the solar unmanned aerial vehicle, the method for laying the photovoltaic modules of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and carrying out quality detection on the photovoltaic modules in the preset number.
The photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and carrying out quality detection on the photovoltaic module after laying is completed.
The photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and welding the electrodes of the adjacent photovoltaic modules.
The photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and filling gaps between adjacent photovoltaic modules with sealant.
Before a preset number of photovoltaic modules are pasted on a preset area of the wing surface of the solar unmanned aerial vehicle, the method for laying the photovoltaic modules of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and (4) sticking the masking paper along the edge face of the front side of each photovoltaic module.
The photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention further comprises the following steps:
and removing the masking paper adhered to the surface of each photovoltaic module.
Wherein said applying pressure to said preset number of photovoltaic modules comprises:
and applying pressure to the photovoltaic modules in the preset number by adopting a cylindrical tool.
According to the photovoltaic module laying method of the monocoque type solar unmanned aerial vehicle, provided by the embodiment of the invention, the photovoltaic modules of the preset number can be pasted on the preset area of the wing surface of the solar unmanned aerial vehicle, and pressure is applied to the photovoltaic modules of the preset number, so that the photovoltaic modules are firmly bonded with the wing surface, the method is easy to realize in engineering, and the convenience in laying the photovoltaic modules of the monocoque type solar unmanned aerial vehicle is improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts. In the drawings:
fig. 1 is a schematic flow chart of a photovoltaic module laying method of a monocoque solar unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 2 is a schematic structural diagram of a front side of a photovoltaic module of the monocoque solar drone provided in an embodiment of the present invention.
Fig. 3 is a schematic view of a back structure of a photovoltaic module of the monocoque solar drone according to an embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the embodiments of the present invention are further described in detail below with reference to the accompanying drawings. The exemplary embodiments and descriptions of the present invention are provided to explain the present invention, but not to limit the present invention. It should be noted that the embodiments and features of the embodiments in the present application may be arbitrarily combined with each other without conflict.
Fig. 1 is a schematic flow diagram of a method for laying photovoltaic modules of a monocoque solar unmanned aerial vehicle according to an embodiment of the present invention, and as shown in fig. 1, the method for laying photovoltaic modules of a monocoque solar unmanned aerial vehicle according to an embodiment of the present invention includes:
s101, sticking a preset number of photovoltaic modules in a preset area on the surface of a wing of a solar unmanned aerial vehicle;
specifically, lay photovoltaic module to monocoque solar unmanned aerial vehicle, can set up photovoltaic module at solar unmanned aerial vehicle's wing surface the region of predetermineeing of solar unmanned aerial vehicle's wing surface pastes the photovoltaic module of predetermineeing quantity through the mode of pasting wing surface. The preset area is set according to actual needs, and the embodiment of the invention is not limited. The preset number is selected according to actual needs, and the embodiment of the invention is not limited.
For example, a solid double-sided adhesive tape may be adhered to the back surface of each photovoltaic module, and each photovoltaic module may be adhered to a preset area of the wing surface of the solar drone through the solid double-sided adhesive tape. Wherein, the back of the photovoltaic module refers to the side which does not absorb solar energy. Can be 1-1.5 mm thick and 720kg/m density3The solid double-sided adhesive tape of (1).
S102, applying pressure to the photovoltaic modules in the preset number to enable the photovoltaic modules to be firmly bonded with the surface of the wing.
Specifically, after the preset number of photovoltaic modules are adhered to the preset area of the wing surface, pressure can be applied to the preset number of photovoltaic modules, so that the photovoltaic modules are firmly adhered to the wing surface.
According to the photovoltaic module laying method of the monocoque type solar unmanned aerial vehicle, provided by the embodiment of the invention, the photovoltaic modules of the preset number can be pasted on the preset area of the wing surface of the solar unmanned aerial vehicle, and pressure is applied to the photovoltaic modules of the preset number, so that the photovoltaic modules are firmly bonded with the wing surface, the method is easy to realize in engineering, and the convenience in laying the photovoltaic modules of the monocoque type solar unmanned aerial vehicle is improved.
On the basis of the above embodiments, further, before a preset number of photovoltaic modules are pasted on a preset area on the wing surface of the solar unmanned aerial vehicle, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
cleaning a preset area of the surface of the wing, and spraying insulating paint on the preset area of the surface of the wing.
Specifically, before laying a photovoltaic module on the wing surface of the solar unmanned aerial vehicle, a preset area of the wing surface needs to be preprocessed. The preset area of the wing surface can be cleaned, and insulating paint is sprayed on the preset area of the wing surface. The surface of the wing is cleaned, so that impurities can be removed, and the firmness of subsequent sticking is improved. And insulating paint is sprayed to insulate the photovoltaic module from the wing. Wherein the insulating varnish may be black. In order to reduce the influence of the insulating paint on the increased weight of the solar unmanned aerial vehicle, the density of the insulating paint is as low as possible on the basis that the adsorption force of the sprayed insulating paint meets the requirement, for example, the insulating paint with the density of 0.8g/ml is selected.
On the basis of the above embodiments, further, before a preset number of photovoltaic modules are pasted on a preset area on the wing surface of the solar unmanned aerial vehicle, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
and adhering insulating adhesive tapes to the preset areas on the surface of the wing and the areas corresponding to the preset number of electrodes of the photovoltaic modules.
Specifically, the laying positions of the photovoltaic modules in the preset number can be divided in a preset area on the surface of the wing, and then the insulating tapes are pasted on the areas corresponding to the electrodes of the photovoltaic modules. The insulating tape can be a polyimide insulating tape. In order to reduce the influence of the weight of the insulating tape on the increase of the solar unmanned aerial vehicle, the thickness of the insulating tape is required to be as small as possible on the basis of meeting the insulation requirement, and the polyimide tape with the thickness of 50-80 microns can be selected, for example, the polyimide tape with the thickness of 60 microns is selected.
On the basis of the above embodiments, further, before a preset number of photovoltaic modules are pasted on a preset area on the wing surface of the solar unmanned aerial vehicle, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
and carrying out quality detection on the photovoltaic modules in the preset number.
Specifically, before laying photovoltaic module, need right preset quantity's photovoltaic module carries out quality testing to avoid photovoltaic module to appear quality problems. The quality detection comprises the steps of detecting the voltage of each string of cells in the photovoltaic module by using a voltmeter, and detecting the fragmentation condition of each string of cells in the photovoltaic module by using an EL (electroluminescence) testing device. If the photovoltaic module has a problem, the photovoltaic module with the problem is replaced.
On the basis of the above embodiments, further, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
and carrying out quality detection on the photovoltaic module after laying is completed.
Specifically, after the photovoltaic modules are laid, the quality of the photovoltaic modules in the preset number is detected, so that the photovoltaic modules with problems in the laying process are found. The quality detection comprises the steps of detecting the voltage of each string of batteries in the photovoltaic module by using a voltmeter and detecting the fragmentation condition of each string of batteries in the photovoltaic module by using EL testing equipment. If find photovoltaic module goes wrong, then change the photovoltaic module who goes wrong, lay again.
On the basis of the above embodiments, further, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
and welding the electrodes of the adjacent photovoltaic modules.
Specifically, after the photovoltaic modules with the preset number are laid, the electrodes of the adjacent photovoltaic modules can be welded, that is, the lap joints of the electrodes between the adjacent photovoltaic modules are welded, so that the adjacent photovoltaic modules are electrically connected.
On the basis of the above embodiments, further, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
and filling gaps between adjacent photovoltaic modules with sealant.
Specifically, because there is the clearance in the welding seam department between the adjacent photovoltaic module, can adopt sealed glue to fill adjacent the clearance between the photovoltaic module makes sealed glue parcel adjacent the electrode of photovoltaic module to increase the fastness between the photovoltaic module and avoid the electrode oxidation. In order to maintain the aerodynamic shape of the solar unmanned aerial vehicle, the height of the sealing glue can be kept consistent with the thickness of the photovoltaic module. In order to reduce the influence of the sealant on the weight increase of the solar unmanned aerial vehicle, the density of the used sealant is as low as possible on the basis of meeting the sealing requirement under the corresponding environmental condition, the sealant with the density of 1-3 g/ml and the temperature adaptive range of-55 ℃ to +65 ℃ can be selected, and for example, the density of the adopted sealant is 2 g/ml.
On the basis of each embodiment, further, before the photovoltaic module of predetermineeing the regional pasting of predetermineeing quantity on solar energy unmanned aerial vehicle's wing surface, still include:
and (4) sticking the masking paper along the edge face of the front side of each photovoltaic module.
Specifically, in order to avoid pollution to the photovoltaic module surface during the laying process of the photovoltaic module, the crepe paper can be pasted along the front edge of each photovoltaic module. In order to maintain the shape of the photovoltaic modules during application, facilitate subsequent filling of gaps between the photovoltaic modules and facilitate treatment of redundant fillers, the textured paper is required to have a small thickness and not to block the gaps between adjacent photovoltaic modules. In which a 50 micron thick and 20 mm wide textured paper may be used. The front side of the photovoltaic module refers to the side capable of absorbing solar energy.
On the basis of the above embodiments, further, the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the present invention further includes:
and removing the masking paper adhered to the surface of each photovoltaic module.
Specifically, after the photovoltaic modules are laid, the masking paper adhered to the surface of each photovoltaic module needs to be removed. In order to remove the masking paper conveniently, the masking paper is required to be easily removed.
On the basis of the foregoing embodiments, further, the applying pressure to the preset number of photovoltaic modules includes:
and applying pressure to the photovoltaic modules in the preset number by adopting a cylindrical tool.
Specifically, it is right when presetting the photovoltaic module of quantity and exerting pressure, can adopt cylindrical frock, exert pressure to photovoltaic module through the drum frock, guaranteed bonding strength on the one hand, on the other hand can be better maintain unmanned aerial vehicle's pneumatic appearance. The cylindrical tool can be a cylinder with the diameter of 6 centimeters and the length of 30 centimeters.
Fig. 2 is a schematic structural diagram of a front side of a photovoltaic module of a monocoque solar unmanned aerial vehicle according to an embodiment of the present invention, and fig. 3 is a schematic structural diagram of a Back side of a photovoltaic module of a monocoque solar unmanned aerial vehicle according to an embodiment of the present invention, where as shown in fig. 2 and fig. 3, there are 9 ibc (indirect Back contact) solar cells laminated to form a photovoltaic module, the size of each cell is 125 mm in length, 125 mm in width, 160 μm in thickness, and an interval between two adjacent cells is 0.7 mm. In fig. 2, the front surface of the photovoltaic module 1 is pasted with the masking paper 2, and the outer side of the photovoltaic module 1 is exposed from the electrode 3. In fig. 2, a solid double-sided adhesive tape 4 is dispersedly adhered to the back surface of the photovoltaic module 1, and a solid double-sided adhesive tape 5 is adhered along the periphery of the back surface of the photovoltaic module 1. The following describes an implementation process of adhering a plurality of photovoltaic modules 1 to the wing surface of the monocoque solar unmanned aerial vehicle by using the photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention.
Firstly, a piece of textured paper 2 with the thickness of 50 microns and the width of 20 millimeters is bonded along the edge of the front side of the photovoltaic module 1, and the distance between the textured paper 2 and the edge of the front side of the photovoltaic module 1 is 1 millimeter. The textured paper 2 can effectively prevent the surface of the photovoltaic module 1 from being polluted by the sealant. And adhering a solid double-sided adhesive tape 5 with the thickness of 1 millimeter and the width of 6 millimeters along the back edge of the photovoltaic module 1, wherein the solid double-sided adhesive tape 5 is 1 millimeter away from the back edge of the photovoltaic module 1.5 solid double-sided adhesive tapes with the length of 12 mm, the width of 12 mm and the thickness of 1 mm can be adhered to the back surface of each IBC solar cell, and a solid double-sided adhesive tape with the length of 12 mm, the width of 12 mm and the thickness of 1 mm is adhered between two adjacent IBC solar cells. Adopt above-mentioned bonding mode under the condition of guaranteeing bonding strength, reduced the use of solid double faced adhesive tape, be favorable to alleviateing monocoque solar energy unmanned aerial vehicle's weight.
And secondly, cleaning up a preset area on the surface of the wing of the monocoque solar unmanned aerial vehicle, and spraying black insulating paint on the preset area on the surface of the wing. The laying positions of the photovoltaic modules 1 are divided in a preset area of the surface of the wing, and a polyimide insulating tape with the thickness of 60 microns is adhered to an area corresponding to the electrode 3 of each photovoltaic module 1.
And thirdly, detecting the voltage of each string of battery cells in each photovoltaic module 1 by using a voltmeter, and detecting the fragmentation condition of each string of battery cells by using EL (electroluminescence) testing equipment. And (4) carrying out the next step after all the photovoltaic modules 1 are detected normally, otherwise, replacing the photovoltaic modules 1 which are detected abnormally.
And fourthly, removing the release film of the solid double-sided adhesive tape 4 and the solid double-sided adhesive tape 5 on the back surface of each photovoltaic assembly 1, and controlling the distance between the adjacent photovoltaic assemblies by utilizing a distance control strip tool, wherein the distance between the adjacent photovoltaic assemblies 1 is 3 millimeters. And bonding the photovoltaic module 1 on a preset area of the surface of the wing. And then applying pressure to the front surface of each photovoltaic module 1 by using a cylindrical tool with the diameter of 6 cm and the length of 30 cm so as to ensure the bonding strength of the solid double-sided adhesive and maintain the aerodynamic shape of the wing surface.
And fifthly, after laying of all the photovoltaic modules 1 on the surface of the wing, detecting the voltage of each string of single batteries in each photovoltaic module 1 by using a voltmeter, and detecting the fragmentation condition of each string of single batteries by using EL (electro luminescence) testing equipment. And (4) carrying out the next step after all the photovoltaic modules 1 are detected normally, otherwise, replacing the photovoltaic modules 1 which are detected abnormally.
And sixthly, welding the electrodes of the adjacent photovoltaic modules 1, namely welding the overlapped parts of the electrodes of the adjacent photovoltaic modules 1 on the polyimide insulating film.
And seventhly, filling the gap between the adjacent photovoltaic modules 1 with sealant with the density of 2g/ml, so that the electrodes of the adjacent photovoltaic modules 1 are wrapped by the sealant, and keeping the height of the sealant consistent with the thickness of the photovoltaic modules 1 so as to maintain the aerodynamic shape of the surface of the wing.
And step eight, after the sealant is solidified, removing the masking paper on the front surface of each photovoltaic module 1.
The photovoltaic module laying method of the monocoque solar unmanned aerial vehicle provided by the embodiment of the invention is easy to realize in engineering and simple in operation steps. The photovoltaic module bonds the light weight that lays that can effectively reduce the material of double faced adhesive tape quality. Exert pressure through cylindrical frock to photovoltaic module, guaranteed bonding strength on the one hand, on the other hand better the pneumatic appearance that has maintained unmanned aerial vehicle. The electrodes are filled with the sealant after welding, so that the electrodes can be prevented from being oxidized on one hand, and the aerodynamic shape of the surface of the wing is maintained on the other hand. Through laying the quality detection to photovoltaic module around, can in time discover the photovoltaic module who goes wrong.
As will be appreciated by one skilled in the art, embodiments of the present invention may be provided as a method, system, or computer program product. Accordingly, the present invention may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present invention may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
The present invention is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the invention. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
In the description herein, reference to the description of the terms "one embodiment," "a particular embodiment," "some embodiments," "for example," "an example," "a particular example," or "some examples," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The above-mentioned embodiments are intended to illustrate the objects, technical solutions and advantages of the present invention in further detail, and it should be understood that the above-mentioned embodiments are only exemplary embodiments of the present invention, and are not intended to limit the scope of the present invention, and any modifications, equivalent substitutions, improvements and the like made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (10)
1. The utility model provides a method for laying photovoltaic module of monocoque solar unmanned aerial vehicle, which is characterized in that includes:
pasting a preset number of photovoltaic modules in a preset area on the surface of a wing of a solar unmanned aerial vehicle;
and applying pressure to the photovoltaic modules in the preset number so that the photovoltaic modules are firmly bonded with the surface of the wing.
2. The method of claim 1, further comprising, prior to affixing a predetermined number of photovoltaic modules to a predetermined area of the wing surface of the solar drone:
cleaning a preset area of the surface of the wing, and spraying insulating paint on the preset area of the surface of the wing.
3. The method of claim 1, further comprising, prior to affixing a predetermined number of photovoltaic modules to a predetermined area of the wing surface of the solar drone:
and adhering insulating adhesive tapes to the preset areas on the surface of the wing and the areas corresponding to the preset number of electrodes of the photovoltaic modules.
4. The method of claim 1, further comprising, prior to affixing a predetermined number of photovoltaic modules to a predetermined area of the wing surface of the solar drone:
and carrying out quality detection on the photovoltaic modules in the preset number.
5. The method of claim 1, further comprising:
and carrying out quality detection on the photovoltaic module after laying is completed.
6. The method of claim 1, further comprising:
and welding the electrodes of the adjacent photovoltaic modules.
7. The method of claim 1, further comprising:
and filling gaps between adjacent photovoltaic modules with sealant.
8. The method of claim 1, further comprising, prior to affixing a predetermined number of photovoltaic modules to a predetermined area of the wing surface of the solar drone:
and (4) sticking the masking paper along the edge face of the front side of each photovoltaic module.
9. The method of claim 8, further comprising:
and removing the masking paper adhered to the surface of each photovoltaic module.
10. The method according to any one of claims 1 to 9, wherein said applying pressure to said preset number of photovoltaic modules comprises:
and applying pressure to the photovoltaic modules in the preset number by adopting a cylindrical tool.
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204029830U (en) * | 2014-09-03 | 2014-12-17 | 江西日普升能源科技有限公司 | A kind of light and thin type crystal silicon solar photovoltaic module |
| CN104229120A (en) * | 2014-09-22 | 2014-12-24 | 北京航空航天大学 | Solar wing structure of aircraft based on photothermal integrated composite energy |
| KR20180004449A (en) * | 2016-07-04 | 2018-01-12 | 주식회사 한국과학모형 | Hard saling yacht which driven by natural wind and photovoltaic power |
| CN208285273U (en) * | 2018-05-28 | 2018-12-25 | 天津市文然科技有限公司 | Unmanned plane solar energy distance increasing unit |
| US20190260328A1 (en) * | 2018-02-20 | 2019-08-22 | Tesla, Inc. | Inter-tile support for solar roof tiles |
| CN209441681U (en) * | 2018-11-15 | 2019-09-27 | 上海太阳能工程技术研究中心有限公司 | A kind of near space unmanned plane semi-rigid solar cell array |
-
2019
- 2019-12-23 CN CN201911332898.1A patent/CN113035984A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204029830U (en) * | 2014-09-03 | 2014-12-17 | 江西日普升能源科技有限公司 | A kind of light and thin type crystal silicon solar photovoltaic module |
| CN104229120A (en) * | 2014-09-22 | 2014-12-24 | 北京航空航天大学 | Solar wing structure of aircraft based on photothermal integrated composite energy |
| KR20180004449A (en) * | 2016-07-04 | 2018-01-12 | 주식회사 한국과학모형 | Hard saling yacht which driven by natural wind and photovoltaic power |
| US20190260328A1 (en) * | 2018-02-20 | 2019-08-22 | Tesla, Inc. | Inter-tile support for solar roof tiles |
| CN208285273U (en) * | 2018-05-28 | 2018-12-25 | 天津市文然科技有限公司 | Unmanned plane solar energy distance increasing unit |
| CN209441681U (en) * | 2018-11-15 | 2019-09-27 | 上海太阳能工程技术研究中心有限公司 | A kind of near space unmanned plane semi-rigid solar cell array |
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