CN104044741B - A kind of carry out solar energy tracking unmanned plane and fill can process - Google Patents
A kind of carry out solar energy tracking unmanned plane and fill can process Download PDFInfo
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- CN104044741B CN104044741B CN201410289374.XA CN201410289374A CN104044741B CN 104044741 B CN104044741 B CN 104044741B CN 201410289374 A CN201410289374 A CN 201410289374A CN 104044741 B CN104044741 B CN 104044741B
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Abstract
A kind of unmanned plane carrying out solar energy tracking, comprise unmanned aerial vehicle body, main rotating machine, permanent seat, light-inductive device, convertible solar panel, cell panel fixed frame, sideway swivel motor, fixed mount, lift cylinder and wing, unmanned aerial vehicle body there is main rotating machine, permanent seat is fixed in the rotating shaft of main rotating machine, convertible solar panel is in a row fixed in cell panel fixed frame, there is sideway swivel motor cell panel fixed frame both sides, the rotating shaft of sideway swivel motor is fixed in the middle part of cell panel fixed frame side, lift cylinder is had below the fixed mount of cell panel fixed frame both sides, lift cylinder is fixed on permanent seat, permanent seat there are 4 light-inductive devices.The convertible solar panel of unmanned plane top solar energy tracking mechanism of the present invention sets in a row and can overturn simultaneously, horizontal surface rotates and is then controlled by main rotating machine, thus can collect solar power to greatest extent, and cost is more cheap, installs more convenient.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of carry out solar energy tracking unmanned plane and fill can process.
Background technology
Unmanned plane is the not manned aircraft utilizing radio telecommand or the process controller provided for oneself to handle, along with the continuous progress of science and technology, the development of unmanned air vehicle technique is more and more ripe, use more and more extensive, not only can be used for battle reconnaissance and supervision, positioning school are penetrated, injured the military missions such as assessment, electronic warfare, but also oneself is as target drone, also can be used for civilian, as border patrol, nuclear radiation detection, aerial photography, mineral exploration aviation, the condition of a disaster supervision, traffic patrolling, security monitoring etc.
Unmanned plane is due to needs Function Extension, just must improve overall flying power, therefore flying power is very big to its performance impact, the mode improving unmanned plane flying power at present preferably the wing of unmanned plane is made solar panel or lay solar panel on wing, wing is made solar panel and often need very large area, cost is very high, and on wing, lay solar panel can affect flight, therefore best at present mode installs solar collecting device additional on fuselage, but owing to being subject to body restriction, the solar panels that can install are limited, therefore in order to improve continuation of the journey effect, just solar energy tracking device must be used.
Current domestic patent has the patent No. to be that CN201210373741.5 name is called solar power unmanned plane, adopt solar energy tracking technology as illustrated in fig. 1 and 2, but there are the following problems for it, first each cell panel of this application is assembled aboard by tracking equipment respectively, such cost is high, installation difficulty is large, if solar panel is installed overstocked, easily interfere with each other, affect solar energy collecting effect, and because unmanned plane major part is flown on high, and solar panel is aboard, therefore strong wind is run into or this mode solar panel of other inclement weathers is especially easily damaged, and when taking off and land or when performing special duty, aircraft flight speed be there are certain requirements, now this mode solar panel can affect flight.
Summary of the invention
For above problem, the invention provides a kind of carry out solar energy tracking unmanned plane and fill can process, the convertible solar panel of this unmanned plane top solar energy tracking mechanism sets in a row, overturn by sideway swivel electric machine control, horizontal surface rotates and is then controlled by main rotating machine, thus can collect solar power to greatest extent, more cheap relative to single upset solar panels design organization cost, install more convenient, for reaching this object, the invention provides a kind of unmanned plane carrying out solar energy tracking, comprise unmanned aerial vehicle body, main rotating machine, permanent seat, light-inductive device, convertible solar panel, cell panel fixed frame, sideway swivel motor, fixed mount, lift cylinder and wing, there is wing described unmanned aerial vehicle body both sides, described unmanned aerial vehicle body there is main rotating machine, described permanent seat is fixed in the rotating shaft of main rotating machine, described permanent seat there are at least 2 cell panel fixed frames, described convertible solar panel is in a row fixed in cell panel fixed frame, there is sideway swivel motor described cell panel fixed frame both sides, the rotating shaft of described sideway swivel motor is fixed in the middle part of cell panel fixed frame side, described sideway swivel motor is fixed in the through hole of fixed mount by connecting element, lift cylinder is had below the fixed mount of described cell panel fixed frame both sides, described fixed mount is fixed on lift cylinder expansion link end, described lift cylinder is fixed on permanent seat, described permanent seat there are 4 light-inductive devices, described light-inductive device angularly around permanent seat center one week.
As a further improvement on the present invention, described permanent seat there is groove, described lift cylinder is fixed in the groove on permanent seat, because lift cylinder itself can take certain altitude, therefore preferably lift cylinder is fixed in the groove on permanent seat, convertible solar panel can be packed up as much as possible like this, reduce flight impact.
As a further improvement on the present invention, described permanent seat there is cell panel standing groove, described cell panel standing groove is below cell panel fixed frame, convertible solar panel can be received in it after cell panel standing groove is set, can further prevent solar panel to be destroyed like this or reduce the impact on flight.
As a further improvement on the present invention, described wing is equipped with wing formula solar panel, and by the solar power collected and solar energy tracking collect to solar power together with power for unmanned plane.
As a further improvement on the present invention, described permanent seat is rectangle or circle, and when permanent seat is that the convertible solar panel that rectangle can be arranged is more, and permanent seat is that the circular impact on flight is less, and producer can select according to unmanned plane actual conditions.
As a further improvement on the present invention, described unmanned aerial vehicle body and permanent seat all adopt the ultralight height of the boron carbide B4C particle reinforce obtained by film metallurgical forming technique to make than strong magnesium lithium Mg-Li based composites, this quality of materials is extremely light, therefore unmanned plane overall weight can greatly be alleviated, and it can obtain tiny grain structure after cold rolling, yield strength ratio as-cast structure is high by 50%, stiffness-to-density ratio comparatively business aluminum alloy and titanium alloy high by 22%, therefore greatly can improve the bulk strength of unmanned plane.
As a further improvement on the present invention, described unmanned aerial vehicle body and the outside all plated films of permanent seat have the ferromagnetic material Mn-Zn of nanoparticle, the nano wave-absorption composite material that Ni-Zn ferrite and ferroelectric BaTiO3 are composited, due to the critical function that investigation early warning is unmanned plane, very high to stealthy Capability Requirement when being therefore used in these fields, and although solar panel can be packed up by the present invention, but still easily investigated by enemy radar, unmanned plane is in order to stealthy, surface coating adopts the ferromagnetic material Mn-Zn of the nanoparticle developed voluntarily, Ni-Zn ferrite and ferroelectric BaTiO3 compound, the coating-type nano wave-absorption composite material formed, thus greatly can improve the overall absorbing property of unmanned plane.
The present invention is a kind of carry out filling of the unmanned plane of solar energy tracking can process, specifically fill can process as follows:
1) stopped status is in when aircraft is not in state of flight, optimum illumination direction and lighting angle is judged by light-inductive device, permanent seat is driven to rotate to optimum orientation by main rotating machine, rotated to best angle by the convertible solar panel of sideway swivel driven by motor, the result of not being completely cured according to light-inductive device gained adjusts permanent seat direction and convertible solar panel, can effect to reach that the best fills;
2) take off or landing state when aircraft is in, during owing to taking off or landing, airshed is larger, in order to prevent air-flow, damage is caused to convertible solar panel, when taking off or land, convertible solar panel turn to parallel with permanent seat end face by sideway swivel motor, lift cylinder expansion link declines, and drives convertible solar panel in cell panel standing groove, causes damage to prevent rising or down gust to convertible solar panel;
3) when aircraft is in state of flight, light-inductive device senses that its light intensity is not high, and under being in cloudy day or inclement weather conditions, convertible solar panel is driven in cell panel standing groove by lift cylinder;
4) when aircraft is in state of flight, light-inductive device senses that light is in fine day state, convertible solar panel is risen by lift cylinder expansion link, optimum illumination direction and lighting angle is judged by light-inductive device, permanent seat is driven to rotate to optimum orientation by main rotating machine, rotated to best angle by the convertible solar panel of sideway swivel driven by motor, the result of not being completely cured according to light-inductive device gained adjusts permanent seat direction and convertible solar panel, can effect to reach that the best fills.
As a further improvement on the present invention, when aircraft is in state of flight, light-inductive device senses that light is in fine day state, time aircraft exceeds usual speed flight or aircraft execution special duty, convertible solar panel is driven in cell panel standing groove by lift cylinder, due to significantly although solar energy collecting can be improved after convertible solar panel rise, but can have an impact to flying speed, therefore when aircraft is for self needing carry out hypervelocity flight or perform scouting, border patrol, had better be packed up as required when the special dutys such as the condition of a disaster supervision.
The invention provides a kind of carry out solar energy tracking unmanned plane and fill can process, this unmanned plane top is provided with solar energy tracking mechanism, controlled to rotate by main rotating machine, then often arrange convertible solar panel to be overturn by sideway swivel electric machine control, solar power is collected effective relative to integrated overturn, more cheap relative to single upset cost, install more convenient, in addition permanent seat of the present invention there is cell panel standing groove, lift cylinder is provided with bottom convertible solar panel both sides motor fixing frame in a row, run into cloudy day or extraordinary circumstances convertible solar panel to be received in cell panel standing groove by lift cylinder, run into inclement weather like this, solar panel is also less likely to occur to damage, in addition unmanned plane wing of the present invention is equipped with wing formula solar panel, and power because it mainly contains solar energy tracking cell panel, wing is auxiliary power supply, therefore not high to wing area designing requirement, thus greatly can reduce the design difficulty of wing, in addition the present invention devises according to solar elevation and azimuth situation and unmanned plane moving law that fill accordingly can process, thus unmanned plane solar energy collecting efficiency can be improved to greatest extent, and unmanned plane flying power.
Accompanying drawing explanation
Fig. 1 is prior art schematic diagram;
Fig. 2 is prior art partial schematic diagram;
Fig. 3 is constructional drawing of the present invention;
Fig. 4 is lateral plan of the present invention;
Fig. 5 is local structural graph of the present invention;
Component in figure is:
1, unmanned aerial vehicle body; 2, main rotating machine; 3, permanent seat;
4, light-inductive device; 5, convertible solar panel; 6, cell panel fixed frame;
7, cell panel standing groove; 8, sideway swivel motor; 9, fixed mount;
10, lift cylinder; 11, connecting element; 12, wing;
13, wing formula solar panel.
Detailed description of the invention
Below in conjunction with accompanying drawing and example, the present invention is described in detail:
The invention provides a kind of carry out solar energy tracking unmanned plane and fill can process, the convertible solar panel of this unmanned plane top solar energy tracking mechanism sets in a row, overturn by sideway swivel electric machine control, horizontal surface rotates and is then controlled by main rotating machine, thus can collect solar power to greatest extent, relative to single upset solar panels, mechanism cost is more cheap, installs more convenient.
As a kind of example of the present invention, the invention provides a kind of unmanned plane carrying out solar energy tracking, comprise unmanned aerial vehicle body 1, main rotating machine 2, permanent seat 3, light-inductive device 4, convertible solar panel 5, cell panel fixed frame 6, sideway swivel motor 8, fixed mount 9, lift cylinder 10 and wing 12, there is wing 12 described unmanned aerial vehicle body 1 both sides, described unmanned aerial vehicle body 1 there is main rotating machine 2, described permanent seat 3 is fixed in the rotating shaft of main rotating machine 2, described permanent seat 3 there are at least 2 cell panel fixed frames 6, described convertible solar panel 5 is in a row fixed in cell panel fixed frame 6, there is sideway swivel motor 8 described cell panel fixed frame 6 both sides, the rotating shaft of described sideway swivel motor 8 is fixed in the middle part of cell panel fixed frame 6 side, described sideway swivel motor 8 is fixed on by connecting element 11 in the through hole of fixed mount 9, lift cylinder 10 is had below the fixed mount 9 of described cell panel fixed frame 6 both sides, described fixed mount 9 is fixed on lift cylinder 10 expansion link end, described lift cylinder 10 is fixed on permanent seat 3, described permanent seat 3 there are 4 light-inductive devices 4, described light-inductive device 4 angularly around permanent seat 3 center one week.
As a kind of best instantiation of the present invention, the invention provides constructional drawing as Fig. 3, a kind of unmanned plane carrying out solar energy tracking shown in Fig. 4 and Fig. 5, comprise unmanned aerial vehicle body 1, main rotating machine 2, permanent seat 3, light-inductive device 4, convertible solar panel 5, cell panel fixed frame 6, sideway swivel motor 8, fixed mount 9, lift cylinder 10 and wing 12, there is wing 12 described unmanned aerial vehicle body 1 both sides, described wing 12 is equipped with wing formula solar panel 13, in order to more a step raising continuation of the journey effect can be equipped with wing formula solar panel collection solar power on wing, and by the solar power collected and solar energy tracking collect to solar power together with power for unmanned plane, described unmanned aerial vehicle body 1 there is main rotating machine 2, described permanent seat 3 is fixed in the rotating shaft of main rotating machine 2, described permanent seat 3 is circular, when permanent seat is that the convertible solar panel that rectangle can be arranged is more, and permanent seat is that the circular impact on flight is less, producer can select according to unmanned plane practical use, described permanent seat 3 there are as shown in Figure 2 at least 2 cell panel fixed frames 6, described convertible solar panel 5 is in a row fixed in cell panel fixed frame 6, there is sideway swivel motor 8 described cell panel fixed frame 6 both sides, the rotating shaft of described sideway swivel motor 8 is fixed in the middle part of cell panel fixed frame 6 side, described sideway swivel motor 8 is fixed on by connecting element 11 in the through hole of fixed mount 9, lift cylinder 10 is had below the fixed mount 9 of described cell panel fixed frame 6 both sides, described fixed mount 9 is fixed on lift cylinder 10 expansion link end, described permanent seat 3 there is groove, described lift cylinder 10 is fixed in the groove on permanent seat 3, because lift cylinder itself can take certain altitude, therefore preferably lift cylinder is fixed in the groove on permanent seat, convertible solar panel can be packed up as much as possible like this, reduce flight impact, described permanent seat 3 there is cell panel standing groove 7, described cell panel standing groove 7 is below cell panel fixed frame 6, convertible solar panel can be received in it after cell panel standing groove is set, can further prevent solar panel to be destroyed like this or reduce the impact on flight, described permanent seat 3 there are 4 light-inductive devices 4, described light-inductive device 4 angularly around permanent seat 3 center one week.
Unmanned aerial vehicle body of the present invention and permanent seat all adopt the ultralight height of the boron carbide B4C particle reinforce obtained by film metallurgical forming technique to make than strong magnesium lithium Mg-Li based composites, this material weight is extremely light, therefore unmanned plane overall weight can greatly be alleviated, and it can obtain tiny grain structure after cold rolling, yield strength ratio as-cast structure is high by 50%, stiffness-to-density ratio comparatively business aluminum alloy and titanium alloy high by 22%, therefore the bulk strength of unmanned plane can greatly be improved, described unmanned aerial vehicle body and the outside all plated films of permanent seat have the ferromagnetic material Mn-Zn of nanoparticle, the material that Ni-Zn ferrite and ferroelectric BaTiO3 are composited, due to the critical function that investigation early warning is unmanned plane, very high to stealthy Capability Requirement when being therefore used in these fields, and although solar panel can be packed up by the present invention, but still easily investigated by enemy radar, therefore unmanned plane of the present invention is in order to the stealthy ferromagnetic material Mn-Zn needing surface coating to adopt the nanoparticle developed voluntarily, Ni-Zn ferrite and ferroelectric BaTiO3 compound, be formed with coating-type nano wave-absorption composite material, thus greatly can improve the overall absorbing property of unmanned plane.
The present invention is a kind of carry out filling of the unmanned plane of solar energy tracking can process, specifically fill can process as follows:
1) stopped status is in when aircraft is not in state of flight, optimum illumination direction and lighting angle is judged by light-inductive device 4, permanent seat 3 is driven to rotate to optimum orientation by main rotating machine 2, convertible solar panel 5 is driven to rotate to best angle by sideway swivel motor 8, be not completely cured according to the result of light-inductive device 4 gained, permanent seat 3 direction and convertible solar panel 5 are adjusted, fills energy effect to reach the best;
2) take off or landing state when aircraft is in, during owing to taking off or landing, airshed is larger, in order to prevent air-flow, damage is caused to convertible solar panel 5, when taking off or land, convertible solar panel 5 turn to parallel with permanent seat 3 end face by sideway swivel motor 8, lift cylinder 10 expansion link declines and drives in convertible solar panel 5 to cell panel standing groove 7, causes damage to prevent rising or down gust to convertible solar panel 5;
3) when aircraft is in state of flight, light-inductive device 4 senses that its light intensity is not high, and under being in cloudy day or inclement weather conditions, convertible solar panel 5 drives in cell panel standing groove 7 by lift cylinder 10;
4) when aircraft is in state of flight, light-inductive device 4 senses that light is in fine day state, convertible solar panel 5 is risen by lift cylinder 10 expansion link, optimum illumination direction and lighting angle is judged by light-inductive device 4, permanent seat 3 is driven to rotate to optimum orientation by main rotating machine 2, convertible solar panel 5 is driven to rotate to best angle by sideway swivel motor 8, be not completely cured according to the result of light-inductive device 4 gained, permanent seat 3 direction and convertible solar panel 5 are adjusted, fills energy effect to reach the best.
Wherein when aircraft is in state of flight, light-inductive device 4 senses that light is in fine day state, if time aircraft exceeds usual speed flight or aircraft execution special duty, convertible solar panel 5 drives in cell panel standing groove 7 by lift cylinder 10, due to significantly although solar energy collecting can be improved after convertible solar panel rise, but can have an impact to flying speed, therefore when aircraft is for self needing had better be packed up as required when carrying out hypervelocity flight or perform the special dutys such as scouting, border patrol, the condition of a disaster supervision.
The above is only preferred embodiments of the present invention, is not restriction the present invention being made to any other form, and any amendment done according to technical spirit of the present invention or equivalent variations, still belong to the present invention's scope required for protection.
Claims (9)
1. one kind can be carried out the unmanned plane of solar energy tracking, comprise unmanned aerial vehicle body (1), main rotating machine (2), permanent seat (3), light-inductive device (4), convertible solar panel (5), cell panel fixed frame (6), sideway swivel motor (8), fixed mount (9), lift cylinder (10) and wing (12), there is wing (12) described unmanned aerial vehicle body (1) both sides, it is characterized in that: described unmanned aerial vehicle body (1) has main rotating machine (2), described permanent seat (3) is fixed in the rotating shaft of main rotating machine (2), described permanent seat (3) there are at least 2 cell panel fixed frames (6), described convertible solar panel (5) is in a row fixed in cell panel fixed frame (6), there is sideway swivel motor (8) described cell panel fixed frame (6) both sides, the rotating shaft of described sideway swivel motor (8) is fixed in the middle part of cell panel fixed frame (6) side, described sideway swivel motor (8) is fixed in the through hole of fixed mount (9) by connecting element (11), there is lift cylinder (10) fixed mount (9) below of described cell panel fixed frame (6) both sides, described fixed mount (9) is fixed on lift cylinder (10) expansion link end, described lift cylinder (10) is fixed on permanent seat (3), described permanent seat (3) there are 4 light-inductive devices (4), described light-inductive device (4) angularly around permanent seat (3) center one week.
2. a kind of unmanned plane carrying out solar energy tracking according to claim 1, is characterized in that: (3) have groove with described permanent seat, and described lift cylinder (10) is fixed in the groove on permanent seat (3).
3. a kind of unmanned plane carrying out solar energy tracking according to claim 1, is characterized in that: described permanent seat (3) has cell panel standing groove (7), and described cell panel standing groove (7) is in cell panel fixed frame (6) below.
4. a kind of unmanned plane carrying out solar energy tracking according to claim 1, is characterized in that: described wing (12) top is equipped with wing formula solar panel (13).
5. a kind of unmanned plane carrying out solar energy tracking according to claim 1, is characterized in that: described permanent seat (3) is rectangle or circle.
6. a kind of unmanned plane carrying out solar energy tracking according to claim 1, is characterized in that: described unmanned aerial vehicle body (1) and permanent seat (3) all adopt the ultralight height of the boron carbide B4C particle reinforce obtained by film metallurgical forming technique to make than strong magnesium lithium Mg-Li based composites.
7. a kind of unmanned plane carrying out solar energy tracking according to claim 6, is characterized in that: the nano wave-absorption composite material that described unmanned aerial vehicle body (1) and the outside all plated films of permanent seat (3) have ferromagnetic material Mn-Zn, Ni-Zn ferrite of nanoparticle and ferroelectric BaTiO3 to be composited.
8. a kind of according to claim 1-7 any one carries out filling of the unmanned plane of solar energy tracking can process, specifically fill can process as follows, it is characterized in that:
1) stopped status is in when aircraft is not in state of flight, optimum illumination direction and lighting angle is judged by light-inductive device (4), permanent seat (3) is driven to rotate to optimum orientation by main rotating machine (2), convertible solar panel (5) is driven to rotate to best angle by sideway swivel motor (8), the result of not being completely cured according to light-inductive device (4) gained adjusts permanent seat (3) direction and convertible solar panel (5), can effect to reach that the best fills;
2) take off or landing state when aircraft is in, during owing to taking off or landing, airshed is larger, in order to prevent air-flow, damage is caused to convertible solar panel (5), when taking off or land, convertible solar panel (5) turn to parallel with permanent seat (3) end face by sideway swivel motor (8), lift cylinder (10) expansion link declines and drives convertible solar panel (5) in cell panel standing groove (7), causes damage to prevent rising or down gust to convertible solar panel (5);
3) when aircraft is in state of flight, light-inductive device (4) senses that its light intensity is not high, and under being in cloudy day or inclement weather conditions, convertible solar panel (5) is driven in cell panel standing groove (7) by lift cylinder (10);
4) when aircraft is in state of flight, light-inductive device (4) senses that light is in fine day state, convertible solar panel (5) is risen by lift cylinder (10) expansion link, optimum illumination direction and lighting angle is judged by light-inductive device (4), permanent seat (3) is driven to rotate to optimum orientation by main rotating machine (2), convertible solar panel (5) is driven to rotate to best angle by sideway swivel motor (8), the result of not being completely cured according to light-inductive device (4) gained adjusts permanent seat (3) direction and convertible solar panel (5), energy effect is filled to reach the best.
9. according to claim 8 a kind of carry out filling of the unmanned plane of solar energy tracking can process, it is characterized in that: when aircraft is in state of flight, light-inductive device (4) senses that light is in fine day state, time aircraft exceeds usual speed flight or aircraft execution special duty, convertible solar panel (5) is driven in cell panel standing groove (7) by lift cylinder (10).
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|---|---|---|---|---|
| GB2528489A (en) | 2014-07-23 | 2016-01-27 | Cassidian Ltd | Improvements in and relating to unmanned aerial vehicles |
| CN104267737B (en) * | 2014-09-22 | 2017-07-14 | 北京航空航天大学 | One kind can be to day solar battery quadrotor |
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| CN109094791B (en) * | 2018-08-13 | 2020-12-11 | 合肥凯石投资咨询有限公司 | Unmanned aerial vehicle with carry formula solar array on back |
| CN108990915A (en) * | 2018-09-11 | 2018-12-14 | 中国水产科学研究院淡水渔业研究中心 | A kind of quick finishing device of fishery |
| CN111959791B (en) * | 2020-08-26 | 2022-02-18 | 海南中橡科技有限公司 | Spout medicine unmanned aerial vehicle with long duration |
| CN112224424A (en) * | 2020-10-19 | 2021-01-15 | 拓航科技有限公司 | Be applied to electric power and patrol and examine unmanned aerial vehicle's photovoltaic charging panel |
| CN113978693A (en) * | 2021-10-22 | 2022-01-28 | 中国电子科技集团公司第十八研究所 | Solar unmanned aerial vehicle with drawable surface power generation skin and power supply method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7270295B2 (en) * | 2004-04-30 | 2007-09-18 | The Regents Of The University Of California | Solar thermal aircraft |
| US7559506B2 (en) * | 2005-09-14 | 2009-07-14 | Kissel Jr Waldemar F | Integral powered wing aircraft |
| CN102837826A (en) * | 2012-10-02 | 2012-12-26 | 李万红 | Solar unmanned aerial vehicle |
| CN203078752U (en) * | 2012-12-28 | 2013-07-24 | 东莞职业技术学院 | Novel sightseeing airplane |
| CN203581381U (en) * | 2013-11-27 | 2014-05-07 | 南京傲翼伟滕自动化科技有限公司 | Improved multi-rotor unmanned aerial vehicle |
| CN203902841U (en) * | 2014-06-26 | 2014-10-29 | 金陵科技学院 | Unmanned aerial vehicle capable of performing solar energy tracking |
-
2014
- 2014-06-26 CN CN201410289374.XA patent/CN104044741B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7270295B2 (en) * | 2004-04-30 | 2007-09-18 | The Regents Of The University Of California | Solar thermal aircraft |
| US7559506B2 (en) * | 2005-09-14 | 2009-07-14 | Kissel Jr Waldemar F | Integral powered wing aircraft |
| CN102837826A (en) * | 2012-10-02 | 2012-12-26 | 李万红 | Solar unmanned aerial vehicle |
| CN203078752U (en) * | 2012-12-28 | 2013-07-24 | 东莞职业技术学院 | Novel sightseeing airplane |
| CN203581381U (en) * | 2013-11-27 | 2014-05-07 | 南京傲翼伟滕自动化科技有限公司 | Improved multi-rotor unmanned aerial vehicle |
| CN203902841U (en) * | 2014-06-26 | 2014-10-29 | 金陵科技学院 | Unmanned aerial vehicle capable of performing solar energy tracking |
Non-Patent Citations (1)
| Title |
|---|
| 太阳能模型飞机的设计方法研究;刘畅，陈公牧，李路，王超，谢福林;《飞机设计》;20131031;第33卷(第5期);第18-20、26页 * |
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| Publication number | Publication date |
|---|---|
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