CN106150915A - High-altitude wind power generation system based on unmanned aerial vehicle platform - Google Patents
High-altitude wind power generation system based on unmanned aerial vehicle platform Download PDFInfo
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- CN106150915A CN106150915A CN201610515873.5A CN201610515873A CN106150915A CN 106150915 A CN106150915 A CN 106150915A CN 201610515873 A CN201610515873 A CN 201610515873A CN 106150915 A CN106150915 A CN 106150915A
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- 238000010248 power generation Methods 0.000 title claims abstract description 37
- 230000033228 biological regulation Effects 0.000 claims description 6
- 230000007423 decrease Effects 0.000 claims description 5
- 229910003460 diamond Inorganic materials 0.000 claims description 3
- 239000010432 diamond Substances 0.000 claims description 3
- 238000010276 construction Methods 0.000 abstract description 3
- 238000013461 design Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 208000027418 Wounds and injury Diseases 0.000 abstract description 2
- 230000006378 damage Effects 0.000 abstract description 2
- 208000014674 injury Diseases 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 8
- 230000005611 electricity Effects 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 5
- 230000000630 rising effect Effects 0.000 description 3
- 230000009194 climbing Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 238000013473 artificial intelligence Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/90—Mounting on supporting structures or systems
- F05B2240/92—Mounting on supporting structures or systems on an airbourne structure
-
- 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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/30—Wind power
-
- 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
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
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Abstract
The present invention provides high-altitude wind power generation system based on unmanned aerial vehicle platform, comprising: be arranged on the electromotor on ground；Big aerofoil high-lift high lift-drag ratio unmanned vehicle, it drives described electrical power generators.The present invention directly utilizes aircraft and aloft collects wind energy, eliminates the huge control tower of construction, is substantially reduced structure design difficulty and manufacturing cost；Owing to aircraft can drop to ground, can carry out on ground so installing and safeguarding, therefore can be substantially reduced the difficulty installed and safeguard；Can be regained when meeting with the vile weather such as typhoon, thus wall blower fan is exposed in the hazard weathers such as typhoon the loss that is subject to, the anti-disaster ability of raising system and service life；High altitude wind machine wind wheel size is little or does not has wind wheel, it is also possible to reduce the injury to birds.
Description
Technical field
The invention belongs to electricity generation system field, be specifically related to a kind of high-altitude wind power generation system based on unmanned aerial vehicle platform.
Background technology
Wind energy, as the regenerative resource of a kind of cleaning, is more and more paid attention to by people.High-altitude wind power generation is a kind of
Novel Wind Power Utilization mode, it is exactly high for there is many advantages, the most significant advantage compared with conventional fan
Contain huge wind energy content in the air.
Along with the development of the modern technology such as unmanned vehicle, Based Intelligent Control, high-altitude wind power generation promises to be the most very much
Reality.Emerge the high-altitude wind power generation system of various ways in recent years, paid close attention to by increasing research institution and company,
Related Technical Issues therein has become the study hotspot of contemporary scientific and engineering field.
But high-altitude wind power generation is a kind of novel Wind Power Utilization technology, we can not apply mechanically existing tradition wind completely
The electricity generating principle of power machine, needs based on aerodynamic principle, in combination with material, control, communicate, the aspect such as artificial intelligence
Emerging technology, carries out concept innovation to high altitude wind energy Application way, designs new high-altitude wind power generation system, improves Wind Power Utilization
Efficiency also reduces cost of electricity-generating.
Summary of the invention
Present invention solves the technical problem that and be: be inefficient for existing level axle wind turbine power generation, set based on unmanned plane
Meter Novel high-altitude wind generator system, it is achieved efficient wind-power electricity generation ability.
The technical scheme is that
High-altitude wind power generation system based on unmanned aerial vehicle platform, comprising:
It is arranged on the electromotor on ground；
Big aerofoil high-lift high lift-drag ratio unmanned vehicle, it drives described electrical power generators.Aircraft is with in large angles of attack
Rising flight, aircraft drag rope drives electrical power generators；Changing attitude after arriving certain altitude to dive downwards, electromotor reclaims
Rope, now needs to consume some energy；Upwards climb when changing attitude again after the downward certain distance of airplane nose down, repeat generating
Process.The electric energy of airplane nose down process consumption much smaller than the process of climbing generated electricity can, thus whole process reach generating effect.
Preferably, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, big aerofoil high-lift promotion hinders
Connected by pull rope than between unmanned vehicle and electromotor；The gesture stability of aircraft is by with aircraft front and back ends even
The drag rope connect realizes, and property simple and reliable for structure is strong.
The front-end and back-end of described big aerofoil high-lift high lift-drag ratio unmanned vehicle are respectively fixed with the first angle of attack regulation
Rope and second angle of attack regulation rope.
Preferably, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift is high
The flight path of lift-drag ratio unmanned vehicle is straight line.The flight path of aircraft have selected linear reciprocation track, it is to avoid many
Interfering between the aircraft of platform high casement wind-driven generator, reduces every Fans to spatial domain and the demand of occupation of land.
Preferably, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift is high
Angle between flight path and the horizontal plane of lift-drag ratio unmanned vehicle is 47 °, makes whole system achieve the highest wind
Can utilization ratio.
Preferably, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift is high
Lift-drag ratio unmanned vehicle speed uplink is 0.4～0.45 times of wind speed, and decrease speed is wind speed 1～2 times.
Preferably, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift is high
Lift-drag ratio unmanned vehicle assumes diamond in shape, and wing chord length root slightly ratio is for 10, and spanwise length is 2 times of root chord length.Aircraft layout
Select big aerofoil, big thickness, high-lift, high lift-drag ratio Flying-wing scheme, can efficiently utilize wind energy and there is good knot
Structure intensity.
Preferably, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, each cross section of wing is selected same
Plant aerofoil profile, be EPPLER399 aerofoil profile.
Present invention advantage compared with prior art is: 1, wind-resources aspect, along with terrain clearance increases wind energy content
Increase, the decades of times even Radix Achyranthis Bidentatae of Near Ground can be reached in high altitude wind energy density, the distribution of high altitude wind energy simultaneously also with I
There is natural coupling in the electricity consumption general layout of state；2, construction aspect, owing to the speed of upper-level winds is more much larger than ground, this means that wants
The wind energy of capture equal-wattage, wind wheel need not be made so big, and high altitude wind machine directly utilizes aircraft and aloft receives simultaneously
Collection wind energy, eliminates the huge control tower of construction, and these can be substantially reduced structure design difficulty and manufacturing cost；3, maintenance is installed
Aspect, owing to aircraft can drop to ground, can carry out on ground so installing and safeguarding, therefore can be substantially reduced
The difficulty installed and safeguard；4, anti-disaster ability aspect, can be regained when meeting with the vile weathers such as typhoon, thus wall blower fan
It is exposed in the hazard weathers such as typhoon the loss being subject to, improves anti-disaster ability and the service life of system；5, this external environment side
Face, high altitude wind machine wind wheel size is little or does not has wind wheel, it is also possible to reduce the injury to birds.
Part is embodied by the further advantage of the present invention, target and feature by description below, and part also will be by this
Invention research and practice and be understood by the person skilled in the art.
Accompanying drawing explanation
When Fig. 1 is in propradation for the high-altitude wind power generation system flight device based on unmanned aerial vehicle platform that the present invention provides
Schematic diagram；
When Fig. 2 is in decline state for the high-altitude wind power generation system flight device based on unmanned aerial vehicle platform that the present invention provides
Schematic diagram；
Aircraft layout signal in the high-altitude wind power generation system based on unmanned aerial vehicle platform that Fig. 3 provides for the present invention
Figure；
Aircraft manufacturing technology in the high-altitude wind power generation system based on unmanned aerial vehicle platform that Fig. 4 provides for the present invention shows
It is intended to；
In the high-altitude wind power generation system based on unmanned aerial vehicle platform that Fig. 5 provides for the present invention, track angle is Cp when 47 °
Distribution isogram.
Detailed description of the invention
The present invention is described in further detail below in conjunction with the accompanying drawings, to make those skilled in the art with reference to description literary composition
Word can be implemented according to this.
Should be appreciated that used herein such as " have ", " comprising " and " including " term do not allot one or many
Other element individual or the existence of a combination thereof or interpolation.
As depicted in figs. 1 and 2, the present invention provides a kind of high-altitude wind power generation system based on unmanned aerial vehicle platform, comprising:
It is arranged on the electromotor 1 on ground；
Big aerofoil high-lift high lift-drag ratio unmanned vehicle 2, it drives described electromotor 1 to generate electricity.
In described high-altitude wind power generation system based on unmanned aerial vehicle platform, big aerofoil high-lift high lift-drag ratio unmanned flight
Connected by pull rope 3 between device 2 and electromotor 1；
As shown in Figure 4, the front-end and back-end of described big aerofoil high-lift high lift-drag ratio unmanned vehicle 2 are respectively fixed with
One angle of attack regulation rope 4 and second angle of attack regulation rope 5.
In described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift high lift-drag ratio is unmanned
The flight path of aircraft is straight line.
In described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift high lift-drag ratio is unmanned
Angle between flight path and the horizontal plane of aircraft is 47 °.
In described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift high lift-drag ratio is unmanned
Aircraft speed uplink is 0.4～0.45 times of wind speed, and decrease speed is wind speed 1～2 times.
As it is shown on figure 3, in described high-altitude wind power generation system based on unmanned aerial vehicle platform, described big aerofoil high-lift is high
Lift-drag ratio unmanned vehicle 2 assumes diamond in shape, and wing chord length root slightly ratio is for 10, and spanwise length is 2 times of root chord length.
In described high-altitude wind power generation system based on unmanned aerial vehicle platform, same aerofoil profile is selected in each cross section of wing, all
For EPPLER399 aerofoil profile.The placement scheme of aircraft have employed Flying-wing, and Flying-wing has high-lift, high lift-drag ratio, knot
The advantages such as structure intensity is good, are highly suitable for high altitude wind power generator.Whole aircraft is a big rhombus, wing chord length root
Slightly ratio is for 10, and the span is 2 times of root chord length.
The technical solution of the present invention is: be placed on ground by electromotor, uses flivver to drive.Aircraft is to attack more greatly
Angle upward flight, aircraft drag rope drives electrical power generators；After arriving certain altitude, change attitude dive downwards, electromotor
Reclaim rope, now need to consume some energy；Upwards climb when changing attitude again after the downward certain distance of airplane nose down, repeat
Power generation process.The electric energy of airplane nose down process consumption much smaller than the process of climbing generated electricity can, thus whole process reach generating imitate
Really.This system is mainly made up of two parts: 1, big aerofoil high-lift high lift-drag ratio unmanned vehicle；2, generator section is placed on ground
Point.
Same aerofoil profile has been selected in each cross section of wing, is EPPLER399 aerofoil profile, and this aerofoil profile has high-lift, height equally
The feature of lift-drag ratio.Relative thickness is the biggest simultaneously, is so more suitable for increasing the structural strength of whole wing.
For the ease of controlling, reducing interfering between land used and aircraft, flight path linearly goes up simultaneously
Rise, change attitude after rising to peak, dive according to the path contrary with rising trace.
Attitude of flight vehicle is controlled to rely on the length changing two ropes being joined directly together with aircraft to realize: when
When needing to reduce aircraft angle of attack, reclaim the rope being connected with aircraft front end, discharge the rope being connected with aircraft rear end simultaneously；
When needs increase aircraft angle of attack, perform inverse operation, the rope that release is connected with aircraft front end, reclaim and aircraft simultaneously
The rope that rear end is connected.
From fig. 5, it can be seen that when the flight path of aircraft selects the rectilinear flight track horizontal by 47 degree of angles, on
Line speed is 0.4～0.45 times of wind speed, and decrease speed is wind speed 1～when 2 times, whole system Wind Power Utilization within the complete period
Efficiency can reach more than 0.25.
Although embodiment of the present invention are disclosed as above, but it is not restricted in description and embodiment listed
Using, it can be applied to various applicable the field of the invention completely, for those skilled in the art, and can be easily
Realizing other amendment, therefore under the general concept limited without departing substantially from claim and equivalency range, the present invention does not limit
In specific details with shown here as the legend with description.
Claims (7)
1. high-altitude wind power generation system based on unmanned aerial vehicle platform, it is characterised in that including:
It is arranged on the electromotor on ground；
Big aerofoil high-lift high lift-drag ratio unmanned vehicle, it drives described electrical power generators.
2. high-altitude wind power generation system based on unmanned aerial vehicle platform as claimed in claim 1, it is characterised in that big aerofoil promotion
Connected by pull rope between power high lift-drag ratio unmanned vehicle and electromotor；
The front-end and back-end of described big aerofoil high-lift high lift-drag ratio unmanned vehicle be respectively fixed with first the angle of attack regulation rope and
Second angle of attack regulation rope.
3. high-altitude wind power generation system based on unmanned aerial vehicle platform as claimed in claim 1, it is characterised in that described big aerofoil
The flight path of high-lift high lift-drag ratio unmanned vehicle is straight line.
4. high-altitude wind power generation system based on unmanned aerial vehicle platform as claimed in claim 1, it is characterised in that described big aerofoil
Angle between flight path and the horizontal plane of high-lift high lift-drag ratio unmanned vehicle is 47 °.
5. high-altitude wind power generation system based on unmanned aerial vehicle platform as claimed in claim 1, it is characterised in that described big aerofoil
High-lift high lift-drag ratio unmanned vehicle speed uplink is 0.4～0.45 times of wind speed, and decrease speed is wind speed 1～2 times.
6. high-altitude wind power generation system based on unmanned aerial vehicle platform as claimed in claim 1, it is characterised in that described big aerofoil
High-lift high lift-drag ratio unmanned vehicle assumes diamond in shape, and wing chord length root slightly ratio is for 10, and spanwise length is 2 times of root chord length.
7. high-altitude wind power generation system based on unmanned aerial vehicle platform as claimed in claim 1, it is characterised in that each cross section of wing
Select same aerofoil profile, be EPPLER399 aerofoil profile.
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| CN201610515873.5A CN106150915B (en) | 2016-07-01 | 2016-07-01 | High-altitude wind power generation system based on unmanned aerial vehicle platform |
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| CN201610515873.5A CN106150915B (en) | 2016-07-01 | 2016-07-01 | High-altitude wind power generation system based on unmanned aerial vehicle platform |
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| CN106150915B CN106150915B (en) | 2020-06-23 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106949012A (en) * | 2017-05-24 | 2017-07-14 | 南安市智德机械设备有限公司 | A kind of suspended wind turbine |
| CN108061013A (en) * | 2017-12-06 | 2018-05-22 | 天津大学 | Portable sea complex energy transformation platform |
| CN108061011A (en) * | 2017-12-06 | 2018-05-22 | 天津大学 | Marine unmanned plane wind power generation platform |
| CN110318931A (en) * | 2019-05-24 | 2019-10-11 | 中国航天空气动力技术研究院 | A kind of flying wing structure for underwater power generation |
| CN111911349A (en) * | 2020-08-20 | 2020-11-10 | 武汉大学 | High-altitude wind power generation system based on dynamic balance flapping wings |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2119451B (en) * | 1982-04-28 | 1985-07-10 | Cognitronics Corp | Apparatus for extracting energy from winds at high altitudes |
| JPH05296137A (en) * | 1992-04-16 | 1993-11-09 | Mitsui Eng & Shipbuild Co Ltd | Wind power generating facility |
| CN101289991A (en) * | 2008-03-25 | 2008-10-22 | 胡世曦 | High altitude wind power generator |
| US20100013226A1 (en) * | 2008-07-18 | 2010-01-21 | Honeywell International Inc. | Tethered Autonomous Air Vehicle With Wind Turbines |
| US20100032963A1 (en) * | 2005-05-03 | 2010-02-11 | Ferguson Frederick D | Systems and methods for tethered wind turbines |
| CN202186516U (en) * | 2011-03-03 | 2012-04-11 | 唐耀辉 | High-altitude combined power-generating device |
| US20130307274A1 (en) * | 2012-04-26 | 2013-11-21 | Yik Hei Sia | Power Generating Windbags and Waterbags |
-
2016
- 2016-07-01 CN CN201610515873.5A patent/CN106150915B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2119451B (en) * | 1982-04-28 | 1985-07-10 | Cognitronics Corp | Apparatus for extracting energy from winds at high altitudes |
| JPH05296137A (en) * | 1992-04-16 | 1993-11-09 | Mitsui Eng & Shipbuild Co Ltd | Wind power generating facility |
| US20100032963A1 (en) * | 2005-05-03 | 2010-02-11 | Ferguson Frederick D | Systems and methods for tethered wind turbines |
| CN101289991A (en) * | 2008-03-25 | 2008-10-22 | 胡世曦 | High altitude wind power generator |
| US20100013226A1 (en) * | 2008-07-18 | 2010-01-21 | Honeywell International Inc. | Tethered Autonomous Air Vehicle With Wind Turbines |
| CN202186516U (en) * | 2011-03-03 | 2012-04-11 | 唐耀辉 | High-altitude combined power-generating device |
| US20130307274A1 (en) * | 2012-04-26 | 2013-11-21 | Yik Hei Sia | Power Generating Windbags and Waterbags |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106949012A (en) * | 2017-05-24 | 2017-07-14 | 南安市智德机械设备有限公司 | A kind of suspended wind turbine |
| CN106949012B (en) * | 2017-05-24 | 2018-10-19 | 南安市智德机械设备有限公司 | A kind of suspended wind turbine |
| CN108061013A (en) * | 2017-12-06 | 2018-05-22 | 天津大学 | Portable sea complex energy transformation platform |
| CN108061011A (en) * | 2017-12-06 | 2018-05-22 | 天津大学 | Marine unmanned plane wind power generation platform |
| CN110318931A (en) * | 2019-05-24 | 2019-10-11 | 中国航天空气动力技术研究院 | A kind of flying wing structure for underwater power generation |
| CN111911349A (en) * | 2020-08-20 | 2020-11-10 | 武汉大学 | High-altitude wind power generation system based on dynamic balance flapping wings |
| CN111911349B (en) * | 2020-08-20 | 2021-12-03 | 武汉大学 | High-altitude wind power generation system based on dynamic balance flapping wings |
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| CN106150915B (en) | 2020-06-23 |
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