CN108001664A - A kind of hydrogen balloon - Google Patents
A kind of hydrogen balloon Download PDFInfo
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- CN108001664A CN108001664A CN201711276099.8A CN201711276099A CN108001664A CN 108001664 A CN108001664 A CN 108001664A CN 201711276099 A CN201711276099 A CN 201711276099A CN 108001664 A CN108001664 A CN 108001664A
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- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 title claims abstract description 43
- 229910052739 hydrogen Inorganic materials 0.000 title claims abstract description 43
- 239000001257 hydrogen Substances 0.000 title claims abstract description 43
- 238000012360 testing method Methods 0.000 claims description 56
- 238000001514 detection method Methods 0.000 claims description 12
- 238000012545 processing Methods 0.000 claims description 11
- 238000006243 chemical reaction Methods 0.000 claims description 9
- 238000000605 extraction Methods 0.000 claims description 6
- 238000012549 training Methods 0.000 claims description 6
- 238000007667 floating Methods 0.000 claims description 5
- 238000005259 measurement Methods 0.000 claims description 3
- 238000010248 power generation Methods 0.000 description 3
- 238000013528 artificial neural network Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/10—Combinations of wind motors with apparatus storing energy
- F03D9/11—Combinations of wind motors with apparatus storing energy storing electrical energy
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/30—Wind motors specially adapted for installation in particular locations
- F03D9/32—Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09F—DISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
- G09F21/00—Mobile visual advertising
- G09F21/06—Mobile visual advertising by aeroplanes, airships, balloons, or kites
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E70/00—Other energy conversion or management systems reducing GHG emissions
- Y02E70/30—Systems combining energy storage with energy generation of non-fossil origin
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Power Engineering (AREA)
- Sustainable Development (AREA)
- Business, Economics & Management (AREA)
- Marketing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- Accounting & Taxation (AREA)
- Studio Devices (AREA)
Abstract
The present invention provides a kind of hydrogen balloon, including：Balloon body, wind-driven generator and the base installed in the wind-driven generator foot guard, the balloon body connects the wind-driven generator by multigroup cable, the storage battery of the wind-driven generator is installed in the base, and the both ends of the wind-driven generator are hinged with advertising framework.Hydrogen balloon of the present invention is provided with wind-driven generator on base, can carry out the electric power storage of wind energy, and storage battery is arranged in base, can effectively utilize high altitude wind energy, improves the resource utilization of hydrogen balloon；Advertising framework can overturn with respect to wind-driven generator and open and fold, and overall structure is simple, easy to use.
Description
Technical field
The present invention relates to a kind of aircraft, more particularly to a kind of hydrogen balloon.
Background technology
In endoatmosphere, the aircraft of flight is known as aircraft, such as balloon, dirigible, aircraft.They are by the quiet floating of air
The air force lift-off flight that power or air relative motion produce.Wherein, the balloon as aircraft is to utilize quiet buoyancy support liter,
There is part also to drive its own movement using propulsive force, balloon includes the different types such as fire balloon, light balloon.Apply and navigating at present
Bat, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
Road, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, have greatly expanded the use of fire balloon and hydrogen balloon in itself
On the way, hydrogen balloon is more used for scientific research.
Some existing hydrogen balloon features are more single, do not carry out rationally profit to the wind energy in high-altitude residing for hydrogen balloon
With.
The content of the invention
(1) technical problems to be solved
The technical problem to be solved in the present invention is to provide a kind of wind-driven generator that is provided with to carry out wind energy electric power storage, advertisement branch
Frame is hinged on the hydrogen balloon of generator both sides.
(2) technical solution
In order to solve the above technical problems, the present invention provides a kind of hydrogen balloon, including：Balloon body, wind-driven generator and
Installed in the base of the wind-driven generator foot guard, the balloon body connects the wind power generation by multigroup cable
Machine, the storage battery of the wind-driven generator are installed in the base, and the both ends of the wind-driven generator are hinged with advertising framework.
Further, further include：Wind-force measuring apparatus, is arranged on the base, is currently located for detecting hydrogen balloon
The instant wind-force size of air position；Inclination angle identification equipment, is arranged on the base, flies in the air for detecting hydrogen balloon
When current flight posture pitch angle；Embedded processing equipment, is arranged on the base, respectively with the wind-force measuring apparatus
And inclination angle identification equipment connection, for based on the instant wind-force size received by the pitching of the current flight posture
The pitch angle that the instant wind-force size that angle is adjusted to and receives matches；Aerial photography equipment, is arranged on below the base,
Towards ground, base lower images collection is carried out to ground environment for when hydrogen balloon declines, starting, to obtain and export bottom
Seat lower images；
Further, further include：
Subregion detection device, is arranged on the base, is connected with the Aerial photography equipment, for receiving the bottom
Seat lower images, determine the signal-to-noise ratio of each subject area in base lower images, and based on each in base lower images
The signal-to-noise ratio of a subject area determines the current signal of whole base lower images；
Amount of images determines equipment, is connected with the subregion detection device, for low in the current signal received
When equal to predetermined lower threshold value, selection and the test image of current signal corresponding number test quantity as default, currently
Signal-to-noise ratio is lower, and the quantity of test image is more, and is additionally operable to be higher than predetermined lower threshold value in the current signal received
When, the test image of fixed qty is selected as default test quantity；
Color space conversion equipment, determines that equipment is connected with described image quantity, for each type scene, chooses default
The image of quantity is tested as test image, the test image of all types scene is all transformed into YUV color spaces to obtain
Multiple test color images；
Size adjusting equipment, is connected with color space conversion equipment, for receiving the multiple test color image, to institute
State multiple test color images and perform normalized respectively to obtain multiple standard testing images of fixed dimension；
Feature amount selecting device, is connected with the size adjusting equipment and the subregion detection device, according to current respectively
Signal-to-noise ratio determines the input quantity type of the model of selection, and the input quantity type according to selection carries out each standard testing image
Feature extraction meets input quantity type, the corresponding test feature amount of the standard testing image of selection to obtain, wherein, currently
Signal-to-noise ratio is lower, and the corresponding data processing amount of input quantity type of the model of selection is more；
Model measurement equipment, is connected with the feature amount selecting device, corresponding each for receiving each standard testing image
A test feature amount, each test feature amount is respectively outputted to complete the test of model parameter in model, wherein, model bag
Input layer, hidden layer and output layer are included, the output quantity of the output layer is standard testing image and the matching for presetting photography scene
Degree；
Model performs equipment, is connected respectively with the feature amount selecting device and the subregion detection device, for receiving
Base lower images, to base lower images successively YUV color space conversions, normalized and input quantity according to selection
The feature extraction of type meets input quantity type, the corresponding identification feature amount of the base lower images of selection to obtain, will
Input of the corresponding identification feature amount of the base lower images as the input layer of model after training, to pass through model after training
The output quantity of output layer obtains the base lower images and the matching degree of default photography scene, when the matching with default photography scene
When degree is more than or equal to preset matching threshold value, scene identification signal is sent；
Wherein, the embedded processing equipment also performs equipment with the model and is connected, for receiving the scene
During identification signal, the decrease speed of hydrogen balloon is adjusted until hydrogen balloon reaches floating state；The model performs equipment and is additionally operable to
When the matching degree with default photography scene is less than preset matching threshold value, the unidentified signal of scene is sent.
(3) beneficial effect
Hydrogen balloon of the present invention is provided with wind-driven generator on base, can carry out the electric power storage of wind energy, and storage battery is arranged on
In base, high altitude wind energy can be effectively utilized, improves the resource utilization of hydrogen balloon；Advertising framework can be with respect to wind power generation
Machine upset is opened and folded, and overall structure is simple, easy to use.
Brief description of the drawings
Fig. 1 is the structure diagram of hydrogen balloon of the present invention；
Fig. 2 is the structure diagram of hydrogen balloon equipment room of the present invention；
Wherein：1 it is balloon body, 2 be wind-driven generator, 3 be base, 4 be cable, 5 is advertising framework.
Embodiment
Refering to Fig. 1 and Fig. 2, the present invention provides a kind of hydrogen balloon, including：Balloon body 1, wind-driven generator 2 and installation
In the base 3 of 2 foot guard of wind-driven generator, balloon body 1 connects wind-driven generator 2, wind power generation by multigroup cable 4
The storage battery of machine 2 is installed in base 3, and the both ends of wind-driven generator 2 are hinged with advertising framework 5.
The present embodiment hydrogen balloon is provided with wind-driven generator on base, can carry out the electric power storage of wind energy, and storage battery is set
In base, high altitude wind energy can be effectively utilized, improves the resource utilization of hydrogen balloon；Advertising framework can be sent out with respect to wind energy
Motor overturning is opened and folded, and overall structure is simple, easy to use.
Hydrogen balloon swims in overhead, is widely used in shooting, advertisement promotion etc..Currently, it is desirable to hydrogen balloon energy
It is enough to slowly enter stable floating state when reaching ground soon, so as to the various operations such as be rescued, be followed the trail of, be shot, so
And some existing hydrogen balloons lack effective hovering means, there is the technical problem that cannot be introduced into hovering pattern, operate
It is too urgent that hydrogen balloon flight can be caused unstable or even ground can be hit.Therefore, further included refering to Fig. 2, the present embodiment：
Wind-force measuring apparatus, set on the base 3, for detect hydrogen balloon be currently located air position instant wind-force it is big
It is small；
Inclination angle identification equipment, is set on the base 3, and current flight posture bows during for detecting hydrogen balloon flight in the air
The elevation angle；
Embedded processing equipment, sets on the base 3, is connected respectively with wind-force measuring apparatus and inclination angle identification equipment,
Instant wind-force for the pitch angle of current flight posture to be adjusted to and received based on the instant wind-force size received is big
The small pitch angle to match；
Aerial photography equipment, is arranged on the lower section of base 3, towards ground, for when hydrogen balloon declines, starting face ring over the ground
Border carries out base lower images collection, to obtain and export base lower images；
Subregion detection device, sets on the base 3, is connected with Aerial photography equipment, for receiving base lower images,
Determine the signal-to-noise ratio of each subject area in base lower images, and based on each object region in base lower images
Signal-to-noise ratio determines the current signal of whole base lower images；
Amount of images determines equipment, is connected with subregion detection device, for the current signal received less than etc.
When predetermined lower threshold value, selection and the test image of current signal corresponding number test quantity, current noise as default
Than lower, the quantity of test image is more, and is additionally operable to when the current signal received is higher than predetermined lower threshold value, choosing
The test image of fixed qty is selected as default test quantity；
Color space conversion equipment, determines that equipment is connected with amount of images, for each type scene, chooses default test
It is multiple to obtain all to be transformed into YUV color spaces as test image by the image of quantity for the test image of all types scene
Test color image；
Size adjusting equipment, is connected with color space conversion equipment, for receiving multiple test color images, to multiple surveys
Examination color image performs normalized to obtain multiple standard testing images of fixed dimension respectively；
Feature amount selecting device, is connected with size adjusting equipment and subregion detection device respectively, true according to current signal
Determine the input quantity type of the model of selection, the input quantity type according to selection carries out feature extraction to each standard testing image
To obtain the input quantity type, the corresponding test feature amount of the standard testing image that meet selection, wherein, current signal is got over
Low, the corresponding data processing amount of input quantity type of the model of selection is more；
Model measurement equipment, is connected with feature amount selecting device, for receiving the corresponding each survey of each standard testing image
Characteristic quantity is tried, each test feature amount is respectively outputted to complete the test of model parameter in model, wherein, model includes defeated
Enter layer, hidden layer and output layer, the output quantity of output layer is standard testing image and the matching degree for presetting photography scene；
Model performs equipment, is connected respectively with feature amount selecting device and subregion detection device, for receiving below base
Image, to the spy of base lower images successively YUV color space conversions, normalized and input quantity type according to selection
Sign extraction meets input quantity type, the corresponding identification feature amount of the base lower images of selection to obtain, by under the base
Input of the corresponding identification feature amount of square image as the input layer of model after training, to pass through the output layer of model after training
Output quantity obtains the base lower images and the matching degree of default photography scene, when the matching degree with default photography scene is more than etc.
When preset matching threshold value, scene identification signal is sent；
Wherein, embedded processing equipment also performs equipment with model and is connected, for when receiving scene identification signal, adjusting
The decrease speed of whole hydrogen balloon is until hydrogen balloon reaches floating state；Model performs equipment and is additionally operable to work as and default photography scene
When matching degree is less than preset matching threshold value, the unidentified signal of scene is sent.
The present embodiment realizes that hydrogen balloon is slow from rapidly dropping to by the identification of the shooting scene based on deep neural network
Slowly the switching hovered, improves the quality of shooting image.Corresponding image recognition pattern is determined based on the corresponding signal-to-noise ratio of image,
So that the image of low signal-to-noise ratio, the identifying processing operation of acquisition is finer, while the identification of the image of high s/n ratio is simplified,
Accelerate the speed of identifying processing operation；Signal-to-noise ratio based on each object region in image determines the current noise of whole image
Than improving the efficiency that signal noise ratio (snr) of image judges；By the identification of the shooting scene based on deep neural network, hydrogen balloon is realized
From the switching slowly hovered is rapidly dropped to, the quality of shooting image is improved.
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, without departing from the technical principles of the invention, some improvements and modifications can also be made, these improvements and modifications
Also it should be regarded as protection scope of the present invention.
Claims (3)
- A kind of 1. hydrogen balloon, it is characterised in that including：Balloon body (1), wind-driven generator (2) and installed in the wind energy The base (3) of generator (2) foot guard, the balloon body (1) connect the wind-driven generator by multigroup cable (4) (2), the storage battery of the wind-driven generator (2) is installed in the base (3), and the both ends of the wind-driven generator (2) are hinged There is advertising framework (5).
- 2. hydrogen balloon as claimed in claim 1, it is characterised in that further include：Wind-force measuring apparatus, is arranged on the base (3) on, the instant wind-force size of air position is currently located for detecting hydrogen balloon；Inclination angle identification equipment, is arranged on the bottom On seat (3), the pitch angle of current flight posture during for detecting hydrogen balloon flight in the air；Embedded processing equipment, is arranged on On the base (3), it is connected respectively with the wind-force measuring apparatus and the inclination angle identification equipment, for based on receiving What the instant wind-force size that the pitch angle of the current flight posture is adjusted to and received by instant wind-force size matched bows The elevation angle；Aerial photography equipment, is arranged on below the base (3), towards ground, for when hydrogen balloon declines, starting over the ground Face ring border carries out base lower images collection, to obtain and export base lower images；
- 3. hydrogen balloon as claimed in claim 2, it is characterised in that further include：Subregion detection device, is arranged on the base (3), is connected with the Aerial photography equipment, for receiving the bottom Seat lower images, determine the signal-to-noise ratio of each subject area in base lower images, and based on each in base lower images The signal-to-noise ratio of a subject area determines the current signal of whole base lower images；Amount of images determines equipment, is connected with the subregion detection device, for the current signal received less than etc. When predetermined lower threshold value, selection and the test image of current signal corresponding number test quantity, current noise as default Than lower, the quantity of test image is more, and is additionally operable to when the current signal received is higher than predetermined lower threshold value, choosing The test image of fixed qty is selected as default test quantity；Color space conversion equipment, determines that equipment is connected with described image quantity, for each type scene, chooses default test It is multiple to obtain all to be transformed into YUV color spaces as test image by the image of quantity for the test image of all types scene Test color image；Size adjusting equipment, is connected with color space conversion equipment, for receiving the multiple test color image, to described more A test color image performs normalized to obtain multiple standard testing images of fixed dimension respectively；Feature amount selecting device, is connected with the size adjusting equipment and the subregion detection device, according to current noise respectively Than the input quantity type of the model of definite selection, the input quantity type according to selection carries out feature to each standard testing image Extraction meets input quantity type, the corresponding test feature amount of the standard testing image of selection to obtain, wherein, current noise Than lower, the corresponding data processing amount of input quantity type of the model of selection is more；Model measurement equipment, is connected with the feature amount selecting device, for receiving the corresponding each survey of each standard testing image Characteristic quantity is tried, each test feature amount is respectively outputted to complete the test of model parameter in model, wherein, model includes defeated Enter layer, hidden layer and output layer, the output quantity of the output layer is standard testing image and the matching degree for presetting photography scene；Model performs equipment, is connected respectively with the feature amount selecting device and the subregion detection device, for receiving base Lower images, to base lower images successively YUV color space conversions, normalized and input quantity type according to selection Feature extraction to obtain input quantity type, the corresponding identification feature amount of the base lower images of selection of meeting, by the bottom Input of the corresponding identification feature amount of seat lower images as the input layer of model after training, to pass through the output of model after training The output quantity of layer obtains the base lower images and the matching degree of default photography scene, when big with the matching degree of default photography scene When equal to preset matching threshold value, scene identification signal is sent；Wherein, the embedded processing equipment also performs equipment with the model and is connected, for receiving the scene identification During signal, the decrease speed of hydrogen balloon is adjusted until hydrogen balloon reaches floating state；The model perform equipment be additionally operable to when with When the matching degree of default photography scene is less than preset matching threshold value, the unidentified signal of scene is sent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711276099.8A CN108001664A (en) | 2017-12-06 | 2017-12-06 | A kind of hydrogen balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711276099.8A CN108001664A (en) | 2017-12-06 | 2017-12-06 | A kind of hydrogen balloon |
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| CN108001664A true CN108001664A (en) | 2018-05-08 |
Family
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| CN201711276099.8A Pending CN108001664A (en) | 2017-12-06 | 2017-12-06 | A kind of hydrogen balloon |
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Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS51121641A (en) * | 1975-04-16 | 1976-10-25 | Mitsui Eng & Shipbuild Co Ltd | A floating balloon type wind power generator |
| KR20020023769A (en) * | 2001-12-17 | 2002-03-29 | 현 용 이 | Anemometer using an ad-balloon |
| US20070120005A1 (en) * | 2005-11-28 | 2007-05-31 | Olson Gaylord G | Aerial wind power generation system |
| CN101830279A (en) * | 2010-05-28 | 2010-09-15 | 朱明华 | Optical and air energies complementary aerial airship |
| CN203422914U (en) * | 2013-07-05 | 2014-02-05 | 天津市汇津广告有限公司 | Hydrogen balloon advertising board |
| CN203544367U (en) * | 2012-10-11 | 2014-04-16 | 张高义雄 | Multifunctional high-altitude balloon |
| CN104061125A (en) * | 2013-03-19 | 2014-09-24 | 宋少如 | Balloon, airship and lifting kite aerial power generating device |
| CN205400998U (en) * | 2016-03-10 | 2016-07-27 | 东莞前沿技术研究院 | Wind energy electricity device and have aerostatics of this wind energy electricity device |
| CN106275410A (en) * | 2016-11-17 | 2017-01-04 | 湖南科瑞特科技股份有限公司 | A kind of wind disturbance resistant unmanned plane |
-
2017
- 2017-12-06 CN CN201711276099.8A patent/CN108001664A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS51121641A (en) * | 1975-04-16 | 1976-10-25 | Mitsui Eng & Shipbuild Co Ltd | A floating balloon type wind power generator |
| KR20020023769A (en) * | 2001-12-17 | 2002-03-29 | 현 용 이 | Anemometer using an ad-balloon |
| US20070120005A1 (en) * | 2005-11-28 | 2007-05-31 | Olson Gaylord G | Aerial wind power generation system |
| CN101830279A (en) * | 2010-05-28 | 2010-09-15 | 朱明华 | Optical and air energies complementary aerial airship |
| CN203544367U (en) * | 2012-10-11 | 2014-04-16 | 张高义雄 | Multifunctional high-altitude balloon |
| CN104061125A (en) * | 2013-03-19 | 2014-09-24 | 宋少如 | Balloon, airship and lifting kite aerial power generating device |
| CN203422914U (en) * | 2013-07-05 | 2014-02-05 | 天津市汇津广告有限公司 | Hydrogen balloon advertising board |
| CN205400998U (en) * | 2016-03-10 | 2016-07-27 | 东莞前沿技术研究院 | Wind energy electricity device and have aerostatics of this wind energy electricity device |
| CN106275410A (en) * | 2016-11-17 | 2017-01-04 | 湖南科瑞特科技股份有限公司 | A kind of wind disturbance resistant unmanned plane |
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Application publication date: 20180508 |