JPH04350369A - High-altitude wind power generation - Google Patents
High-altitude wind power generationInfo
- Publication number
- JPH04350369A JPH04350369A JP3121020A JP12102091A JPH04350369A JP H04350369 A JPH04350369 A JP H04350369A JP 3121020 A JP3121020 A JP 3121020A JP 12102091 A JP12102091 A JP 12102091A JP H04350369 A JPH04350369 A JP H04350369A
- Authority
- JP
- Japan
- Prior art keywords
- mooring
- wind power
- lanyard
- airship
- ground
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000010248 power generation Methods 0.000 title claims abstract description 8
- 230000005540 biological transmission Effects 0.000 claims abstract description 11
- 238000010586 diagram Methods 0.000 description 6
- 238000004804 winding Methods 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000012528 membrane Substances 0.000 description 2
- 239000000615 nonconductor Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000010292 electrical insulation Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- 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
Abstract
Description
【0001】0001
【産業上の利用分野】本発明は風力発電の改良に関する
ものである。FIELD OF THE INVENTION This invention relates to improvements in wind power generation.
【0002】0002
【従来の技術】周知の通り風力発電は、地上叉は海上に
設置されるのが原則で、今までの実績は、ほとんど地上
である。実際は海上の方が風力条件も良いのであるが、
設置のための、オプション技術や環境の不整備のためで
あろう。また風速の絶対値自身が小さく、しかも、その
値が一定せず、変動の多いものであつた。このため経済
性も悪く、小規模にとどまり発達していない。BACKGROUND OF THE INVENTION As is well known, wind power generation is generally installed on land or on the sea, and most of the results to date have been on land. In reality, the wind conditions are better at sea,
This is probably due to inadequate optional technology and environment for installation. Furthermore, the absolute value of the wind speed itself was small, and moreover, the value was not constant and varied widely. For this reason, it is not economically viable and remains small and undeveloped.
【0003】0003
【発明が解決しようとする課題】上述した如く、低空の
風力エネルギーが、小さくて変動が多いので、これを高
空の、偏西風の吹く高度に求めるもので、最近の熱気球
による、九州宮崎からカナダの北部に達する横断飛行で
は、10780Kmの距離を48時間で、平均時速22
5Kmで飛行し、最高時速は300Kmにも達したよう
である。この風力は主として、地球の自転と、コリオリ
ーの加速度によるものとされ、変動のない安定なエネル
ギーである。しかし、このような高空の風力エネルギー
を如何にして利用するかは大きな問題である。[Problem to be Solved by the Invention] As mentioned above, wind energy at low altitudes is small and fluctuates a lot, so it is necessary to obtain this energy at high altitudes where westerly winds blow. A cross-country flight reaching the northern part of the country covered a distance of 10,780 km in 48 hours at an average speed of 22
It seems that it flew at a speed of 5 km and reached a maximum speed of 300 km. This wind power is mainly caused by the Earth's rotation and Coriolis acceleration, and is stable energy that does not fluctuate. However, how to utilize such high-altitude wind energy is a big problem.
【0004】0004
【課題を解決するための手段】本発明は、高空に浮かぶ
飛行船またはクライダーに、風力発電機を取り付け、こ
れを繋留する繋留索を、発電した電力の送電線として共
用するものであり、日本の太平洋に向かう海岸線沿つて
多数上昇せしめるのである。この場合風力発電の問題の
一つとされる、発電プロペラによる騒音公害も、遠く離
れた洋上の上空であるため解消される。このような方式
では、風力エネルギーが大きいため、ユニット当たりの
出力は、最低でも千キロワツト、大型では万キロワツト
も見込めるし、かつ変動の少ない風力であるので、経済
性も達成される。[Means for Solving the Problems] The present invention is to attach a wind power generator to an airship or crider floating at high altitude, and to share the mooring cables that moor it together as a power transmission line for the generated electric power. Many of them will rise along the coastline towards the Pacific Ocean. In this case, noise pollution caused by power generation propellers, which is considered to be one of the problems associated with wind power generation, is also eliminated because it is located far away over the ocean. In this type of system, since the wind energy is large, the output per unit can be expected to be at least 1,000 kilowatts, or even 10,000 kilowatts for large units, and since the wind power has little fluctuation, it is also economical.
【0005】[0005]
【実施例】次に、本発明について図面を参照して説明す
る。図1は本発明の第1の実施例の構造図である。1は
飛行船本体であり、普通の飛行船と同様な構造でよい。
すなわち軟式、硬式のいずれでもよい。2はプロペラと
、発電機よりなる風力発電機である。普通の飛行船では
、エンジンと推進プロペラとなるものである。これは飛
行船本体1の周囲や全長にわたり多数設ける。本発明で
は、飛行船にかかる荷重は繋留索のみで燃料や、貨客が
ない点が特色であり、風力発電機2はエンジンプロペラ
より、自由に多数設けられる可能性がある。3は繋留索
である。これは送電線を兼ねるものとし、絶縁された二
線か、同心円状ケーブルなどを使用する。4は浮力バル
ーンであり、繋留索3の周囲に同心状に取り付けてある
。これは必ずしも、このような構成とする必要はなく、
浮力バルーンを別個の球体としてもよい。このようなバ
ルーンには、水素やヘリームのような軽い気体を入れて
浮力を生じせしめる。この補助浮力装置により、繋留索
3の荷重を軽減するのである。5は繋留索巻き取り装置
であり、本発明を地上に降下せしめて、点検、補修する
に際して繋留索3を巻き取るものであり、同時に地上に
固定する定点であり、繋留索3の張力に耐えるよう地上
に設定する。また、これは風力発電の送電端となり、地
上の送電線と連結される。6は尾翼であつて、飛行船の
姿勢の安定化に役立たせる。DESCRIPTION OF THE PREFERRED EMBODIMENTS Next, the present invention will be explained with reference to the drawings. FIG. 1 is a structural diagram of a first embodiment of the present invention. 1 is the airship body, which may have the same structure as a normal airship. In other words, it may be either a soft type or a hard type. 2 is a wind power generator consisting of a propeller and a generator. In a normal airship, this would be the engine and propeller. A large number of these are provided around the airship body 1 and along its entire length. The present invention is characterized in that the load on the airship is only the mooring cables and no fuel or passengers, and a larger number of wind power generators 2 than engine propellers may be provided. 3 is a tether. This will also serve as a power transmission line, and will use two insulated wires or a concentric cable. A buoyancy balloon 4 is attached concentrically around the tether 3. This does not necessarily have to be a configuration like this,
The buoyancy balloon may be a separate sphere. These balloons are filled with a light gas such as hydrogen or helium to create buoyancy. This auxiliary buoyancy device reduces the load on the tether 3. Reference numeral 5 denotes a tethering rope winding device, which winds up the tethering rope 3 when the present invention is lowered to the ground for inspection and repair, and at the same time is a fixed point for fixing to the ground, and is capable of withstanding the tension of the tethering rope 3. Set it on the ground. This will also serve as the transmission end for wind power generation and will be connected to the above-ground power transmission line. 6 is the tail, which helps stabilize the attitude of the airship.
【0006】図2は本発明の第2の実施例の構造図であ
る。7はグライダー主翼であり、高空の毎時300Km
にも達する風速により、揚力を生じて浮遊する。2はプ
ロペラと発電機よりなる風力発電機である。これは航空
機のエンジンと同様に、グライダーの主翼の前端に取り
付ける。3は繋留索であり、これにより高速気流中の定
点に保持され、相対速度によりグライダー主翼7に揚力
を生じる。4は浮力バルーンであり、繋留索3の周囲に
同心状に取り付けてある。これらは前実施例の飛行船の
場合と同様である。5も同様に繋留索巻き取り装置であ
る。8はグライダーの胴体であり、6は尾翼である。こ
の場合は凧のように空中に浮かぶだけであるので大きな
作用はないが、尾翼6により姿勢が安定化される。この
グライダー型では、点検や補修のため降下せしめる時、
一部の風力発電機を電動機とし地上に降下せしめること
が出来る。ただし、このときは地上より電力を、逆に供
給してやる必要がある。FIG. 2 is a structural diagram of a second embodiment of the present invention. 7 is the glider main wing, 300km/h at high altitude
Wind speeds that reach up to 100% create lift and cause it to float. 2 is a wind power generator consisting of a propeller and a generator. It is attached to the front end of the glider's wing, similar to an aircraft engine. Reference numeral 3 denotes a tethering cable, which holds the glider at a fixed point in the high-speed airflow and generates lift on the glider main wing 7 due to its relative speed. A buoyancy balloon 4 is attached concentrically around the tether 3. These are the same as in the case of the airship in the previous embodiment. Similarly, 5 is a tether winding device. 8 is the body of the glider, and 6 is the tail. In this case, the tail fin 6 stabilizes the attitude, although there is no major effect since it simply floats in the air like a kite. With this glider type, when descending for inspection or repair,
Some wind power generators can be used as electric motors to lower them to the ground. However, in this case, it is necessary to supply electricity from the ground.
【0007】図3は二心型の繋留索を示し、図4は同心
型の繋留索を示す。9、10、11、12が送電線で、
導電性、引張強度、軽量性が望まれ、新素材の利用も考
えられる。13は電気絶縁物であるが、やはり引張強度
が望ましく、ガラス繊維など、電気絶縁性と引張強度を
兼ね備えたものが適当である。4は浮力バルーンであり
、繋留索3の荷重を支えるよう、両端のみならず中間で
も、索や膜で送電線と浮力バルーン膜間を相互に連絡す
る。内部には水素やヘリウムなど軽い気体を封入する。FIG. 3 shows a two-core type tether, and FIG. 4 shows a concentric type tether. 9, 10, 11, 12 are power lines,
Conductivity, tensile strength, and lightness are desired, and the use of new materials is also considered. Reference numeral 13 is an electrical insulator, which preferably has tensile strength, and a material that has both electrical insulation and tensile strength, such as glass fiber, is suitable. Reference numeral 4 denotes a buoyancy balloon, which connects the power transmission line and the buoyancy balloon membrane not only at both ends but also in the middle with cables and membranes so as to support the load of the tether 3. A light gas such as hydrogen or helium is sealed inside.
【0008】[0008]
【発明の効果】以上説明したように、本発明では風力の
安定して豊富な高空で風力発電するため、経済性が高く
、環境汚染や騒音公害もなく、地球規模でエネルギー問
題の解決の一方法となる可能性がある。[Effects of the Invention] As explained above, the present invention generates wind power at high altitudes where wind power is stable and plentiful, so it is highly economical, does not cause environmental pollution or noise pollution, and is one of the solutions to energy problems on a global scale. This could be a method.
【図1】本発明による飛行船型高空風力発電機の構造図
である。FIG. 1 is a structural diagram of an airship-type high-altitude wind power generator according to the present invention.
【図2】本発明によるグライダー型高空風力発電機の構
造図である。FIG. 2 is a structural diagram of a glider-type high-altitude wind power generator according to the present invention.
【図3】本発明による飛行船またはグライダーの二心型
繋留索の構造図である。FIG. 3 is a structural diagram of a two-core tether cable for an airship or glider according to the present invention;
【図4】本発明による飛行船またはグライダーの同心型
繋留索の構造図である。FIG. 4 is a structural diagram of a concentric tether for an airship or glider according to the present invention;
1 飛行船本体 2 風力発電機 3 繋留索 4 浮力バルーン 5 繋留索巻き取り装置 6 尾翼 7 グライダー主翼 8 胴体 9 送電線 10 送電線 11 送電線 12 送電線 13 電気絶縁物 1 Airship body 2 Wind power generator 3 Mooring cable 4 Buoyancy balloon 5 Mooring rope winding device 6 Tail wing 7 Glider main wing 8. Torso 9 Power transmission line 10 Power transmission line 11 Power transmission line 12 Power transmission line 13 Electrical insulators
Claims (1)
、風力発電機を取り付け、これらの地上に対する繋留索
を送電線に兼用した、高空風力発電。[Claim 1] High-altitude wind power generation in which a wind power generator is attached to a flying vehicle such as an airship or a glider, and the mooring cables connected to the ground also serve as power transmission lines.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3121020A JPH04350369A (en) | 1991-05-27 | 1991-05-27 | High-altitude wind power generation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3121020A JPH04350369A (en) | 1991-05-27 | 1991-05-27 | High-altitude wind power generation |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH04350369A true JPH04350369A (en) | 1992-12-04 |
Family
ID=14800822
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3121020A Pending JPH04350369A (en) | 1991-05-27 | 1991-05-27 | High-altitude wind power generation |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH04350369A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20010069515A (en) * | 2001-04-10 | 2001-07-25 | 조근환 | Power generation by atmospheric friction |
US7098553B2 (en) * | 2005-01-12 | 2006-08-29 | Theodore F Wiegel | Traffic-driven wind generator |
EP1731759A2 (en) | 2005-06-09 | 2006-12-13 | Yehuda Roseman | Device for producing useful electricity from jetstreams |
WO2011026256A1 (en) * | 2009-09-03 | 2011-03-10 | 北京奇想创新科技中心 | System and method for high altitude wind power generation |
US8704397B2 (en) | 2005-06-09 | 2014-04-22 | Yehuda Roseman | System for producing electricity from jetstreams and tower therefor |
CN105257481A (en) * | 2015-11-04 | 2016-01-20 | 李明武 | Aerial wind power generation device |
WO2018192851A1 (en) * | 2017-04-21 | 2018-10-25 | Sanfritsch Gmbh | Cable for the stationary attachment of a high-altitude wind turbine |
RU2794371C1 (en) * | 2022-07-14 | 2023-04-17 | Борис Соломонович Бабицкий | Mobile wind power plant |
-
1991
- 1991-05-27 JP JP3121020A patent/JPH04350369A/en active Pending
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20010069515A (en) * | 2001-04-10 | 2001-07-25 | 조근환 | Power generation by atmospheric friction |
US7098553B2 (en) * | 2005-01-12 | 2006-08-29 | Theodore F Wiegel | Traffic-driven wind generator |
EP1731759A2 (en) | 2005-06-09 | 2006-12-13 | Yehuda Roseman | Device for producing useful electricity from jetstreams |
JP2006342790A (en) * | 2005-06-09 | 2006-12-21 | Yehuda Roseman | Method for generating power using jet stream |
US8704397B2 (en) | 2005-06-09 | 2014-04-22 | Yehuda Roseman | System for producing electricity from jetstreams and tower therefor |
WO2011026256A1 (en) * | 2009-09-03 | 2011-03-10 | 北京奇想创新科技中心 | System and method for high altitude wind power generation |
CN105257481A (en) * | 2015-11-04 | 2016-01-20 | 李明武 | Aerial wind power generation device |
WO2018192851A1 (en) * | 2017-04-21 | 2018-10-25 | Sanfritsch Gmbh | Cable for the stationary attachment of a high-altitude wind turbine |
KR20190139880A (en) * | 2017-04-21 | 2019-12-18 | 잔프리치 게엠베하 | Cable for fixedly fastening high altitude wind generators |
JP2020517851A (en) * | 2017-04-21 | 2020-06-18 | ザンフリッチュ・ゲゼルシャフト・ミト・ベシュレンクテル・ハフツング | Cable for fixing aerial wind power generator |
RU2794371C1 (en) * | 2022-07-14 | 2023-04-17 | Борис Соломонович Бабицкий | Mobile wind power plant |
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