JPH06205549A - Generation set - Google Patents
Generation setInfo
- Publication number
- JPH06205549A JPH06205549A JP4358550A JP35855092A JPH06205549A JP H06205549 A JPH06205549 A JP H06205549A JP 4358550 A JP4358550 A JP 4358550A JP 35855092 A JP35855092 A JP 35855092A JP H06205549 A JPH06205549 A JP H06205549A
- Authority
- JP
- Japan
- Prior art keywords
- ground
- infrared laser
- laser
- moon
- base
- 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
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
- Y02E10/50—Photovoltaic [PV] energy
Landscapes
- Photovoltaic Devices (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、月面に設けた太陽光発
電所又は原子力発電所からのエネルギーを地上で利用可
能にさせる発電装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a power generation device for making energy from a solar power plant or a nuclear power plant provided on the moon surface available on the ground.
【0002】[0002]
【従来の技術】電力供給源としての電力設備は、水力発
電から火力発電へと移行したが、火力発電の普及は、安
定した電力供給を可能にする一方、地球の温暖化と石油
不足を招くことになった。そこで、原子力発電が注目さ
れ、世界的に原子力発電設備の建設が進められている。
原子力発電の欠点は、事故が起きた時の環境汚染や人体
への悪影響である。これらの欠点は、人類の滅亡にもつ
ながることから、原子力発電設備の建設の反対理由とな
っている。2. Description of the Related Art Electric power equipment as an electric power source has changed from hydroelectric power generation to thermal power generation. The spread of thermal power generation enables stable electric power supply, but also causes global warming and oil shortage. is what happened. Therefore, attention is paid to nuclear power generation, and construction of nuclear power generation facilities is in progress worldwide.
Disadvantages of nuclear power generation are environmental pollution and adverse effects on the human body when an accident occurs. These shortcomings are the reason for opposition to the construction of nuclear power generation facilities, as they also lead to the destruction of humanity.
【0003】電力需要は年々増加することから、安全に
して且つ安定した電力供給設備の開発は急務である。こ
のような要請に応じ、太陽光発電衛星の考えが注目され
る。この太陽光発電衛星は、太陽光を電力に変換し、こ
れをマイクロウエーブで地上に送電するものである。Since the demand for electric power increases year by year, there is an urgent need to develop a safe and stable electric power supply facility. In response to such a request, the idea of a photovoltaic power generation satellite is drawing attention. This solar power generation satellite converts sunlight into electric power and transmits it to the ground by a microwave.
【0004】[0004]
【本発明が解決しようとする課題】太陽光発電衛星は、
しかし、送電量が少なく、加えて、衛星の数が膨大とな
り、且つ衛星の地上への落下対策に問題を残す。このた
め、構想としては興味があるものの、実用化の可能性は
小さい。それ故に、本発明は、前述した従来の考えの不
具合を解消し、新たな考えに基づく発電装置を提供する
ことを解決すべき課題とする。[Problems to be Solved by the Invention]
However, the amount of power transmission is small, the number of satellites becomes huge, and there is a problem in countermeasures against falling satellites to the ground. Therefore, although the idea is interesting, the possibility of practical application is small. Therefore, it is an object of the present invention to solve the above-mentioned problems of the conventional idea and to provide a power generation device based on the new idea.
【0005】[0005]
【課題を解決するための手段】本発明は、前述した課題
を解決するために、月面に太陽光又は原子力を用いた発
電設備を作ること、および傾斜構造によるエネルギー変
換材料を活用することという概念を導入する。In order to solve the above-mentioned problems, the present invention is to make a power generation facility using sunlight or nuclear power on the lunar surface and to utilize an energy conversion material having a graded structure. Introduce the concept.
【0006】本発明は、具体的には、月面太陽光発電所
又は月面原子力発電所としてのエネルギー発生源からの
発生エネルギーを紫外線レーザに変換する装置と、紫外
線レーザを受け且つ赤外線レーザに変換する宇宙基地
と、および赤外線レーザを電力に変換する地上受光基地
とからなる発電装置を提供する。Specifically, the present invention relates to an apparatus for converting the energy generated from an energy source such as a lunar solar power station or a lunar nuclear power station into an ultraviolet laser, and an infrared laser which receives the ultraviolet laser. Provided is a power generation device including a space station for conversion and a ground light receiving base for converting an infrared laser into electric power.
【0007】[0007]
【作用】月面で作られたエネルギーは、紫外線レーザに
より宇宙基地へ送られるが、この宇宙基地で紫外線レー
ザを赤外線レーザに変換し、赤外線レーザを地上へ送
り、必要個所へ送電する。赤外線レーザの利用は、地上
の生物への悪影響は全くなく、集光率も高く、送光効率
が高い。The energy produced on the lunar surface is sent to the space station by an ultraviolet laser, which converts the ultraviolet laser into an infrared laser, sends the infrared laser to the ground, and transmits it to the required places. The use of the infrared laser has no adverse effect on living things on the ground, has a high light collection rate, and has high light transmission efficiency.
【0008】[0008]
【実施例】図1を参照して、本発明に用いられる基本シ
ステム1(装置)を説明する。月2の表面に、太陽光発
電所又は原子力発電所3を設ける。宇宙基地としての衛
星4を地上の受光基地5と中継可能にする。月2と宇宙
中継基地4との間は、紫外線レーザ6(波長数10〜3
00nm)を用い、宇宙中継基地4と地上基地5との間
は赤外線レーザ7(波長数700〜1000数百nm)
を用いる。DESCRIPTION OF THE PREFERRED EMBODIMENTS A basic system 1 (apparatus) used in the present invention will be described with reference to FIG. A solar power plant or a nuclear power plant 3 will be installed on the surface of the moon 2. The satellite 4 as a space base can be relayed to the light receiving base 5 on the ground. Between the moon 2 and the space relay station 4, the ultraviolet laser 6 (wavelength number 10 to 3
00 nm) and an infrared laser 7 (wavelength number 700 to 1000 hundreds nm) between the space relay station 4 and the ground station 5.
To use.
【0009】月面2の太陽光又は原子力発電所3は、図
2に示す如く、太陽光源又は原子炉8からの太陽光又は
熱及び放射線9を、傾斜構造によるエネルギー変換材料
10,11により光電又は核熱および熱電変換させ、電
力を発生させる。熱電素子11は、たとえば、2000
Kの熱をヒートパイプ12とフィン13を用いて、10
00Kに落し、熱勾配を作り、電力を発生させる。この
電力15は、レーザ発信機14により、紫外線域の紫外
線レーザ6に変換され、衛星4へ送信される。As shown in FIG. 2, the sunlight or nuclear power plant 3 on the lunar surface 2 photoelectrically converts sunlight or heat and radiation 9 from a solar light source or a nuclear reactor 8 by using energy conversion materials 10 and 11 having an inclined structure. Alternatively, nuclear heat and thermoelectric conversion are performed to generate electric power. The thermoelectric element 11 is, for example, 2000
The heat of K is used for 10 with the heat pipe 12 and the fins 13.
The temperature is dropped to 00K, a thermal gradient is created, and electric power is generated. The electric power 15 is converted by the laser transmitter 14 into the ultraviolet laser 6 in the ultraviolet range and transmitted to the satellite 4.
【0010】衛星4で紫外線レーザから赤外線レーザ7
に変換し、赤外線レーザ7を地上基地5へ送信する。地
上基地5では、たとえば、P/1/Nからなる光電変換
素子16により赤外線レーザ7を電力17に変換させ、
必要個所へ送電する。From satellite 4 ultraviolet laser to infrared laser 7
Then, the infrared laser 7 is transmitted to the ground base 5. At the ground base 5, for example, the infrared laser 7 is converted into electric power 17 by the photoelectric conversion element 16 composed of P / 1 / N,
Transmit power to required places.
【0011】[0011]
【効果】月面でウラン等の原子燃料の入手が可能である
ので地上からの燃料供給は不用である。又、月面での原
子力発電は、放射線遮へいを原則的に必要としないの
で、発電設備を軽量小型にできる。傾斜構造技術の活用
は、原子力から電気への高効率直接変換が可能で、しか
も、回転機構を有しないから、安定した無人運転が可能
となる。本発明で使用する紫外線レーザと赤外線レーザ
は、損失、拡散が少いので受光率が高く、生物への悪影
響もない。飛行体のような障害物を検知した時、紫外線
レーザや赤外線レーザを直ちに遮断できるので、安全性
のための操作が容易である。総送電効率は、紫外線レー
ザへの変換率50%、赤外線レーザから直流への変換率
を95%とし、約40%と高効率となる。[Effect] Since nuclear fuel such as uranium can be obtained on the moon surface, fuel supply from the ground is unnecessary. In addition, since nuclear power generation on the moon does not require radiation shielding in principle, the power generation equipment can be made light and compact. The use of the gradient structure technology enables highly efficient direct conversion from nuclear power to electricity, and since it does not have a rotating mechanism, it enables stable unmanned operation. The ultraviolet laser and the infrared laser used in the present invention have a small loss and a small diffusion, and thus have a high light receiving rate and have no adverse effect on living things. When an obstacle such as a flying object is detected, the ultraviolet laser and the infrared laser can be immediately shut off, so that the operation for safety is easy. The total power transmission efficiency is as high as about 40% when the conversion rate to the ultraviolet laser is 50% and the conversion rate from the infrared laser to the direct current is 95%.
【図1】本発明の一例の説明図である。FIG. 1 is an explanatory diagram of an example of the present invention.
【図2】各基地に使用される装置の説明図である。FIG. 2 is an explanatory diagram of devices used in each base.
2 月 3 発電所 4 衛星 5 地上基地 6 紫外線レーザ 7 赤外線レーザ February 3 Power station 4 Satellite 5 Ground station 6 Ultraviolet laser 7 Infrared laser
Claims (1)
としてのエネルギー発生源からの発生エネルギーを紫外
線レーザに変換する装置と、紫外線レーザを受け且つ赤
外線レーザに変換する宇宙基地と、および赤外線レーザ
を電力に変換する地上受光基地とからなる発電装置。1. A device for converting energy generated from an energy source as a lunar solar power plant or a lunar nuclear power plant into an ultraviolet laser, a space station for receiving an ultraviolet laser and converting it into an infrared laser, and A power generator consisting of a ground light receiving base that converts an infrared laser into electric power.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP4358550A JPH06205549A (en) | 1992-12-28 | 1992-12-28 | Generation set |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP4358550A JPH06205549A (en) | 1992-12-28 | 1992-12-28 | Generation set |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH06205549A true JPH06205549A (en) | 1994-07-22 |
Family
ID=18459900
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP4358550A Pending JPH06205549A (en) | 1992-12-28 | 1992-12-28 | Generation set |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH06205549A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0715895A (en) * | 1993-06-25 | 1995-01-17 | Kansai Electric Power Co Inc:The | Energy transport system by use of laser beam |
JPH09247875A (en) * | 1996-03-11 | 1997-09-19 | Naohisa Suzuki | Generation of energy on surface of moon, and transport of the energy to earth by laser |
CN102368159A (en) * | 2011-11-11 | 2012-03-07 | 中海阳新能源电力股份有限公司 | Sun-following tracking simulation method of light reflecting celestial body |
JP2013128396A (en) * | 2011-12-06 | 2013-06-27 | Boeing Co:The | Methods and systems for light energy augmented power generation |
WO2023228702A1 (en) * | 2022-05-26 | 2023-11-30 | 克弥 西沢 | Conductive line, transfer device, and space solar beam energy transportation method |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3933323A (en) * | 1974-03-20 | 1976-01-20 | Raytheon Company | Solid state solar to microwave energy converter system and apparatus |
JPS5266300A (en) * | 1975-11-29 | 1977-06-01 | Masaaki Kusano | Method of supplying energy to space ship |
JPS55133638A (en) * | 1979-04-04 | 1980-10-17 | Mitsubishi Electric Corp | Solar generating power transmission system |
GB2059694A (en) * | 1979-09-14 | 1981-04-23 | British Aerospace | Solar energy supply system and method |
JPS58103839A (en) * | 1981-12-15 | 1983-06-21 | 三菱電機株式会社 | Solar generating power transporting system |
JPS6156698A (en) * | 1984-02-03 | 1986-03-22 | 有限会社新和商会 | Dryer |
JPS63133846A (en) * | 1986-11-20 | 1988-06-06 | 三井造船株式会社 | Transmission method by laser and laser generator |
-
1992
- 1992-12-28 JP JP4358550A patent/JPH06205549A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3933323A (en) * | 1974-03-20 | 1976-01-20 | Raytheon Company | Solid state solar to microwave energy converter system and apparatus |
JPS5266300A (en) * | 1975-11-29 | 1977-06-01 | Masaaki Kusano | Method of supplying energy to space ship |
JPS55133638A (en) * | 1979-04-04 | 1980-10-17 | Mitsubishi Electric Corp | Solar generating power transmission system |
GB2059694A (en) * | 1979-09-14 | 1981-04-23 | British Aerospace | Solar energy supply system and method |
JPS58103839A (en) * | 1981-12-15 | 1983-06-21 | 三菱電機株式会社 | Solar generating power transporting system |
JPS6156698A (en) * | 1984-02-03 | 1986-03-22 | 有限会社新和商会 | Dryer |
JPS63133846A (en) * | 1986-11-20 | 1988-06-06 | 三井造船株式会社 | Transmission method by laser and laser generator |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0715895A (en) * | 1993-06-25 | 1995-01-17 | Kansai Electric Power Co Inc:The | Energy transport system by use of laser beam |
JP2527905B2 (en) * | 1993-06-25 | 1996-08-28 | 関西電力株式会社 | Free electron laser light generator and its laser energy transport system |
JPH09247875A (en) * | 1996-03-11 | 1997-09-19 | Naohisa Suzuki | Generation of energy on surface of moon, and transport of the energy to earth by laser |
CN102368159A (en) * | 2011-11-11 | 2012-03-07 | 中海阳新能源电力股份有限公司 | Sun-following tracking simulation method of light reflecting celestial body |
JP2013128396A (en) * | 2011-12-06 | 2013-06-27 | Boeing Co:The | Methods and systems for light energy augmented power generation |
WO2023228702A1 (en) * | 2022-05-26 | 2023-11-30 | 克弥 西沢 | Conductive line, transfer device, and space solar beam energy transportation method |
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