JPS61231773A - Electric power generator for artificial planet - Google Patents
Electric power generator for artificial planetInfo
- Publication number
- JPS61231773A JPS61231773A JP60073736A JP7373685A JPS61231773A JP S61231773 A JPS61231773 A JP S61231773A JP 60073736 A JP60073736 A JP 60073736A JP 7373685 A JP7373685 A JP 7373685A JP S61231773 A JPS61231773 A JP S61231773A
- Authority
- JP
- Japan
- Prior art keywords
- sunlight
- planet
- optical fiber
- battery array
- main part
- 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
- 239000013307 optical fiber Substances 0.000 claims abstract description 8
- 238000010248 power generation Methods 0.000 claims description 9
- 230000005611 electricity Effects 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 7
- 239000000835 fiber Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 238000003491 array Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000004907 gland Anatomy 0.000 description 1
- 230000001678 irradiating effect Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
- H01L31/0543—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means comprising light concentrating means of the refractive type, e.g. lenses
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
- H01L31/0547—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means comprising light concentrating means of the reflecting type, e.g. parabolic mirrors, concentrators using total internal reflection
-
- 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
- Y02E10/52—PV systems with concentrators
Abstract
Description
【発明の詳細な説明】
り戚東上の利用分野〕
この発明は人工衛星に搭載して、太陽光を電気エネルギ
に変換する電力発生＃Ｃｈに関するものでるる。[Detailed Description of the Invention] Field of Application of Riki Tojo] This invention relates to a power generation channel #Ch that is mounted on an artificial satellite and converts sunlight into electrical energy.
第４図は、従来の人工餉星用′厄力発生装叙の概念を示
す図であり９図において（１）は衛星本体、（２）はパ
ドル、（３）は太陽電池アレイ、（４）は１！線である
。Figure 4 is a diagram showing the concept of the conventional ``harmonic force generation equipment'' for an artificial star. In Figure 9, (1) is the satellite body, (2) is the paddle, (3) is the solar array, (4) ) is 1! It is a line.
このようなｍｇにおいて、ｌ＃星本体（１）に取付けら
ｎたパドル（２）は、その異面に計装された太陽電池ア
レイ（３）の受光面を常に太陽方向に向けるように制御
さ牡る。太陽電池アレイ（３）は受光した太陽光を電気
エネルギに変換し、を線（４１によってこの電気エネル
ギを衛星本体（１１に伝導し、衛星に搭載した各−機器
に電力を供給することができる。In such a mg, the paddle (2) attached to the l# star body (1) is controlled so that the light-receiving surface of the solar cell array (3), which is instrumented on the other side, always faces toward the sun. Let's go. The solar cell array (3) converts the received sunlight into electrical energy, and conducts this electrical energy to the satellite body (11) through the wire (41), where it can supply power to each device on board the satellite. .
ところで上記従来の電力発生ｋｋは発生する電力がパド
ル（２）に計装した太陽電池プレイ（３）の面積に比例
するので、大きな電力を発生させるためには多数の太Ｖ
ｖＩ電池を必要とする。また、太耐電池アレイ（３）を
直接半組空間に晒すので、パンアレン帝にトラップさｎ
た放射腺によって急速に電力発生能力が低下するなどの
欠点があった。By the way, in the above-mentioned conventional power generation kk, the generated power is proportional to the area of the solar battery play (3) instrumented on the paddle (2), so in order to generate large power, a large number of large V
Requires vI batteries. In addition, since the thick battery array (3) is directly exposed to the half-assembly space, it will not be trapped by Pan Allen Emperor.
The disadvantage was that the power generation ability rapidly decreased due to the radiation glands.
この発ＢＡは、かかる問題点を解次１゛るためになされ
たもので、太陽電池アレイの面積轟）の発生電力が大き
く、又、太陽電電アレイを術星本体内部に計装できるよ
うにした人工衛星用電力発生装置を得ることを目的とす
るものである。This generation BA was made in order to solve these problems, and the power generated by the area of the solar cell array is large, and the solar cell array can be instrumented inside the main body of the star. The purpose of this invention is to obtain a power generation device for an artificial satellite.
この発明に係る電力発生装置は、パドルに計装さｎた集
光器と、この集光器で集光された太陽光を伝送する元フ
ァイバケーブルの末端に設けられた光拡散器と、この光
拡散器から投光される太陽光を光ｆｉ変換する太陽電池
プレイとを備えたものでおる。The power generation device according to the present invention includes a light collector that is instrumented on a paddle, a light diffuser that is provided at the end of a source fiber cable that transmits sunlight collected by the light collector, and It is equipped with a solar cell play that converts the sunlight projected from the light diffuser into optical fi.
この発明においては、太陽光を集光器で果元して、光フ
ァイバケーブルで衛星本体内に伝送し。In this invention, sunlight is collected by a concentrator and transmitted into the satellite body using an optical fiber cable.
元ファイバケーブルの末端に取付けた光拡散器で伝送さ
ｎた太陽光を拡散して９太陽電池アレイを照射し、電力
を発生する。A light diffuser attached to the end of the original fiber cable diffuses the transmitted sunlight to illuminate the nine solar cell arrays and generate electricity.
第１図はこの発明による人工衛星の電力発生装置の全体
構成を示す図でめり、（１）〜（３）は上記従来装置と
同−又は相当のものでおる。また、第２図は８１図の構
成要素である集光器（５）を示し、また第３図は同じく
光拡散器（７）の構成を示す図である。FIG. 1 is a diagram showing the overall configuration of a power generation device for an artificial satellite according to the present invention, and (1) to (3) are the same as or equivalent to the conventional device described above. Further, FIG. 2 shows a condenser (5) which is a component of FIG. 81, and FIG. 3 is a diagram showing the configuration of a light diffuser (7).
図において、（５）はパドル（３）に計装された集−／
ｌ、器。In the figure, (5) is a collection instrumented on paddle (3).
l, vessel.
（６）は一端が集光器（５）に接続さｎｆｃ元ファイバ
ケーブル、（７）は光ファイバケーブル（６）の他端に
接続された光拡散器、（８）はレンズ、（９）は支持体
、 Ｑｌは放物面貌である。(6) is an NFC source fiber cable with one end connected to the concentrator (5), (7) is a light diffuser connected to the other end of the optical fiber cable (6), (8) is a lens, (9) is the support and Ql is the paraboloid.
上記のような構成において、集光器（５）は太陽光ＳＰ
！：レンズ（８）によって集光する。集光された太陽光
を光ファイバケーブル（６）によって衛星本体（１）内
部伝送する。元ファイバケーブル（６）の末端に取付け
た光拡散器（７）によって伝送された太陽Ｍ：、Ｓ？：
拡散し、衛星本体（１）内部に設けらｎた太陽電池アレ
イ（３）を照射して電力を発生させる。In the above configuration, the concentrator (5)
! : Focus the light by the lens (8). The concentrated sunlight is transmitted inside the satellite body (1) via an optical fiber cable (6). The solar M:, S? transmitted by a light diffuser (7) attached to the end of the original fiber cable (6)? :
The light is diffused and illuminates the solar cell array (3) provided inside the satellite body (1) to generate electric power.
尚、支持体＋９１ ｆｉ 、 レンズ（８）及びプしフ
ァイバケーブル（６）を支持するものであり、又、放物
面鏡αＧは太陽光Ｓの拡散を行う。The support body +91 fi supports the lens (8) and the fiber cable (6), and the parabolic mirror αG diffuses sunlight S.
この発明は以上説明したとおり、パドルに取付けた集光
器で太陽光を集光し、太＠光のエネルギ密度を上けて、
衛星本体内部の太陽電池アレイを照射することにより、
太陽電池プレイの単位計装面積轟りの発生電力を大きく
することができる。As explained above, this invention collects sunlight with a concentrator attached to a paddle, increases the energy density of the light,
By irradiating the solar array inside the satellite body,
The power generated per unit instrumentation area of solar cell play can be increased.
又、太陽電池アレイを直接宇宙空間に晒す必要がないの
で放射線による電力発生能力の低下も緩和できるなどの
効果がある。Furthermore, since there is no need to directly expose the solar cell array to outer space, it is possible to alleviate the reduction in power generation ability caused by radiation.
第１図はこの発明の一夾施例を示す人工ｒＩ＃Ｉ星の電
力発生装置の侮成図、第２図はこの発明の構成要素であ
る集光器の構成図、第３図は同じく光拡散器の構成図、
第４図は従来の人工衛星用電力発生装置の構成を示す凶
である。
図において（りは衛星本体、（２）はパドル、（３）は
太陽電池アレイ、（５）は集光器、（６）は元ファイバ
ケーブル、（７１は光拡散器、（８）はレンズ、（９）
は支持体。
０１は放物面鏡である。
なお１図中同一行号は同−又は相当部分を示す。Fig. 1 is a schematic diagram of a power generator for an artificial rI#I star showing one embodiment of this invention, Fig. 2 is a block diagram of a condenser which is a component of this invention, and Fig. 3 is a similar diagram. Configuration diagram of light diffuser,
FIG. 4 shows the configuration of a conventional power generation device for an artificial satellite. In the figure, (ri is the satellite body, (2) is the paddle, (3) is the solar array, (5) is the concentrator, (6) is the original fiber cable, (71 is the light diffuser, and (8) is the lens. , (9)
is a support. 01 is a parabolic mirror. Note that the same line numbers in Figure 1 indicate the same or equivalent parts.
Claims (1)
けられ、太陽光を集光する集光器と、一端が上記集光器
に接続され、上記集光器で集光された太陽光を他端側に
伝送する光ファイバケーブルと、この光ファイバケーブ
ルの他端に接続された光拡散器と、人工衛星本体内部に
設けられ、上記光拡散器から投光される太陽光を光電変
換する太陽電池アレイとを具備したことを特徴とする人
工衛星の電力発生装置。A paddle attached to the satellite body, a concentrator provided on the paddle to collect sunlight, and one end connected to the concentrator to collect sunlight collected by the concentrator. An optical fiber cable that transmits to one end, a light diffuser connected to the other end of the optical fiber cable, and a solar panel installed inside the satellite body that converts sunlight emitted from the light diffuser into electricity. A power generation device for an artificial satellite, characterized by comprising a battery array.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60073736A JPS61231773A (en) | 1985-04-08 | 1985-04-08 | Electric power generator for artificial planet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60073736A JPS61231773A (en) | 1985-04-08 | 1985-04-08 | Electric power generator for artificial planet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61231773A true JPS61231773A (en) | 1986-10-16 |
Family
ID=13526816
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60073736A Pending JPS61231773A (en) | 1985-04-08 | 1985-04-08 | Electric power generator for artificial planet |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61231773A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4976789A (en) * | 1989-12-26 | 1990-12-11 | The United States Of America As Represented By The Secretary Of The Army | Power transmission device |
| US5089055A (en) * | 1989-12-12 | 1992-02-18 | Takashi Nakamura | Survivable solar power-generating systems for use with spacecraft |
| US5501743A (en) * | 1994-08-11 | 1996-03-26 | Cherney; Matthew | Fiber optic power-generating system |
| US6037535A (en) * | 1994-06-03 | 2000-03-14 | Yoshino; Kazuo | Sunlight collection apparatus |
| JP2010003759A (en) * | 2008-06-18 | 2010-01-07 | Arima Ecoenergy Technologies Corp | Light collection type photovoltaic cell device with optical guide |
-
1985
- 1985-04-08 JP JP60073736A patent/JPS61231773A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5089055A (en) * | 1989-12-12 | 1992-02-18 | Takashi Nakamura | Survivable solar power-generating systems for use with spacecraft |
| US4976789A (en) * | 1989-12-26 | 1990-12-11 | The United States Of America As Represented By The Secretary Of The Army | Power transmission device |
| US6037535A (en) * | 1994-06-03 | 2000-03-14 | Yoshino; Kazuo | Sunlight collection apparatus |
| US5501743A (en) * | 1994-08-11 | 1996-03-26 | Cherney; Matthew | Fiber optic power-generating system |
| JP2010003759A (en) * | 2008-06-18 | 2010-01-07 | Arima Ecoenergy Technologies Corp | Light collection type photovoltaic cell device with optical guide |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR920006588B1 (en) | Solar ray device for illumination | |
| ES2076359T3 (en) | DISPOSITION OF SOLAR CONCENTRATOR. | |
| EP0180877A3 (en) | Photovoltaic cell array with light concentrating device | |
| ES477108A1 (en) | Method of and system for generating energy from solar and wind energy sources | |
| WO1999045596A1 (en) | Method and apparatus for directing solar energy to solar energy collecting cells | |
| FR2434996A1 (en) | DEVICE FOR USING SOLAR ENERGY FOR LIGHTING ROOMS NOT ACCESSIBLE TO SUN LIGHT | |
| EP2513570A1 (en) | Solar power generator module | |
| US3379394A (en) | Optical solar energy converter | |
| US4960468A (en) | Photovoltaic converter having apertured reflective enclosure | |
| JPS61231773A (en) | Electric power generator for artificial planet | |
| JPH11163382A (en) | Photoelectric conversion device | |
| JPS58135683A (en) | Power generation device by solar battery | |
| JPS59709B2 (en) | A device that concentrates solar energy to generate electricity | |
| KR850001560B1 (en) | Device using both as collecting light and generating | |
| CN213186026U (en) | Photovoltaic module light condensing device | |
| CN212210887U (en) | Wind, light and water multi-energy complementary comprehensive utilization device capable of reducing heat loss | |
| RU2121632C1 (en) | Device for concentration of solar radiation | |
| JPS5680177A (en) | Power generator by solar ray | |
| JPS59228772A (en) | Solar battery power source | |
| CN212367175U (en) | Photovoltaic curtain wall unit and curtain wall system | |
| JPS6140063A (en) | Solar cell mounting apparatus | |
| CN213661558U (en) | Silicon solar cell separating and placing equipment | |
| CN207691724U (en) | A kind of solar collecting device of more combination of monomers | |
| JPS5994466A (en) | Solar battery system | |
| JPS58141577A (en) | Parabolic beam-condensing type solar cell |