JPS61164520U - - Google Patents
Info
- Publication number
- JPS61164520U JPS61164520U JP4835885U JP4835885U JPS61164520U JP S61164520 U JPS61164520 U JP S61164520U JP 4835885 U JP4835885 U JP 4835885U JP 4835885 U JP4835885 U JP 4835885U JP S61164520 U JPS61164520 U JP S61164520U
- Authority
- JP
- Japan
- Prior art keywords
- solar cell
- cell array
- shunt
- thyristor
- controls
- 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 claims description 3
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Control Of Electrical Variables (AREA)
Description
第１図はこの考案の一実施例を示す人工衛星の
電力発生装置の構成図、第２図は従来の人工衛星
の電力発生装置の構成図である。
図において、１は主太陽電池アレー、２はシヤ
ント太陽電池アレー、３は電力制御器、４はシヤ
ント回路、５はダイオード、６はサイリスタ、７
は制御回路である。なお、図中同一符号は同一又
は相当部分を示す。
FIG. 1 is a block diagram of a power generation device for an artificial satellite showing an embodiment of this invention, and FIG. 2 is a block diagram of a conventional power generation device for a satellite. In the figure, 1 is the main solar cell array, 2 is the shunt solar cell array, 3 is the power controller, 4 is the shunt circuit, 5 is the diode, 6 is the thyristor, and 7 is the shunt solar cell array.
is the control circuit. Note that the same reference numerals in the figures indicate the same or equivalent parts.
Claims (1)
太陽電池アレーを直列接続したものとサイリンタ
、主太陽電池アレーおよびシヤント太陽電池アレ
ーを直列接続したものとを並列接続してなる電源
と、上記シヤント太陽電池アレーにダイオード、
サイリスタを介して並列接続されたシヤント回路
と、上記電源の出力電圧を検出し、上記電源の出
力電圧が一定となるようにシヤント回路のインピ
ーダンスを制御する電力制御器と、上記サイリス
タのゲートに制御信号を与えてサイリスタをオン
／オフ制御する制御回路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 power supply consisting of a diode, a main solar cell array, and a shunt solar cell array connected in series, and a cylintor, a main solar cell array, and a shunt solar cell array connected in series, connected in parallel, and a diode connected to the shunt solar cell array. ,
A shunt circuit connected in parallel through the thyristor, a power controller that detects the output voltage of the power supply and controls the impedance of the shunt circuit so that the output voltage of the power supply is constant, and a power controller that controls the gate of the thyristor. A power generation device for an artificial satellite, comprising a control circuit that controls a thyristor on/off by applying a signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4835885U JPS61164520U (en) | 1985-04-01 | 1985-04-01 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4835885U JPS61164520U (en) | 1985-04-01 | 1985-04-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61164520U true JPS61164520U (en) | 1986-10-13 |
Family
ID=30564539
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4835885U Pending JPS61164520U (en) | 1985-04-01 | 1985-04-01 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61164520U (en) |
-
1985
- 1985-04-01 JP JP4835885U patent/JPS61164520U/ja active Pending