JPH0214247U - - Google Patents
Info
- Publication number
- JPH0214247U JPH0214247U JP9274288U JP9274288U JPH0214247U JP H0214247 U JPH0214247 U JP H0214247U JP 9274288 U JP9274288 U JP 9274288U JP 9274288 U JP9274288 U JP 9274288U JP H0214247 U JPH0214247 U JP H0214247U
- Authority
- JP
- Japan
- Prior art keywords
- storage battery
- circuit mechanism
- power supply
- comparator
- output voltage
- 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
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
Landscapes
- Control Of Charge By Means Of Generators (AREA)
Description
図面は、本考案に係る走行機体における電源装
置の一実施例を示すものであつて、第１図は、カ
ルチベータの全体斜視図、第２図は、要部回路図
、第３図は、始動スイツチの切替説明図、第４図
ａは、サイリスタＯＦＦ時の整流器出力波形図、
第４図ｂは、サイリスタＯＮ時の整流器出力波形
図、である。
図中、１３……蓄電池、１４……充電回路機構
、１５……始動回路機構、１６……シリコン制御
整流素子、１８……比較器、Ｖ１……基準充電電
圧、Ｖ２……整流出力電圧、である。
The drawings show an embodiment of the power supply device for a traveling aircraft according to the present invention, in which FIG. 1 is an overall perspective view of a cultivator, FIG. 2 is a circuit diagram of a main part, and FIG. An explanatory diagram of switching the starting switch, Fig. 4a is a rectifier output waveform diagram when the thyristor is OFF,
FIG. 4b is a rectifier output waveform diagram when the thyristor is ON. In the figure, 13...storage battery, 14...charging circuit mechanism, 15...starting circuit mechanism, 16...silicon control rectifying element, 18...comparator, V1 ...reference charging voltage, V2 ...rectifying output Voltage.
Claims (1)
電池と、上記蓄電池の電源供給を受けて駆動装置
を始動する始動回路機構と、運転中に蓄電池を充
電する充電回路機構とを備えた走行機体における
電源装置において、上記充電回路機構には、基準
充電電圧と整流出力電圧とを比較する比較器を設
けると共に、上記比較器出力と連動して整流出力
電圧を制御するシリコン制御整流素子を設けたこ
とを特徴とする走行機体における電源装置。 A power source for a traveling aircraft that includes a storage battery that supplies power to an electrical equipment group and a drive device, a starting circuit mechanism that receives power supply from the storage battery to start the drive device, and a charging circuit mechanism that charges the storage battery during operation. In the device, the charging circuit mechanism is provided with a comparator that compares the reference charging voltage and the rectified output voltage, and a silicon-controlled rectifying element that controls the rectified output voltage in conjunction with the comparator output. A power supply device for a traveling aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9274288U JPH0214247U (en) | 1988-07-13 | 1988-07-13 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9274288U JPH0214247U (en) | 1988-07-13 | 1988-07-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0214247U true JPH0214247U (en) | 1990-01-29 |
Family
ID=31317181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9274288U Pending JPH0214247U (en) | 1988-07-13 | 1988-07-13 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0214247U (en) |
-
1988
- 1988-07-13 JP JP9274288U patent/JPH0214247U/ja active Pending