High-power light-weight control power distribution circuit applied to spacecraft
The invention discloses a high-power light-weight control power distribution circuit applied to a spacecraft, and the circuit comprises a first MOS tube and a first magnetic latching relay, and the signal input end of the first magnetic latching relay is used for receiving an instruction pulse signa...
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creator | LIU SHENGYANG FU YUEPING LIN XINGYONG SU SIYOU ZHANG JINTAO |
description | The invention discloses a high-power light-weight control power distribution circuit applied to a spacecraft, and the circuit comprises a first MOS tube and a first magnetic latching relay, and the signal input end of the first magnetic latching relay is used for receiving an instruction pulse signal. The controlled end of the first magnetic latching relay controls the voltage difference between the source electrode and the grid electrode of the first MOS tube so as to control the on-off state of the first MOS tube to be kept, and the source electrode and the drain electrode of the first MOS tube are connected in series in the control power distribution circuit. The grid electrode of the first MOS tube is connected with a DC power supply through a first divider resistor, and is connected with the controlled end of the first magnetic latching relay through a second divider resistor. Based on a high-power and light-weight power supply and distribution framework combining a low-power relay and an MOS (Metal Oxid |
format | Patent |
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subjects | APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC,OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWERSUPPLY SYSTEMS CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONTROL OR REGULATION THEREOF CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUTPOWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GENERATION SYSTEMS FOR STORING ELECTRIC ENERGY |
title | High-power light-weight control power distribution circuit applied to spacecraft |
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