发明名称 POWER SUPPLY FOR A SATELLITE RECEIVER
摘要 A power supply (10) for a satellite receiver system includes a dual input supply voltage arrangement (200). When a higher output v oltage is selected, a source of a lower supply input voltage is coupled to an input, main current conducting terminal of a series pass transistor (Q1). On the other hand, when a lower output voltage is selected, a source of a lower supply input voltage is coupled to the input main current conducting terminal of the series pass transistor. A comparator (22) senses a magnitude of an output voltage (16) produced by the series pass transistor. When, as a result of an over current condition, the output voltage is lower than a reference threshold level (22a), any selection of the higher output voltage is automatically over-ridden and the source of the lower supply input voltage, instead, is coupled to the input main current conducting terminal of the series pass transistor.
申请公布号 KR20040105835(A) 申请公布日期 2004.12.16
申请号 KR20047015618 申请日期 2003.04.03
申请人 发明人
分类号 H04B1/06;H04B1/18;H04B1/38 主分类号 H04B1/06
代理机构 代理人
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