发明名称 POWER SUPPLY FOR A SATELLITE RECEIVER
摘要 <p>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.</p>
申请公布号 EP1490979(B1) 申请公布日期 2015.08.12
申请号 EP20030746133 申请日期 2003.04.03
申请人 THOMSON LICENSING 发明人 FITZPATRICK, JOHN, JAMES;LELEY, SURESH, VISHWANATM;BOWYER, ANDREW, ERIC;CURTIS, III, JOHN, JOSEPH;PITSCH, ROBERT, ALAN
分类号 H04B1/18;H04H40/90 主分类号 H04B1/18
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