| 摘要 |
An apparatus for regulating voltage and aerospace electrical power systems are implemented. A multi-functional apparatus for regulating voltage, according to one embodiment, comprises: a DC to DC converter ( 315 ), wherein the DC to DC converter ( 315 ) is controlled to operate in a first direction to receive a DC voltage from a first bus ( 329 ) and to output a first regulated DC voltage adjusted to charge a battery ( 307 ), wherein the first bus ( 329 ) receives power from a second bus ( 201 ), and is controlled to operate in a second direction to receive a battery DC voltage from the battery ( 307 ) and to output a second regulated DC voltage to the first bus ( 329 ) to power a load ( 231 ) independently or in combination with the second bus ( 201 ).
|
