| 摘要 |
<p>An electrical power system (40) for an aircraft having electrical loads (70, 72) and at least one jet engine with a high pressure spool (26) and a low pressure spool (28), the electrical power system (40) includes a first electrical machine driven by a first pressure spool (26, 28) and outputting a first voltage (52) , a second electrical machine driven by a second pressure spool (26, 28) and outputting a second voltage (56), and an electrical distribution bus receiving the first and second voltages (52, 56) and supplying the voltages (52, 56) to the loads (70, 72).</p> |
