| 摘要 |
<p>PROBLEM TO BE SOLVED: To provide an electric power system for an aircraft, which can supply high power to a load while suppressing upsizing of an electric motor and the like.SOLUTION: An electric power system 1 for an aircraft includes a high-voltage bus 14 for FCS, which is used to supply electric power to an electric actuator 41. The high-voltage bus 14 for FCS is configured to be capable of being constantly connected to a main generator 21 and a flywheel battery 27, which serve as two or more different types of power supply devices.</p> |
