| 摘要 |
A method and system for supplying an aircraft with electrical power, said aircraft being provided with a plurality of loads (C1-C4) to be powered, said power supply system comprising a plurality of power sources (S1, S2, S3) and an onboard power management module, the power management module (MG) being electrically connected to said power sources (S1, S2, S3) and to said loads (C1-C4) to be powered. The power management module (MG) is arranged to order the powering of at least one of said loads (C1-C4) by at least two different power sources (S1, S2, S3) in parallel in the case of an increase in the power requirements, said load (C1-C4) initially being powered by a single power source (S1, S2, S3). |
