| 摘要 |
Energy supply network for an aircraft or spacecraft (1), comprising at least one energy generating device (7-1 to 7-6) for generating electrical energy, comprising at least two energy control devices (10, 12), at least one of which is coupled directly to at least one of the energy generating devices (7-1 to 7-6) and which are adapted each to provide a controlled supply voltage so as to supply electrical loads (17-1 to 17-16) located in the aircraft (1) with energy, and comprising a high-voltage direct current transmission device (1 1), which couples the at least two energy control devices (10, 12) to one another by means of high-voltage direct current transmission. |
