| 摘要 |
The method involves realizing a starting step of an autonomous electricity production and conditioning system (22). An electric network (20) of an aircraft (10) comprising batteries is electrically connected to an auxiliary alternator (60) for supplying the auxiliary alternator with outside air in the starting step. A deactivation step of the auxiliary alternator is realized when a power turbine (52) rotates a rotary shaft (50) independently such that a main alternator (58) is operated as a generator, and provides electric power to the electric network when the shaft is rotated. An independent claim is also included for an aircraft. |
