ELECTRICAL ARCHITECTURE OF AN AIRCRAFT, AIRCRAFT COMPRISING THE ARCHITECTURE AND OPERATING METHOD OF THE ARCHITECTURE

摘要

The invention relates to an aircraft architecture, an aircraft comprising the architecture and a method of operating the architecture. According to the invention, the architecture comprises two air conditioning systems (12, 14), two converters (62L, 62R) each intended to supply one of the air conditioning systems (12, 14) and at least one first electric machine (24L) ensuring the start of a first main engine (42L) of the aircraft. The electrical architecture (60) is configured so that the two converters (62L, 62R) can jointly supply the first electrical machine (24L).