FIELD: motors and pumps.
SUBSTANCE: invention relates to aircraft taxiing systems. Aircraft engine (10) includes core gas turbine engine (11). Gas turbine engine (11) includes compressor (12), combustor (14) and high pressure turbine (16). Aircraft engine also includes fan assembly (13) connected to core gas turbine engine (11). Aircraft engine further includes electric taxi system connected to fan assembly (13). Electric taxi system includes energy storage device (52) and motor (54) responsive to the energy supply by energy storage device (52). Said motor (54) is connected to fan assembly (13) and is configured to actuate fan assembly (13) during taxi operations.
EFFECT: invention simplifies taxiing.
16 cl, 4 dwg
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