FIELD: turbo-machines.
SUBSTANCE: turbomachine for aircraft, containing turbomachine shaft and pumping module (100), containing structural housing (9), pump shaft (11), connected to turbine machine shaft (1), turbo-machine fuel supply pump (3), mounted on said pump shaft (11) and inside structural unit (9), and electric device (5), mounted on said pump shaft (11) and made with possibility of said pump shaft (11) rotation to actuate supply pump (3) or with possibility to be driven into rotation by said pump shaft (11) for turbine machine unit (8) electric power supply, wherein electric device comprises rotor components (51), installed on supply pump movable part (32) outer periphery, and stator components (52), installed on structural housing inner periphery.
EFFECT: enabling gas turbine engine fast and reliable start-up, shorter duration of service for replacement of filtration unit fuel filter.
15 cl, 15 dwg
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