FIELD: engines and pumps.
SUBSTANCE: aircraft gas turbine engine 1 comprises, at least, one rotor shaft supporting, at least, one compressor, turbine and housing. At least, one generator assembly 10 is fitted on rotor shaft to generate electric power. Generator assembly 10 comprises mounting plate 11b and generator 12. Assembly 10 is fitted on said mounting plate 11a arranged on engine side and may de detached therefrom. Said plate 11a has connection elements to fasten generator assembly 10 thereto. Mounting plate 11a comprises, at least, one mechanical mount, device to transmit motion to generator, electrical contacts and/or pipeline connection ports.
EFFECT: simplified mounting/dismantling and servicing.
11 cl, 5 dwg
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