TURBINE GENERATOR Russian patent published in 2024 - IPC F01D15/10 F02C7/268 

FIELD: turbomachine building.

SUBSTANCE: invention relates to the field of turbomachinery, namely to power generation systems based on a gas turbine engine having an axial compressor, invention can be used in power plants of aircraft, as well as an independent source of electric energy. In a turbine generator comprising a combustion chamber and a turbo compressor with an axial compressor located on it in front of the combustion chamber and a turbine behind the combustion chamber with the possibility of rotation of the rotor of the axial compressor and an electromechanical energy converter located coaxially to the rotor of the turbo compressor, wherein the axial compressor comprises stages with a row of blades of the guide apparatus, rigidly connected to the housing of the axial compressor, and a row of working blades; according to the invention, the rows of working blades of the axial compressor are located on the outer surface of the rotor formed by a cylindrical shell containing at least one annular section for fixing the outwardly oriented working blades, at least one end cover with trunnions for the rotor resting on the bearings and the annular bore on the cylindrical shell inner surface for the permanent magnets forming the integrated electromechanical energy converter rotor, wherein the stator is located in the inner cavity of the cylindrical shell.

EFFECT: higher productiveness and efficiency due to expansion of functional capabilities of components of aircraft power plant by means of integration of gas turbine engine and electromechanical energy converter, which form power unit, into single unit.

1 cl, 3 dwg