Aerodynamic perfection of the high-pressure cylinder stage of the steam turbine by capacity 300 MW by means of spatial profiling of blades
The results are presented for research and the laws of influence received on basis it district and axial offset (scimitar-shape and sweep) working and directing blades of a step of the high-pressure cylinder the steam turbine on spatial structure of a stream and aerodynamic characteristics of a flowing part are presented.