Improved Compressor Exit Diffuser for an Industrial Gas Turbine

U Orth,H. Ebbing,H. Krain,Anton Weber,B. Hoffmann

Improved Compressor Exit Diffuser for an Industrial Gas Turbine

2001

U Orth
H. Ebbing
H. Krain
Anton Weber
B. Hoffmann

The aerodynamical design process used for the optimization of a centrifugal compressor stage is described. Advanced design tools for blade generation and 3D aerodynamic calculation methods were used. The manufacturing procedure and experimental verification is described.

Keywords:

Control theory
Aerodynamics
Automotive engineering
Centrifugal compressor
Turbine
Thermal efficiency
Engineering
Design process
Mechanical engineering
Gas compressor
Industrial gas
Impeller
Centrifugal force

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