Gas turbine engine

Details Gas turbine engine Gas turbine engine

1995-06-19

1997-05-06

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60751, 415179, F02C 700, F04D 2954

Patent

active

056260180

ABSTRACT:
A gas turbine engine with first and second axial flow compressors and an intercooler therebetween is provided with a diffuser to diffuse the air flow leaving the downstream end of the first axial flow compressor at a first radial distance from the axis to the upstream end of the intercooler at a second radial distance from the axis. The diffuser comprises a first radially extending wall, a second radially extending wall and a plurality of diffuser vanes extending therebetween which define a plurality of generally radially extending diffusing passages. The vanes are wedge shaped. This arrangement provides diffusion in a short axial length.

REFERENCES:
patent: 3552877 (1971-01-01), Christ
patent: 4455121 (1984-06-01), Jen

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