Gas turbine engine having a mixed flow compressor

Details Gas turbine engine having a mixed flow compressor Gas turbine engine having a mixed flow compressor

1990-06-11

1992-03-10

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60751, 60760, F02C 314

Patent

active

050940694

ABSTRACT:
A gas turbine engine is disclosed having a mixed-flow compressor and a connecting mixed-flow diffuser. The mixed-flow diffuser is disposed inside the annularly arranged combustion chambers and supplying them, from the direction of the radial interior side, in the reverse flow, with compressor air. Gas turbine engines of this type are more compact and show a higher efficiency than turbine engines having radial flow compressors.

REFERENCES:
patent: 2640319 (1953-06-01), Wislicenus
patent: 3365892 (1968-01-01), Derderian
patent: 3404853 (1968-10-01), Miller

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