High efficiency, twin spool, radial-high pressure, gas turbine e

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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60 3936, F02C 305

Patent

active

050818325

ABSTRACT:
A low cost, low fuel consumption, twin-spool turbine engine with external power take-off essentially exclusively from the high pressure (H.P.) spool uses a radial in-flow turbine and a centrifugal compressor in the H.P. spool and a flow-optimized L.P. spool to achieve pressure ratios above 12/1 for simple cycle engines. Intercooled and recuperated versions are included. The turbine engine according to this invention is ideally suited for applications up to about 1000 KW and will provide some 20% less fuel consumption in this power range compared with conventional designs.

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