Method for operating gas turbine unit for combined production of

Power plants – Combustion products used as motive fluid

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Details

60 3905, 60 3925, 60 39511, F02C 330, F02C 710

Patent

active

051933373

ABSTRACT:
Gas turbine unit comprising a high pressure turbine (10) driving a high pressure compressor (11), and a low pressure turbine (13) driving a low pressure compressor (14) and a generator (12), a combustion chamber supplying gas to the compressors, and a recuperator (18) for heat exchange between exhaust gas and compressor air, the low pressure turbine having an adjustable geometry and an adjustable connection (20) being provided bypassing the recuperator, and a method in operating the gas turbine unit wherein the electrical power is adjusted to a desired value by changing the geometry of the low pressure turbine and the heat power is adjusted by adjusting the bypass flow to a desired value.

REFERENCES:
patent: 2095991 (1937-10-01), Lysholm
patent: 3038308 (1962-06-01), Fuller
patent: 3335565 (1967-08-01), Aguet
patent: 3796045 (1974-03-01), Foster-Pegg
patent: 4132064 (1979-01-01), Kumm
patent: 4893466 (1990-01-01), Egnell et al.

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