Title:
METHOD OF OPERATION OF A GAS TURBINE ENGINE POWER PLANT AND A GAS TURBINE ENGINE POWER PLANT
Document Type and Number:
WIPO Patent Application WO2000053907
Kind Code:
A8
Abstract:
A gas turbine engine that has a turbine (1) mounted downstream of a combustor (5), a compressor turbine (2) mounted downstream of turbine (1) for producing power for driving a compressor (3), a heat exchanger (6) having a first circuit (6<1>) connected to compressor turbine (2) and a second circuit (6<2>) connected between compressor (2) and turbine (1) and a fluid discharge device (7) between compressor (3) and combustor (5). The gas turbine engine has a reactor (8) that has a heating device (9), inlets (F, W) connected to sources of fuel and water and an outlet connected to combustor (5). Heating device (9) is connected to the outlet of compressor turbine (2). The engine also has a system for keeping the temperature at the outlet of compressor turbine (2) constant.
Inventors:
RAKHMAILOV ANATOLY
Application Number:
PCT/US2000/003711
Publication Date:
February 08, 2001
Filing Date:
March 10, 2000
Export Citation:
Assignee:
ALM DEV INC (US)
International Classes:
F02C3/067; F02C3/10; F02C3/20; F02C3/28; F01D15/10; F02C3/34; F02C6/18; F02C7/08; F02C9/00; F02C9/28; (IPC1-7): F02C3/067; F02C7/08; F02C9/28; F02C3/28
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