High temperature compression and reheat gas turbine cycle and re

Power plants – Combustion products used as motive fluid

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Details

60 3915, 60 3917, F02C 600

Patent

active

060791977

ABSTRACT:
A high temperature compression and reheat gas turbine system, and method for operating the system, is disclosed. The system includes a low temperature compressor, a combustor, a high pressure turbine, a high temperature compressor, a reheat combustor, and a low pressure turbine. The high pressure turbine only partially expands the process gas. The high pressure compressor compresses the high pressure turbine exit gas stream before a reheat combustor raises the process gas stream enthalpy entering the low pressure turbine.

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