REHEATED GAS TURBINE SYSTEM, IN PARTICULAR SUCH A SYSTEM HAVING A FUEL CELL

摘要

The present invention relates to (with reference to FIG. 2) a gas turbine system comprising: a gas compressor (210); an upstream heat source, e.g. a fuel cell (212), which receives gas compressed by the compressor (210) and heats the gas passing therethrough (and when a fuel cell generates electrical power); an intermediate turbine (220) which receives the gas previously heated in the upstream heat source and which is connected to and drives the compressor (210); and an output turbine (240) which receives gas output by the intermediate turbine (220). Expanded gas leaving the intermediate turbine passes to the output turbine through either or both of a downstream combustion chamber and/or a downstream fuel cell, whereby the expanded gas is reheated prior to expansion in the output turbine (240). Preferably the system is configured such that the temperature of the gas received by the output turbine (240) is higher than the temperature of the gas received by the intermediate turbine (220).