GAS TURBINE SYSTEM WITH HEAT RECOVERY CYCLE AND METHOD FOR USING THE SAME

摘要

A gas compressor system (102) comprising: (a) a gas turbine unit directly coupled to a gas compressor (102) for supplying compressed gas to a gas transmission line and producing hot exhaust gases; 1766 ז' באב התשס" ד - July 25, 2004 (b) a heat recovery heat exchanger system (110) containing organic working fluid responsive to heat contained in said hot exhasut gases for producing organic fluid and cooled gases which are vented; (c) an organic vapor turbine (111) responsive to said vaporized working fluid for generating power and from which expanded working fluid exits; (d) an air-cooled condenser (113) for condensing said expanded vaporized working fluid, and a pump (114) for returning exchanger system; and (e) an intermediate heat transfer fluid cycle (104, 106, 108) for transferring heat from said hot exhaust gases of the gas turbine unit to said organic working fluid.