Patent ID: 11680526

Abstract:
The gas turbine system includes: a first gas turbine element 2; a second gas turbine element 3; a single combustor 4; a first supply pipe 61 which connects the first compressor 21 to the combustor 4; a second supply pipe 62 which connects the second compressor 31 to the combustor 4; a first discharge pipe 66 and a second discharge pipe 67 which discharge a fluid discharged from the combustor 4 to the outside; and a heat exchanger 5. The heat exchanger 5 allows each of a low-temperature fluid flowing through the first supply pipe 61 and the second supply pipe 62 and a high-temperature fluid flowing through the first discharge pipe 66 and the second discharge pipe 67 to flow therethrough and exchanges heat between the low-temperature fluid and the high-temperature fluid.