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1. A turbine system comprising:
a first housing; a second housing; at least one compressor unit configured to compress a fluid; at least one intercooler configured to cool the fluid discharged from the at least one compressor unit; a combustor unit configured to burn fuel with the compressed fluid; a turbine unit configured to be driven due to a combustion gas that is generated when the combustor unit burns the fuel; a recuperator configured to heat the fluid compressed by the at least one compressor unit, by using at least an exhaust gas discharged from the turbine unit; and a first device configured to receive power that is generated when the turbine unit is driven, wherein the at least one compressor unit is configured to operate using at least the generated power, and is separately disposed from at least one of the turbine unit and the first device, wherein the first housing accommodates at least the at least one compressor unit and the at least one intercooler, wherein the second housing accommodates at least the combustor unit, the recuperator, and the first device, and wherein the first and second housings are separated by space in an extending direction of a first rotational shaft mechanically coupled to the at least one compressor unit.
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