| 摘要 |
The invention relates to a production method and to an assembly for a gas turbine system having a low output, which can be used as a shaft output gas turbine, a hot gas generator or as an air supplier. The aim of the invention is to provide a method with which small gas turbines can be produced with the most cost-effective components. The novel method is characterized in that at least one exhaust gas turboblower ( 1 ) of internal combustion engines, and air heaters ( 11, 12 ) that are manufactured or adapted with regard to the output parameters of the exhaust gas turboblower are joined to additional subassemblies, which are also adapted to said exhaust gas turboblower, in order to form a gas turbine. The outlet of the compressor ( 5 ) of the exhaust gas turboblower ( 1 ) is connected to the gas producer i.e. to the combustion chamber ( 12 ).
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