System for heavy duty gas turbine combustion chamber and turbine component level test

The invention discloses a system for a heavy duty gas turbine combustion chamber and turbine component level test. The system comprises a test system, an electrical control system and a data acquisition system. The test system comprises a main gas supply unit, and the gas supply unit is sequentially communicated with a temperature adjusting device, a combined test section and a plurality of groups of steam exhaust sliding sections; the combined test section comprises a combustion chamber test section and a turbine test section, the combustion chamber test section is connected with a combustion unit, and the turbine test section is connected with the multiple groups of steam exhaust sliding sections; the combustion chamber test section comprises a combustion chamber cylinder body, the turbine test section and the combustion chamber cylinder body are detachably provided with a turbine cylinder body, and turbine blades are arranged between the turbine cylinder body and the combustion chamber cylinder body; and t