In a compressor turbine the shaft of compressor and turbine is common. basically its a case of gas turbine plant...where power is devloped by this turbo compressor concept
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But in some gas turbine there are two separate shaft ( double shaft) , and in end of rotor compressor located two or more disc and stator that names CT (compressor turbine) , even in single shaft is too.
this department is located in hot section too , instead rotor compressor that located in cold section.
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