| 摘要 |
A rotor assembly A for use in a turbine (10) that has a rotor (12) supported in a turbine compressor casing (32) of the turbine (10) for rotational movement of the rotor (12) about a rotor axis. The rotor assembly A comprises a first gas flow assembly (16) positioned within the turbine compressor casing (32) and around the rotor (12). The first gas flow assembly (16) has a plurality of nozzles (102) that are removeably attached to an inner circumference 1 (14 )of the rotor (12), each nozzle (102) having a nozzle inlet (116), a nozzle outlet (118) and a nozzle blade disposed there between. The rotor assembly A further comprises a heat assembly (14) partially positioned within the turbine compressor casing (32) of the rotor (12).
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