To put a whole moving blade gas turbine and a whole moving blade steam turbine to practical use by properly selecting a double inversion magnetic bearing for journalling an outer shaft device and an inner shaft device, and respective rotational speed ratios, and arranging at least two pairs of magnetic power transmissions for property distributing rotational output of the total moving blade turbine.

An outer side compression moving blade barrel device and an inner side compression moving blade barrel device are composed by integrally casting a first stage compressor moving blade group 1, an even-numbered stage compressor moving blade group 9, an odd-numbered stage compressor moving blade group 2, and a final stage compressor moving blade group 3, respectively in circular form and in inner and outer directions diametrally, followed by fixing and assembling. Similarly, an outer turbine moving blade device and an inner turbine moving blade device are composed of a first stage turbine moving blade group 4, an even-numbered turbine moving blade group 10, an odd-numbered stage turbine moving blade group 5, and a final stage turbine moving blade group 6. They are journalled by means of a double inversion magnetic bearing, for connecting power. It is thus possible to put various whole moving blade gas turbines and whole moving blade steam turbines into practice.