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Turbomachine for use as generator, has blades rotating around respective axles parallel to rotation axle of rotor, where axles of blades are disposed in circle on rotor and positioning of blades is similar for each angular position of rotor
Turbomachine for use as generator, has blades rotating around respective axles parallel to rotation axle of rotor, where axles of blades are disposed in circle on rotor and positioning of blades is similar for each angular position of rotor
The turbomachine has blades (5) rotating around respective axles (6) parallel to a rotation axle (11) of a rotor, where the axles (6) are disposed in circle on the rotor. The rotation of the blades is synchronized such that each blade carries out a half rotation for one turn of the rotor. The positioning of different blades is similar for each angular position of the rotor with respect to a stator (1). An independent claim is also included for a compression device comprising two turbomachines placed in series.
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