| 摘要 |
An integrated turbomachine (1) is described, comprising: a casing (3); an electric motor (5) and a driven turbomachine component (7) housed in the casing (3); a rotating shaft (15) drivingly connecting the electric motor (5) and the driven turbomachine component (7); a thrust bearing (27) and a radial bearing (21, 23, 25) rotatingly supporting the shaft (15); an axial locking device (51) housed inside the casing (3), for applying a thrust to the shaft (15), parallel to the rotation axis (A-A) of the shaft, and comprised of an actuator member (57), configured to selectively activate and/or deactivate the axial locking device. |
