Abstract: A turbomachine has at least one rotor disk that is attached at an overhung end of a mounted first shaft, and an electric rotor of an electric machine that is connected with the end of the first shaft that lies opposite the rotor disk, by way of a coupling. The electric rotor is arranged between the first shaft and a second shaft, mounted so as to rotate, which is oriented in alignment with the first shaft, and is also connected with the electric rotor by way of a coupling. The electric rotor is arranged between the couplings as a coupling intermediate piece, without any mounting of its own, and has coupling elements that work together with coupling elements on the shaft ends, without radial play.

Abstract: An expansion turbine stage for compressed gases has a housing and a turbine rotor. The housing has flow guide channels for feeding the compressed gas to the turbine rotor. The turbine rotor, which is over-mounted and has centripetal flow through it, is followed by an out-flow diffuser enclosed by the housing, to delay the cold expanded gas. The out-flow diffuser is arranged in a holder bore in the housing, as a separate component. For thermal insulation of the housing relative to the cold expanded gas stream, the out-flow diffuser is made of a non-metallic material having a low heat conductivity.

Abstract: A rotor of an expansion turbine for low-temperature applications that comprises a turbine rotor, wherein a cold gas is admitted and flows through the rotor centripetally. There is also a turbine shaft. There is also a stud screw that can be inserted in a threaded bore of the turbine shaft on the face side of the shaft that extends through the turbine rotor. There is also a rotor nut mounted on the protruding end of the stud screw. The turbine rotor is secured on the end of the turbine shaft in an overhung manner with the help of the rotor nut and the pre-tensioned stud screw. A rotor hub cap consisting of a heat-insulating material is mounted on the free end of the stud screw protruding into the cold gas flowing off, as well as on the rotor nut.

Abstract: A turbo-machine includes a housing (1); a rotor (3) of a centripetally flow-through expansion turbine stage (4) overhung on the one end of the rotor shaft; a rotor of a radially flow-through compressor stage (6) overhung on the other end of the rotor shaft; a measuring system (7) for directly detecting an axial thrust of the rotor shaft (2) supported in roller bearings (8); and at least two pressure control valves (10, 11), which are installed in control lines (12, 13) and controlled by a controller (9). Via the control lines (12, 13), a rotor piston surface (14), which is sealed against the housing (1) and located on the rear side of one of the rotors, for example the compressor rotor (5), can be acted upon by the pressure (p1) prevailing on the inlet into the compressor stage, and the pressure (p2) on the outlet of the compressor stage (6).

Abstract: A rotor of an expansion turbine for low-temperature applications that comprises a turbine rotor, wherein a cold gas is admitted and flows through the rotor centripetally. There is also a turbine shaft. There is also a stud screw that can be inserted in a threaded bore of the turbine shaft on the face side of the shaft that extends through the turbine rotor. There is also a rotor nut mounted on the protruding end of the stud screw. The turbine rotor is secured on the end of the turbine shaft in an overhung manner with the help of the rotor nut and the pre-tensioned stud screw. A rotor hub cap consisting of a heat-insulating material is mounted on the free end of the stud screw protruding into the cold gas flowing off, as well as on the rotor nut.

Abstract: A turbo-machine includes a housing (1); a rotor (3) of a centripetally flow-through expansion turbine stage (4) overhung on the one end of the rotor shaft; a rotor of a radially flow-through compressor stage (6) overhung on the other end of the rotor shaft; a measuring system (7) for directly detecting an axial thrust of the rotor shaft (2) supported in roller bearings (8); and at least two pressure control valves (10, 11), which are installed in control lines (12, 13) and controlled by a controller (9). Via the control lines (12, 13), a rotor piston surface (14), which is sealed against the housing (1) and located on the rear side of one of the rotors, for example the compressor rotor (5), can be acted upon by the pressure (p1) prevailing on the inlet into the compressor stage, and the pressure (p2) on the outlet of the compressor stage (6).

Abstract: An expansion turbine for low-temperature applications containing a turbine stage into which a cold gas is admitted. A turbine rotor is mounted on a shaft. Also provided is a roller support for the shaft being lubricated with a minimum amount of oil or grease. The roller support contains a roller bearing located adjacent to the turbine stage. The roller bearing is comprised of an inner bearing ring, rollers, and an outer bearing ring supported on the side of the housing. An insulating bush made of ceramic engineering material is arranged between the inner bearing ring and the shaft. The bush thermally separates the inner bearing ring from the cold shaft.

Abstract: A bearing arrangement for turbo-machines containing a bearing housing, a rotor mounted on a rotor shaft in an overhung position, and a roller bearing set. The roller bearing set contains at least two roller bearings arranged on a one-part cylindrical bearing carrier with a minimum installed clearance. The bearing carrier is inserted into a bearing bore of the bearing housing leaving a radial installed gap that permits dampened movements of vibration. The carrier is supported on the peripheral side of the bore with initially tensioned, elastic vibration damping elements.

Abstract: An expansion turbine for low-temperature applications containing a turbine stage into which a cold gas is admitted. A turbine rotor is mounted on a shaft. Also provided is a roller support for the shaft being lubricated with a minimum amount of oil or grease. The roller support contains a roller bearing located adjacent to the turbine stage. The roller bearing is comprised of an inner bearing ring, rollers, and an outer bearing ring supported on the side of the housing. An insulating bush made of ceramic engineering material is arranged between the inner bearing ring and the shaft. The bush thermally separates the inner bearing ring from the cold shaft.

Abstract: A turbine has a housing, an impeller centered on and rotatable about an axis in the housing, and an axle assembly in the housing having a large-diameter mounting part and a small-diameter bearing stem centered on the axis and extending into the impeller. A sun gear traversed by the bearing stem is fixed to the impeller and forms with the impeller a rotor having a center of mass spaced axially a predetermined distance from the large-diameter mounting part. A ring gear rotatable in the housing about the axis around the sun gear meshes with planet gears rotatable on the housing about respective planet axes radially equispaced from and angularly equispaced about the impeller axis. Each planet gear meshes inwardly with the sun gear. A bearing supports the rotor on the stem of the axle assembly at a bearing location spaced from the large-diameter mounting part by a distance equal to between 0.4 and 1.2 times the predetermined distance between the center of mass and the mounting part.

Abstract: A turbine has a housing, an impeller centered on and rotatable about an axis in the housing, and a small-diameter bearing stem centered on the axis, fixed on the housing, and extending from an attachment location on the housing toward the impeller. A pinion traversed by the bearing stem is fixed to the impeller and forms with the impeller a rotor having a center of mass spaced axially a predetermined distance from the attachment location. A gear rotatable on the housing adjacent the axis and meshing with the pinion is supported on the stem by an inner bearing engaged between the pinion and the stem. An outer bearing supports the rotor on the stem of the axle assembly at a bearing location spaced from the attachment location by a distance equal to between 0.4 and 1.2 times the predetermined distance between the center of mass and the attachment location.