The present application provides a radial counter flow jet gas cooling system for a rotor of a dynamoelectric machine. The radial counter flow jet gas cooling system may include a centering pin, a number of axial inlet ducts, a number of radial outlet ducts in communication with the axial inlet ducts, an axial subslot positioned about the axial inlet ducts, and a radial counter flow duct in communication with the axial subslot and extending along the centering pin.

An active magnetic bearing apparatus for supporting a rotor of a rotary machine comprises an axial magnetic bearing unit and a radial magnetic bearing unit mounted directly to one another. One of the axial magnetic bearing unit and the radial magnetic bearing unit is mounted to a support for attachment to a housing of the rotary machine.

An active magnetic bearing apparatus for supporting a rotor of a rotary machine comprises an axial magnetic bearing unit and a radial magnetic bearing unit mounted directly to one another. One of the axial magnetic bearing unit and the radial magnetic bearing unit is mounted to a support for attachment to a housing of the rotary machine.

A stator cooling housing for a stator of a rotary electric motor includes a cylindrical frame adapted to be mounted around an iron core and having an outer lateral surface and inlet and outlet channels. A cylindrical jacket is arranged against the outer lateral surface of the cylindrical frame. The cylindrical jacket comprises an inner side having a plurality of cylindrical grooves forming with the outer lateral surface of the cylindrical frame adjacent fluid cooling channels arranged around the cylindrical frame from a frame upper portion to a frame lower portion. Fluid communication portions are arranged such that a cooling fluid is enabled to run from the inlet channel, through the adjacent fluid cooling channels from the frame upper portion to the frame lower portion, and through the outlet channel to form a cooling circuit.

A stator cooling housing for a stator of a rotary electric motor includes a cylindrical frame adapted to be mounted around an iron core and having an outer lateral surface and inlet and outlet channels. A cylindrical jacket is arranged against the outer lateral surface of the cylindrical frame. The cylindrical jacket comprises an inner side having a plurality of cylindrical grooves forming with the outer lateral surface of the cylindrical frame adjacent fluid cooling channels arranged around the cylindrical frame from a frame upper portion to a frame lower portion. Fluid communication portions are arranged such that a cooling fluid is enabled to run from the inlet channel, through the adjacent fluid cooling channels from the frame upper portion to the frame lower portion, and through the outlet channel to form a cooling circuit.

A rotor assembly and motor having the rotor assembly is described. The rotor assembly includes a rotor core formed from a plurality of rotor sheets, each rotor sheet having a cross section shape defining a plurality of magnet retaining tabs, the magnet retaining tabs defining a magnet receiving gap and at least one magnet shaped to be installed within the magnetic receiving gap.

A power plant and method for operating a power plant having a gas turbine and a generator which are arranged on a section, a shaft which connects the gas turbine to the generator in order to transmit a force, and a clutch which is arranged in the shaft between the gas turbine and the generator such that the shaft includes at least two sub-shafts, a first sub-shaft between the generator and the clutch and a second sub-shaft, which is referred to as a gas turbine intermediate shaft, between the gas turbine and the clutch. An electric motor is arranged in the section between the clutch and the gas turbine in order to accelerate the gas turbine.

A power plant and method for operating a power plant having a gas turbine and a generator which are arranged on a section, a shaft which connects the gas turbine to the generator in order to transmit a force, and a clutch which is arranged in the shaft between the gas turbine and the generator such that the shaft includes at least two sub-shafts, a first sub-shaft between the generator and the clutch and a second sub-shaft, which is referred to as a gas turbine intermediate shaft, between the gas turbine and the clutch. An electric motor is arranged in the section between the clutch and the gas turbine in order to accelerate the gas turbine.

A synchronous electrical machine includes a stator having a circumferential row of teeth carrying stator windings. The electrical machine further includes a coaxial rotor having a circumferential row of poles carrying field windings. Each pole has first and second side flanks and a tip surface which extends continuously there between to form an air gap to the teeth of the stator. On a transverse cross-section through the machine, one of the side flanks forms a leading edge of the pole, and the other side flank forms an opposite, trailing edge of the pole. Each pole carries a row of permanent magnets which extends across the tip surface from one of the side flanks to the other side flank, the permanent magnets compensating for armature magnetic reaction. The radial thickness of the permanent magnets increases smoothly with progressive distance across the tip surface from one of the side flanks to the other side flank.

A stacked motor assembly for an aircraft includes a forward motor having an exhaust port and an aft motor disposed aft of the forward motor, the aft motor having an intake port. The stacked motor assembly includes an exhaust conduit originating from the exhaust port of the forward motor and disposed at least partially around the aft motor such that exhaust from the forward motor bypasses the aft motor. The stacked motor assembly also includes an intake conduit terminating at the intake port of the aft motor and disposed at least partially around the forward motor such that intake air for the aft motor bypasses the forward motor.