This gas dryer includes: a first drying tower having a first desiccant provided therein; and a second drying tower having a second desiccant provided therein. Either the first drying tower or the second drying tower is switched to a drying circuit side for drying hydrogen gas of an electric device, and another of the first drying tower or the second drying tower is switched to a reactivation circuit side for reactivating the first desiccant or the second desiccant provided therein. The gas dryer includes a cooler which is provided on the reactivation circuit side and which, with only supply of compressed air, generates air having such a temperature that can condense moisture in the gas on the reactivation circuit side.

This gas dryer includes: a first drying tower having a first desiccant provided therein; and a second drying tower having a second desiccant provided therein. Either the first drying tower or the second drying tower is switched to a drying circuit side for drying hydrogen gas of an electric device, and another of the first drying tower or the second drying tower is switched to a reactivation circuit side for reactivating the first desiccant or the second desiccant provided therein. The gas dryer includes a cooler which is provided on the reactivation circuit side and which, with only supply of compressed air, generates air having such a temperature that can condense moisture in the gas on the reactivation circuit side.

Aircraft electric motors are described. The aircraft electric motors include a cooling system comprising an annular heat exchanger, a motor housing arranged radially inward from the heat exchanger, the motor housing defining a rotor-stator cavity and a gear assembly cavity, a rotor sleeve arranged within the rotor-stator cavity, a gear assembly arranged within the gear assembly cavity, a first shaft operably coupled to the rotor sleeve and configured to be rotationally driven by the rotor sleeve to drive rotation of a portion of the gear assembly, and a second shaft operably coupled to the gear assembly and configured to be rotationally driven by the gear assembly.

Systems and methods are provided to cool a heat producing component in an electrical machine system. The electrical machine includes a supercritical carbon dioxide (SCO.sub.2) wherein the SCO.sub.2 is a working medium of a heat exchanger that is arranged in the electrical machine system to cool a fluid that cools the heat producing component and/or wherein the SCO.sub.2 directly cools at the heat producing component.

Systems and methods are provided to cool a heat producing component in an electrical machine system. The electrical machine includes a supercritical carbon dioxide (SCO.sub.2) wherein the SCO.sub.2 is a working medium of a heat exchanger that is arranged in the electrical machine system to cool a fluid that cools the heat producing component and/or wherein the SCO.sub.2 directly cools at the heat producing component.

A stator core is provided that can define a plurality of core slots in a surface thereof. The core slots can extend between a first and a second end portion of the stator core. A winding can be housed in the core slots. The winding can define a channel through at least a portion thereof. A cooling system can be operably coupled with the channel and can be configured to move a cooling fluid through the channel. A turbulator can be positioned within the channel. The turbulator can be within a flowpath of the cooling fluid and can be integrally formed with the winding.

A stator core is provided that can define a plurality of core slots in a surface thereof. The core slots can extend between a first and a second end portion of the stator core. A winding can be housed in the core slots. The winding can define a channel through at least a portion thereof. A cooling system can be operably coupled with the channel and can be configured to move a cooling fluid through the channel. A turbulator can be positioned within the channel. The turbulator can be within a flowpath of the cooling fluid and can be integrally formed with the winding.

A hydrogen expander magnetic generator apparatus can include a magnetic generator to recover energy. Embodiments can utilize a permanent magnetic motor (PM) and energy conversion system (ECS) for converting energy from a rotating shaft of a turboexpander. Some embodiments can position magnets on the shaft such that the magnets are protected from exposure to hydrogen to avoid damage to the magnets. Some embodiments can include retrofitting of a pre-existing expander to remove an oil brake and replace it with an embodiment of the PM and ECS.

A hydrogen expander magnetic generator apparatus can include a magnetic generator to recover energy. Embodiments can utilize a permanent magnetic motor (PM) and energy conversion system (ECS) for converting energy from a rotating shaft of a turboexpander. Some embodiments can position magnets on the shaft such that the magnets are protected from exposure to hydrogen to avoid damage to the magnets. Some embodiments can include retrofitting of a pre-existing expander to remove an oil brake and replace it with an embodiment of the PM and ECS.

A stator for an electric rotary machine includes: a stator core which has plural slots; and segmented coils of a plurality of phases, wherein: the stator core is provided with a base plate at least one side thereof in an axial direction; the segmented coils of the plurality of phases include plural slot coils which are individually disposed in the plural slots of the stator core and which extend substantially linearly, and plural connection coils which are individually disposed in the base plate and which make up bridge portions by connecting the slot coils of a same phase together; the connection coil is accommodated in a connection coil accommodating groove formed on a front surface of the base plate; and the base plate is provided with a communication portion on an outer circumferential surface thereof for communicating with the connection coil accommodating groove.