Patent Application
20230261535
Turbomachines are well known and used in a variety of applications, such as pumps. One type of turbomachine includes a stator that can be electrically energized to rotationally drive a rotor.
A machine according to an exemplary aspect of the present disclosure includes a stator, and a rotor that is rotatable with respect to the stator. The rotor includes a shaft that has a paramagnetic shell that defines a cavity therein, and a magnet at least is partially disposed in the cavity. The magnet is of complementary shape to the cavity such that the magnet and paramagnetic shell are rotationally interlocked.
In a further embodiment of the foregoing machine, the paramagnetic shell is selected from a titanium-based alloy or an aluminum-based alloy.
In a further embodiment of any of the foregoing machines, the shaft includes an elongated stem portion extending from the paramagnetic shell. The paramagnetic shell defines a first outer diameter and the elongated stem portion defines a second outer diameter that is less than the first outer diameter.
In a further embodiment of any of the foregoing machines, the elongated stem and the paramagnetic shell are of single-piece construction.
In a further embodiment of any of the foregoing machines, the shaft further includes a cap enclosing the magnet in the cavity.
In a further embodiment of any of the foregoing machines, the magnet includes at least one flat side.
In a further embodiment of any of the foregoing machines, the magnet includes first and second parallel flat sides.
In a further embodiment of any of the foregoing machines, the magnet and the cavity are of matching cross-sectional shapes.
In a further embodiment of any of the foregoing machines, the magnet and the cavity are of matching stadium cross-sectional shapes.
In a further embodiment of any of the foregoing machines, the magnet includes a center bore.
In a further embodiment of the any of the foregoing machines, the machine includes a housing in which the rotor is disposed and an impeller that is coupled with the shaft.
A rotor for a machine according to another exemplary aspect of the present disclosure includes a shaft having a paramagnetic shell that defines a cavity therein, and a magnet disposed in the cavity. The magnet is of complementary shape to the cavity such that the magnet and paramagnetic shell are rotationally interlocked.
In a further embodiment of the foregoing rotor, the paramagnetic shell is selected from a titanium-based alloy or an aluminum-based alloy.
In a further embodiment of any of the foregoing rotors, the shaft includes an elongated stem portion extending from the paramagnetic shell. The paramagnetic shell defines a first outer diameter and the elongated stem portion defining a second outer diameter that is less than the first outer diameter.
In a further embodiment of any of the foregoing rotors, the magnet and the cavity are of matching cross-sectional shapes.
In a further embodiment of any of the foregoing rotors, the elongated stem and the paramagnetic shell are of single-piece construction.
In a further embodiment of any of the foregoing rotors, the rotor includes a cap enclosing the magnet in the cavity.
In a further embodiment of any of the foregoing rotors, the magnet includes first and second parallel flat sides.
A machine according to another exemplary aspect of the present disclosure includes a stator, and a rotor including a shaft having a paramagnetic metallic alloy shell that defines a cavity therein, and a magnet disposed in the cavity. The magnet is rotationally interlocked with the paramagnetic shell such that when the stator energizes the magnet rotational energy of the magnet transmits to the paramagnetic shell and rotates the rotor.
In a further embodiment of the foregoing machine, the magnet and the cavity are of matching cross-sectional shapes, and the paramagnetic metallic alloy shell is selected from a titanium-based alloy or an aluminum-based alloy.
The various features and advantages of the present disclosure will become apparent to those skilled in the art from the following detailed description. The drawings that accompany the detailed description can be briefly described as follows.
In general, the machine 20 includes an outer housing 22 in which a stator 24 and rotor 26 are mounted. The stator 24 is fixed about an axis A, which is the rotational axis of the rotor 26. The rotor 26 is comprised of a shaft 28 and a magnet 30. The shaft may be supported on bearings (not shown). The magnet 30 is a permanent magnet, such as a rare earth magnet. An impeller 32 is coupled on the shaft 30 for co-rotation therewith. The stator 24 includes a coil that may be energized by an electric current to rotationally energize the magnet 30 and thereby rotate the shaft 28 and impeller 32. The system can be reversed such that the impeller is replaced by a turbine and the magnet can energize the coil in the stator to generate an electrical current.
In this example, the paramagnetic shell 36 and the stem portion 34 are of single-piece construction, which may facilitate enhancing strength and reducing performance variations in comparison to multi-piece configurations. For example, the paramagnetic shell 36 and the stem portion 34 are a monolithic body. The monolithic body is a single, continuous piece, as opposed to a collection of functional parts that are bonded, secured, or fused together in joints. For example, a monolithic body may be formed by casting, additive manufacturing, and/or machining. The paramagnetic shell 36 and the stem portion 34 are formed of a paramagnetic alloy, such as but not limited to, titanium-based alloys or aluminum-based alloys.
The paramagnetic shell 36 defines a cavity 40 therein. The cavity 40 is bound by an axial wall 40a and a radial wall 40b. The opposed axial side is bound by the cap 38. Together, the axial wall 40a, the radial wall 40b, and the cap 38 define the shape of the cavity 40. Optionally, if infiltration of working fluid into the cavity 40 is undesired, a seal may be provided around the perimeter of the cap 38 for hermetically sealing the cavity 40.
Referring also to
As shown, the cavity 40 and the magnet 30 have matching stadium cross-sectional shapes, represented at 44a and 44b, respectively. The stadium cross-sectional shape has two flat, parallel or substantially parallel sides that are bound with curved ends, such as semi-circles. In alternate examples, the magnet 30 has at least one flat side. The shape of the cavity 40 and the magnet 30 may be modified as long as they are of complimentary shape and rotationally interlock. Other example shapes include, but are not limited to, oval and rectangle.
During operation of the machine 20, the stator 24 is energized to energize the magnet 30. In response, the magnet 30 rotates about axis A. Due to the rotational interlocking of the magnet 30 with the paramagnetic shell 36, the rotational energy of the magnet 30 imparts torque on the paramagnetic shell 36 thereby causing rotation of the rotor 26 (and impeller 32). For instance, the paramagnetic shell 36 reacts shaft 28 bending loads and transmits magnet 30 torque due to stator 24 electric field interaction and reacts rotating assembly bending loads so that the magnet 30 only sees primarily the torque contact load transmitted to the paramagnetic shell 36.
The paramagnetic shell 36 is located between the stator 24 and the magnet 30 and, therefore, is in the magnetic field generated by the stator 24. However, the paramagnetic character of the shell 36 facilitates limiting magnetic interference and losses due to eddy currents. Additionally, the paramagnetic shell 36 may be relatively thin to further reduce interference. As an example, at its thinnest, the paramagnetic shell 36 has a wall thickness of less than about 0.5 millimeters up to about 7 millimeters. The actual selected thickness may take into account the material, application requirements, stresses resulting from speeds and size, and field strength. Moreover, titanium-based alloys, such as but not limited to Ti-6Al-4V, may also provide good strength across a wide range of operating temperatures, resistance to hydrogen embrittlement, and good performance at cryogenic temperatures with exposure to liquid hydrogen or liquid oxygen.
Although a combination of features is shown in the illustrated examples, not all of them need to be combined to realize the benefits of various embodiments of this disclosure. In other words, a system designed according to an embodiment of this disclosure will not necessarily include all of the features shown in any one of the Figures or all of the portions schematically shown in the Figures. Moreover, selected features of one example embodiment may be combined with selected features of other example embodiments.
The preceding description is exemplary rather than limiting in nature. Variations and modifications to the disclosed examples may become apparent to those skilled in the art that do not necessarily depart from this disclosure. The scope of legal protection given to this disclosure can only be determined by studying the following claims.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US2020/041378 | 7/9/2020 | WO |
