The present invention is generally directed toward the filed of electric motors. More specifically, the present invention is directed to outer rotor-type electric motors. Still more specifically, the present invention is directed to rotors of outer rotor-type motors, which tend to be useful for use in direct drive clothes washing machines.
Direct drive clothes washing machine motor rotors are directly coupled to the shaft that drives the washing machine to transmit the torque produced by the motor. The types of rotors used in these applications until now fall within in two general categories: plastic rotors and steel rotors. Each general type is associated with advantages and disadvantages. For example, steel rotors, although relatively strong and durable, tend to be relatively heavy and costly. In contrast, plastic rotors tend to be lighter and less costly than steel rotors but because the plastic typically used is significantly less strong/durable than metal, such rotors must be designed to overcome this factor. Typically, the coupling geometry of a plastic rotor must be adjusted to provide a relatively large area of engagement with the drive shaft. This results in a plastic rotor typically having a relatively long axial length, which is not desirable especially for horizontal axis washing machines. Relatively, long axial lengths are not limited to plastic rotors, however, many, if not all, steel rotor designs tend to have relatively overall long axial lengths.
In view of the foregoing, a need still exists for a rotor having one or more of the following characteristics: relatively low cost, relatively short in axial length, relatively light weight, relatively strong/durable coupling with the drive shaft.
The present invention is directed to a rotor for an outer rotor-type electric motor, the rotor comprising a metallic coupler that comprises: an inner axial surface configured to interface with a shaft to be driven by the rotor when the motor is energized; and an outer axial surface that corresponds to a multiplicity of outer teeth. The rotor further comprising a polymeric frame that comprises a hub molded over at least the outer axial surface of the metal coupler; a base that is integrally formed with the hub and extending radially outward therefrom; a side wall that is integrally formed with the base; and a multiplicity of magnet spacers each of which is integrally formed with the side wall. The rotor further comprising a backing ring of a magnetic material molded over by the polymeric frame and having an outer axial surface in contact with the sidewall of the polymeric frame. The rotor still further comprising a multiplicity of permanent magnets in contact with an inner axial surface of the backing ring and molded over by the polymeric frame and spaced apart by the magnet spacers of the polymeric frame.
As mentioned above, the present invention is directed to a rotor for an outer rotor-type electric motor.
Referring to
Metallic Coupler
Referring to
The metallic coupler 10 further comprises an outer axial surface 13 that corresponds to a multiplicity of outer teeth 14. The outer teeth 14 may be of any configuration (e.g., number, size (e.g., axial length and radial height), shape (e.g., cross-section), spacing (e.g., circumferential)) that is appropriate for the particular application. More particularly, the foregoing configuration options may be selected in various combinations such that interface between the outer axial surface and a polymeric frame (described in greater detail below) is sufficiently secure and robust to withstand and transmit the torque produce by the motor during its useful lifetime. The outer teeth, for example, may be selected from the group consisting of knurls, splines, keys, diamond knurls, or combinations thereof. In one embodiment there are a multiplicity of outer teeth. For example, the number of outer teeth may be at least 10. In another embodiment, the number of outer teeth is least 20 and no more than about 40. In the embodiment depicted in
The metallic coupler 10 may further comprise one or more annular shoulders 15 radially inward of, and axially outward of each axial end of the outer axial surface 13 and wherein a hub 21 (see below for more a detailed description) is additionally molded over at least one of said annular shoulders 15 such that it is generally flush with axially outermost exterior surfaces 16 of the metallic coupler.
Polymeric Frame
The rotor of the present invention further comprises a polymeric frame 20 that comprises a hub 21 molded over at least the outer axial surface of the metal coupler 13. The hub has an outer diameter, ODhub, that is essentially the same as the nominal outer diameter of the couple, ODcoupler. The polymeric frame further comprises a base 22 that is integrally formed with the hub 21 and extending radially outward therefrom. The base has a thickness, Tbase, which corresponds to the greatest distance, measured axially, between any two points on the opposite sides of the base. The polymeric frames further comprise a side wall 23 that is integrally formed with the base 22, wherein the sidewall has a thickness, Tsidewall. Typically, Tbase is within the range of about 1.3 to about 3.5 mm (about 0.05 to about 0.14 in). For the embodiment depicted in
The base 22 of the polymeric frame 20 may comprise a one or more openings 25, which may provide benefits such as reduced weight and enhanced cooling. In one embodiment of the present invention the polymeric frame further comprises a multiplicity of openings 25. More specifically, the openings have a total surface area that is within a range that is from about 10% to about 30% of the nominal surface area of the base. More typically, the openings have a total surface area that is within a range that is from about 10% to about 20% of the nominal surface area of the base. For example, the embodiment depicted in
Reinforcement Ribs
The polymeric frame may comprise a multiplicity of reinforcement ribs 26, 27, 28 each of which integrally formed with at least the base. In the depicted embodiment of the present invention each reinforcement rib has a thickness, Trib, that is about equal to Tbase.
Spacer Ribs
One or more of said reinforcement ribs may be integrally formed with a magnets spacer and extend therefrom 26. These ribs may also extend to the hub and be integrally formed therewith. In the depicted embodiment the number of these “spacer ribs” corresponds to the number of magnet spacers
Concentric Ribs
One or more of said reinforcement ribs may be concentric with the hub 27. Further one or more reinforcement ribs 28 may extend from and be integrally formed with one or more of said concentric ribs.
Backing Ring
The rotor of the present invention further comprises a backing ring 30 having a thickness, Tbr, and a height, Hbr, of a magnetic material molded over by the polymeric frame 20 and having an outer axial surface 31 in contact with the sidewall 23 of the polymeric frame 20. Typically, Tbr is within the range of about 1.0 to about 5.0 mm (about 0.04 to about 0.20 in) and Hbr within the range of about 30 to about 45 mm (about 1.18 to about 1.17 in). In the embodiment depicted in
Magnets
The rotor of the present invention further comprises a multiplicity of permanent magnets 40 having a thickness, Tmagnet, and a height, Hmagnet, in contact with an inner axial surface 32 of the backing ring 30 and molded over by the polymeric frame 20 and spaced apart by the magnet spacers 24 of the polymeric frame 20. The magnets may be any appropriate material such as ferrite magnets. Typically, Tmagnet is within the range of about 5.0 to about 15.0 mm (about 0.20 to about 0.60 in) and Hmagnet within the range of about 30 to about 45 mm (about 1.18 to about 1.77 in). In the embodiment depicted in
Rotor Dimensions
The foregoing aspects of the rotor of present invention allow for the design and production of rotors that are able to operate in the clothes washing machines having one or more desirable characteristics such as relatively low cost, relatively short in axial length (especially in view of the ability to have a relatively large diameter), relatively light weight, relatively strong/durable coupling with the drive shaft. More particularly, the present invention may be used to produce a for a rotor to have one or more of the following characteristics:
Tbr may be about equal to Tsidewall and Hbr may be about equal to Tmagnet,
Hmagnet may be at least about 50% of the Hrotor,
Hmagnet may be at least about 55% of the Hrotor,
Hcoupler may be no more than about 45% of Hrotor,
Hcoupler may be no more than about 40% of Hrotor;
ODcoupler may be no more than about 20% of ODrotor;
ODcoupler may be no more than about 15% of ODrotor;
ODhub may be less than about 30% of ODrotor;
ODhub may be less than about 20% of ODrotor;
Tbase and Tsidewall may each be less than Tmagnet; and
Tbase and Tsidewall may each be about less than 70% of Tmagnet.
A rotor in accordance with that depicted in
As various modifications could be made in the constructions and methods herein described and illustrated without departing from the scope of the invention, it is intended that all matter contained in the foregoing description or shown in the accompanying drawings shall be interpreted as illustrative rather than limiting. Thus, the breadth and scope of the present invention should not be limited by the above-described exemplary embodiment, but should be defined only in accordance with the following claims appended hereto and their equivalents.
It should also be understood that when introducing elements of the present invention in the claims or in the above description of exemplary embodiments of the invention, the terms “comprising,” “including,” and “having” are intended to be open-ended and mean that there may be additional elements other than the listed elements. Additionally, the term “portion” should be construed as meaning some or all of the item or element that it qualifies. Moreover, use of identifiers such as first, second, and third should not be construed in a manner imposing any relative position or time sequence between limitations.
The present application claims the benefit of U.S. Provisional Application No. 61/374,578, filed Aug. 17, 2010, which is incorporated herein by reference in its entirety.
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