Rotor assembly for an electric excited synchronous motor (eesm)
US-2024429783-A1 · Dec 26, 2024 · US
US9866082B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9866082-B2 |
| Application number | US-201414163284-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 24, 2014 |
| Priority date | Jan 24, 2013 |
| Publication date | Jan 9, 2018 |
| Grant date | Jan 9, 2018 |
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The invention relates to a rotor and a motor and compressor comprising the rotor. The rotor comprises a rotor core defining an outer periphery, a bore concentric with a center of the rotor core, a plurality of magnet slots positioned on the outer periphery, and a plurality of oil holes located radially outward from the center between the bore and the magnet slots. Each oil hole includes a body portion and at least one projected portion. The projected portions are located radially outward from the body portions and positioned between the body portions and the magnet slots. The projected portions may increase the contact area of the compressor oil with the rotor core to effectively cool down the rotor core. Another advantage of the projected portions may be to further cool down the magnets in the magnet slots. Cooling the magnets may protect against their demagnetization.
Opening claim text (preview).
The invention claimed is: 1. A rotor comprising, a rotor core defining i) an outer periphery extending between opposing surfaces of the rotor core, ii) a bore concentric with a center axis of the rotor core, iii) a plurality of magnet slots positioned on the outer periphery, and iv) a plurality of oil holes configured to receive oil, the plurality of magnet slots each including a midpoint located on a diameter drawn through a center of a cross section taken orthogonal to the center axis of the rotor core, the plurality of oil holes located radially outward from the center between the bore and the magnet slots, each oil hole including a body portion and at least one projected portion having a pinnacle portion with a peak located on the diameter and extending to the midpoint of one of the magnet slots, the body portion and the at least one projected portion of said each oil hole extending from one of the opposing surfaces of the rotor core to the other opposing surface of the rotor core, the at least one projected portion of said each oil hole located radially outward from the body portion and positioned between the body portion and the magnet slots, the entirety of the at least one projected portion of one of the plurality of oil holes extending from the body portion of said one of the plurality of oil holes to a magnet slot of the plurality of magnet slots to allow the body portion and the at least one projected portion of said one of the plurality of oil holes and the magnet slot to form an integral oil hole. 2. The rotor of claim 1 , wherein in the cross section of the rotor core, each body portion is bounded between i) an inner circle boundary, the inner circle boundary capable of being drawn on the cross section concentric with the rotor core and radially outward from the bore, and ii) an outer circle boundary, the outer circle boundary capable of being drawn on the cross section concentric with the rotor core and located radially outward from the inner circle boundary and radially inward from the magnet slots. 3. The rotor of claim 2 , wherein each of the oil holes corresponds to a magnet slot of the plurality of magnet slots. 4. The rotor of claim 3 , characterized in that the rotor further includes magnets fixed in the magnet slots. 5. The rotor of claim 2 , further comprising magnets fixed in the magnet slots. 6. The rotor of claim 5 , wherein the quantity of the oil holes is equal to or a multiple of the number of magnets. 7. A motor comprising the rotor of claim 2 . 8. A compressor comprising the rotor of claim 2 , a hollow shaft and an oil pump, the hollow shaft located in the bore of the rotor core, the oil pump configured to transmit the oil to a top of the hollow shaft so that the oil flows into the plurality of oil holes which are between the hollow shaft and the magnet slots to cool the magnets. 9. The rotor of claim 2 , wherein the quantity of the oil holes is equal to or a multiple of the number of magnets slots. 10. The rotor of claim 9 , wherein each of the oil holes corresponds to a magnet slot of the plurality of magnet slots. 11. The rotor of claim 1 , wherein each of the oil holes corresponds to a magnet slot of the plurality of magnet slots. 12. The rotor of claim 11 , further comprising magnets fixed in the magnet slots. 13. The rotor of claim 1 , characterized in that the rotor further comprising magnets fixed in the magnet slots. 14. The rotor of claim 13 , wherein the quantity of the oil holes is equal to or a multiple of the number of magnets. 15. The rotor of claim 14 , wherein each of the oil holes corresponds to a magnet slot of the plurality of magnet slots. 16. A motor, comprising the rotor of claim 1 . 17. A compressor comprising the rotor of claim 1 , a hollow shaft and an oil pump, the hollow shaft located in the bore of the rotor core, the oil pump configured to transmit the oil to a top of the hollow shaft so that the oil flows into the plurality of oil holes which are between the hollow shaft and the magnet slots to cool the magnets. 18. The rotor of claim 1 , wherein the quantity of the oil holes is equal to or a multiple of the number of magnet slots. 19. The rotor of claim 18 , characterized in that each of the oil holes corresponds to a magnet slot. 20. A motor, characterized in that the motor comprises the rotor of claim 18 .
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