Multistage compressor system with intercooler
US-12163518-B2 · Dec 10, 2024 · US
US10253774B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10253774-B2 |
| Application number | US-201214346704-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 29, 2012 |
| Priority date | Sep 26, 2011 |
| Publication date | Apr 9, 2019 |
| Grant date | Apr 9, 2019 |
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A compressor includes a closed container housing a compression element driven by the shaft of a motor. The compression element includes a first and second bearings supporting first and second shaft portions, and at least one cylinder having at least one cylinder chamber disposed between the first and second bearings. At least one roller is fitted to the shaft in the at least one cylinder chamber. The first bearing is disposed closer to the motor than the second bearing. The first and second bearings have first and second annular grooves opened to the at least one cylinder chamber and first and second elastic portions provided in first and second opposing surfaces, respectively. A diameter of the second shaft portion is smaller than a diameter of the first shaft portion. A rigidity of the second elastic portion is smaller than a rigidity of the first elastic portion.
Opening claim text (preview).
What is claimed is: 1. A compressor comprising: a closed container; a compression element disposed in the closed container; and a motor disposed in the closed container, the motor being configured and arranged to drive the compression element via a shaft, the compression element including a first bearing configured and arranged to support a first shaft portion of the shaft, a second bearing configured and arranged to support a second shaft portion of the shaft, and at least one cylinder disposed between the first bearing and second bearing, the at least one cylinder having at least one cylinder chamber the first bearing being disposed closer to the motor than the second bearing, the first bearing having a first annular groove opened to the at least one cylinder chamber and a first annular shaped elastic portion positioned radially inside of the first annular groove provided in a first opposing surface thereof that is opposed to the at least one cylinder, the second bearing having a disc-shaped end plate portion, a boss portion provided in a center of the end plate portion, and a second annular groove opened to the at least one cylinder chamber and a second annular shaped elastic portion positioned radially inside of the second annular groove provided in a second opposing surface thereof that is opposed to the at least one cylinder, with a depth of the second annular groove being smaller than a thickness of the disc-shaped plate portion, a diameter of the second shaft portion being smaller than a diameter of the first shaft portion, and a rigidity of the second elastic portion being smaller than a rigidity of the first elastic portion. 2. The compressor as claimed in claim 1 , wherein the depth of the second annular groove is larger than a depth of the first annular groove. 3. The compressor as claimed in claim 1 , wherein a first outer circumferential surface of the first elastic portion is formed into a cylindrical-surface shape so that a first diameter of the first outer circumferential surface becomes constant from a first cylinder chamber side toward a first counter cylinder chamber, and a second outer circumferential surface of the second elastic portion is formed into a taper shape so that a second diameter of the second outer circumferential surface gradually increases from a second cylinder chamber side toward a second counter cylinder chamber side. 4. The compressor as claimed in claim 3 , wherein a width of a second cylinder chamber side end portion of the second elastic portion is equal to or smaller than a width of a first cylinder chamber side end portion of the first elastic portion. 5. The compressor as claimed in claim 3 , wherein a width of a second cylinder chamber side end portion of the second elastic portion is smaller than a width of a first cylinder chamber side end portion of the first elastic portion. 6. The compressor as claimed in claim 1 , wherein a second cylinder chamber side width of the second annular groove is larger than a first cylinder chamber side width of the first annular groove. 7. A compressor comprising: a closed container; a compression element in the closed container; and a motor disposed in the closed container, the motor being configured and arranged to drive the compression element via a shaft, the compression element including a first bearing configured and arranged to support a first shaft portion of the shaft, a second bearing configured and arranged to support a second shaft portion of the shaft, and at least one cylinder disposed between the first bearing and second bearing, the at least one cylinder having at least one cylinder chamber, the first bearing being disposed closer to the motor than the second bearing, the first bearing having a first annular groove opened to the at least one cylinder chamber and a first annular shaped elastic portion positioned radially inside of the first annular groove provided in a first opposing surface thereof that is opposed to the at least one cylinder, the second bearing having a disc-shaped end plate portion, a boss portion provided in a center of the end plate portion, and a second annular groove opened to the at least one cylinder chamber and a second annular shaped elastic portion positioned radially inside of the second annular groove provided in a second opposing surface thereof that is opposed to the at least one cylinder, with a depth of the second annular groove being smaller than a thickness of the disc-shaped plate portion, a diameter of the second shaft portion being smaller than a diameter of the first shaft portion, a rigidity of the second elastic portion being smaller than a rigidity of the first elastic portion, a first outer circumferential surface of the first elastic portion being formed into a cylindrical-surface shape so that a first diameter of the first outer circumferential surface becomes constant from a first cylinder chamber side toward a first counter cylinder chamber side, and a second outer circumferential surface of the second elastic portion being formed into a taper shape so that a second diameter of the second outer circumferential surface gradually increases from a second cylinder chamber side toward a second counter cylinder chamber side. 8. The compressor as claimed in claim 2 , wherein a first outer circumferential surface of the first elastic portion is formed into a cylindrical-surface shape so that a first diameter of the first outer circumferential surface becomes constant from a first cylinder chamber side toward a first counter cylinder chamber side, and a second outer circumferential surface of the second elastic portion is formed into a taper shape so that a second diameter of the second outer circumferential surface gradually increases from a second cylinder chamber side toward a second counter cylinder chamber side. 9. The compressor as claimed in claim 2 , wherein a second cylinder chamber side width of the second annular groove is larger than a first cylinder chamber side width of the first annular groove. 10. The compressor as claimed in claim 3 , wherein a second cylinder chamber side width of the second annular groove is larger than a first cylinder chamber side width of the first annular groove. 11. The compressor as claimed in claim 4 , wherein a second cylinder chamber side width of the second annular groove is larger than a first cylinder chamber side width of the first annular groove. 12. The compressor as claimed in claim 5 , wherein a second cylinder chamber side width of the second annular groove is larger than a first cylinder chamber side width of the first annular groove. 13. The compressor as claimed in claim 7 , wherein a free end of the second annular elastic portion is disposed radially inwardly of the first annular elastic portion. 14. The compressor as claimed in claim 7 , wherein a second groove outer circumferential surface of the second annular groove is disposed radially inwardly of a first groove outer circumferential surface of the first annular groove. 15. The compressor as claimed in claim 1 , wherein a free end of the second annular elastic portion is disposed radially inwardly of the first annular elastic portion. 16. The compressor as claimed in claim 1 , wherein a second groove outer circumferential surface of the second annular groove is disposed radially inwardly of a first groove outer circumferential surface of the first annular groove.
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