Gas compressor
US-2015132168-A1 · May 14, 2015 · US
US2018030833A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2018030833-A1 |
| Application number | US-201615550419-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 19, 2016 |
| Priority date | Feb 12, 2015 |
| Publication date | Feb 1, 2018 |
| Grant date | — |
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A gas compressor is configured such that a suction-side area that is in sliding contact with the inner circumferential surface of a cylinder chamber when a compression chamber is in the suction stroke has a larger radius of curvature than that of a compression-side area that is in sliding contact with the inner circumferential surface of the cylinder chamber when the compression chamber is in the compression stroke.
Opening claim text (preview).
1 . A gas compressor comprising: a cylinder block in a cylindrical shape, having a cylinder chamber where to compress refrigerant; a rotor rotatably provided in the cylinder chamber, the rotor having an outer circumferential surface facing an inner circumferential surface of the cylinder chamber and a plurality of vane slots opening on the outer circumferential surface with intervals in a rotational direction of the rotor; and a plurality of vanes housed in the respective vane slots and biased in a direction of protruding from the outer circumferential surface, distal end surfaces of the vanes sliding on the inner circumferential surface along with rotation of the rotor, the vanes partitioning a space between the outer circumferential surface and the inner circumferential surface into a plurality of compression chambers in which the refrigerant is sucked and compressed, wherein the distal end surface of each of the vanes has a suction-side area that is in sliding contact with the inner circumferential surface when the compression chamber separated by the vane having the distal end surface is in a suction stroke, and a compression-side area that is in sliding contact with the inner circumferential surface when the compression chamber separated by the vane having the distal end surface is in a compression stroke, the suction-side area and the compression-side area have smaller radii of curvature than that of the inner circumferential surface, and the suction-side area has a larger radius of curvature than that of the compression-side area. 2 . The gas compressor according to claim 1 , wherein the compression-side area has a single radius of curvature. 3 . The gas compressor according to claim 1 , wherein an upstream portion and a downstream portion of the distal end surface in the rotational direction of the rotor constitute the suction-side area and the compression-side area, respectively. 4 . The gas compressor according to claim 1 , wherein a center of curvature of the suction-side area and a center of curvature of the compression-side area are arranged on a normal line to the distal end surface at a connection point between the suction-side area and the compression-side area. 5 . The gas compressor according to claim 1 , wherein the connection point between the suction-side area and the compression-side area is arranged downstream of a middle point of the distal end surface in the rotational direction.
the inner and outer member being in contact along more than one line or surface · CPC title
the fluid being the working fluid · CPC title
the surfaces of the inner and outer member, forming the inlet and outlet opening · CPC title
using lift valves · CPC title
both members having co-operating elements in spiral form · CPC title
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