Two-stage refrigerant compressor and operation method thereof
US-2024418169-A1 · Dec 19, 2024 · US
US9004888B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9004888-B2 |
| Application number | US-201314065263-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 28, 2013 |
| Priority date | Oct 30, 2012 |
| Publication date | Apr 14, 2015 |
| Grant date | Apr 14, 2015 |
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A rotary compressor includes a compression unit that includes an annular cylinder including a cylinder inner wall, a suction port, and a vane groove, an end plate covering an end portion of the cylinder, an annular piston revolving in the cylinder to form an actuation chamber between the cylinder inner wall and the annular piston; and a vane protruding into the actuation chamber to divide the actuation chamber into a suction chamber and a compression chamber. A discharge port, which is provided in the end plate near the vane groove, communicates with the compression chamber, and a discharge groove, which is provided in the cylinder inner wall near the vane groove, communicates the compression chamber with the discharge port, and one side end portion of the discharge groove is located in an end portion of a wall portion of the vane groove on the compression chamber side.
Opening claim text (preview).
What is claimed is: 1. A rotary compressor comprising: a compression unit including: an annular cylinder including a suction port and a vane groove which are radially provided to a side portion of the annular cylinder; an end plate which covers an end portion of the cylinder; an annular piston which is fitted into an eccentric portion of a rotary shaft rotated by a motor and revolves in the cylinder along a cylinder inner wall of the cylinder so as to form an actuation chamber between the cylinder inner wall and the annular piston; and a vane which protrudes into the actuation chamber from an inside of the vane groove provided in the cylinder so as to abut against the annular piston and divide the actuation chamber into a suction chamber and a compression chamber, wherein a discharge port is provided in the end plate near the vane groove, the discharge port communicates with the compression chamber, and a part of the discharge port is located outside the cylinder inner wall, and a discharge groove is provided in the cylinder inner wall near the vane groove, the discharge groove communicates the compression chamber with the discharge port, and one side end portion of the discharge groove is located in an end portion of a wall portion of the vane groove on a compression chamber side, wherein the discharge groove is formed in a semicircular shape with a curvature radius R 2 which is equal or approximate to a radius R 1 of the discharge port, the semicircular shape inclining in a manner that a depth of the discharge groove becomes deeper as a position within the semicircular shape approaches the end plate, a center of the curvature radius R 2 being formed so as to be offset by a predetermined angle from a center of the discharge port to a vane groove side. 2. The rotary compressor according to claim 1 , wherein the rotary compressor is a two cylinder type or a two stage compression type. 3. A rotary compressor comprising: a compression unit including: an annular cylinder including a suction port and a vane groove which are radially provided to a side portion of the annular cylinder; an end plate which covers an end portion of the cylinder; an annular piston which is fitted into an eccentric portion of a rotary shaft rotated by a motor and revolves in the cylinder along a cylinder inner wall of the cylinder so as to form an actuation chamber between the cylinder inner wall and the annular piston; and a vane which protrudes into the actuation chamber from an inside of the vane groove provided in the cylinder so as to abut against the annular piston and divide the actuation chamber into a suction chamber and a compression chamber, wherein a discharge port is provided in the end plate near the vane groove, the discharge port communicates with the compression chamber, and a part of the discharge port located outside the cylinder inner wall, and a discharge groove is provided in the cylinder inner wall near the vane groove, the discharge groove communicates the compression chamber with the discharge port, and one side end portion of the discharge groove is located in an end portion of a wall portion of the vane groove on a compression chamber side, wherein the discharge groove is formed in a semicircular shape with a curvature radius R 3 which is larger than a radius R 1 of the discharge port, the semicircular shape inclining in a manner that a depth of the discharge groove becomes deeper as a position within the semicircular shape approaches the end plate, and communicates with a majority of a part of the discharge port located outside the cylinder inner wall. 4. The rotary compressor according to claim 3 , wherein the rotary compressor is a two cylinder type or a two stage compression type.
with inlet and outlet valves specially adapted for rotary or oscillating piston pumps · CPC title
Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet · CPC title
of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth equivalents than the outer member · CPC title
the surfaces of the inner and outer member, forming the working space, being surfaces of revolution · CPC title
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