# US 2022/0034318 A1 · Vane rotary compressor > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2022/0034318 A1 - Document ID: US20220034318A1 - Status: Published application - Kind: A1 - Application number: 17/502,098 - Filed: 2021-10-15 - Published: 2022-02-03 - Earliest claimed: 2018-11-16 - Assignees: LG Electronics Inc. - Applicants: LG Electronics Inc. - Inventors: Joonhong PARK; Kiyoul NOH; Seokhwan MOON - Web page: https://patentgrep.com/patent/US20220034318A1 ## CPC - F04C 18/344: with vanes reciprocating with respect to the inner member - F01C 21/0863: {the fluid being the working fluid} - F04C 29/00: Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00 - F04C 29/023: {Lubricant distribution through a hollow driving shaft (F04C29/025 takes precedence)} - F01C 21/0845: {comprising elastic means, e.g. springs} - F04C 23/008: {Hermetic pumps} - F04C 2210/26: Refrigerants with particular properties, e.g. HFC-134a - F04C 2230/602: Gap; Clearance - F04C 2240/50: Bearings - F04C: ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS (engines F03C); ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS - F01C: ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES (internal-combustion aspects F02B53/00, F02B55/00) ## Abstract A vane rotary compressor includes a roller rotatably supported in a cylinder and including a plurality of vane slots formed along a circumferential direction with back pressure chambers formed at one end of each of the vane slots. A plurality of vanes are slidably supported in the vane slots protruding toward an inner circumferential surface of the cylinder. A compression space formed by the vanes between the roller and the cylinder includes an inlet port and an outlet port formed at both sides of a contact point between the roller and the cylinder. A vane positioned between the inlet port and the outlet port is configured such that a front gap between a front surface of the vane and the inner circumferential surface of the cylinder is smaller than a rear gap between a rear surface of the vane and an inner surface of the back pressure chamber. ## Claims ### Claim 1 A vane rotary compressor, comprising: a cylinder; a main bearing and a sub bearing coupled to the cylinder to form a compression space together with the cylinder, wherein at least one of the main bearing and the sub bearing includes a back pressure pocket formed on a surface facing the cylinder; a rotation shaft radially supported by the main bearing and the sub bearing; a roller coupled to the rotation shaft and rotatably supported within the cylinder between the main bearing and the sub bearing, the roller being configured such that an outer circumferential surface of one side of the roller is positioned in close proximity with an inner circumferential surface of the cylinder at a contact point, the roller including a plurality of vane slots formed along a circumferential direction of the roller, with each of the vane slots including one end opened toward the outer circumferential surface of the roller, and a back pressure chamber formed at the opposite end of the vane slot and in fluid communication with the back pressure pocket during at least a portion of a full rotation of the roller; a plurality of vanes slidably supported in the vane slots of the roller, and protruding in a direction toward the inner circumferential surface of the cylinder with the plurality of vanes dividing the compression space into a plurality of compression chambers, wherein the compression space is provided with an inlet port and an outlet port formed at both sides of the contact point; and an elastic member supported within the back pressure chamber of each of the vane slots and configured to support a rear surface of the respective vane slidably supported in the vane slot when the vane moves into the back pressure chamber of the vane slot, wherein the elastic member is a leaf spring, and a fixing groove is formed in a slit shape on an inner circumferential surface of the back pressure chamber of each of the vane slots, and wherein a circumferential end of the elastic member is inserted into the fixing groove of the back pressure chamber. ### Claim 2 (depends on 1) The compressor of claim 1, wherein the fixing groove is formed at each of both circumferential sides of the back pressure chamber facing each other, and wherein both ends of the elastic member in the circumferential direction are inserted into the fixing groove, respectively. ### Claim 3 (depends on 2) The compressor of claim 2, wherein the fixing groove is inclined in opposite directions toward the rear surface of the vane, and wherein a central portion of the elastic member protrudes toward the rear surface of the vane. ### Claim 4 (depends on 1) The compressor of claim 1, wherein the elastic member is provided with a through hole or a through groove so that front and rear spaces of the elastic member communicate with each other. ### Claim 5 (depends on 1) The compressor of claim 1, wherein an axial length of the elastic member is shorter than an axial length of the back pressure chamber so that front and rear spaces of the elastic member communicate with each other. ### Claim 6 (depends on 1) The compressor of claim 1, wherein the back pressure chamber has a maximum width greater than or equal to a width of the vane slot. ### Claim 7 (depends on 6) The compressor of claim 6, wherein the inner surface of the back pressure chamber has a curved shape and the rear surface of the vane has a right-angled corner. ### Claim 8 (depends on 6) The compressor of claim 6, wherein the inner surface of the back pressure chamber has a curved shape and the vane has a rear corner chamfered to have a tapered shape. ### Claim 9 (depends on 1) The compressor of claim 1, wherein a vane of the plurality of vanes located between the inlet port and the outlet port during a rotation of the roller is configured such that a front gap between a front surface of the vane and an inner circumferential surface of the cylinder is smaller than a rear gap between a rear surface of the vane and an inner surface of the back pressure chamber facing the rear surface of the vane, and greater than a lateral gap between the inner surface of the back pressure chamber and a side surface of the vane, in a state where the rear surface of the vane facing the back pressure chamber is in contact with the inner surface of the back pressure chamber. ### Claim 10 (depends on 9) The compressor of claim 9, wherein the front gap is greater than or equal to a predetermined minimum assembly gap, and wherein the back pressure chamber has a maximum width greater than or equal to a width of the vane slot. ### Claim 11 (depends on 1) The compressor of claim 1, wherein at least one of the main bearing and the sub bearing includes a back pressure pocket in fluid communication with the back pressure chambers of the plurality of vane slots during at least a portion of a full rotation of the rotor, wherein the back pressure pocket is divided into a plurality of pockets along a circumferential direction of the at least one of the main bearing and the sub bearing, and wherein the plurality of pockets have different inner pressures, and wherein each of the plurality of pockets includes a bearing protrusion portion formed on an inner circumferential side of the pocket and forming a radial bearing surface with respect to the outer circumferential surface of the rotation shaft. ### Claim 12 (depends on 11) The compressor of claim 11, wherein the plurality of pockets comprises: a first pocket having a first pressure; and a second pocket having a second pressure higher than the first pressure, and wherein the bearing protrusion portion of the second pocket includes a communication flow path extending through the bearing protrusion portion and in fluid communication with an inner circumferential surface of the bearing protrusion portion facing the outer circumferential surface of the rotation shaft. ### Claim 13 (depends on 12) The compressor of claim 12, wherein at least a part of the communication flow path overlaps an oil groove formed on a radial bearing surface of one of the main bearing or the sub bearing, and wherein the communication flow path is formed as a communication groove or a communication hole. ### Claim 14 (depends on 13) The compressor of claim 13, wherein the rotation shaft includes an oil flow path formed in a central portion thereof along an axial direction, wherein the oil flow path includes an oil passage hole extending through the rotation shaft from the oil flow path to the outer circumferential surface of the rotation shaft, and wherein the oil passage hole is formed within a range of the radial bearing surface. ### Claim 15 A vane rotary compressor, comprising: a cylinder; a main bearing and a sub bearing coupled to the cylinder to form a compression space together with the cylinder, wherein each of the main bearing and the sub bearing includes a divided back pressure pocket formed on a surface facing the cylinder, the divided back pressure pocket including a first pocket having a first inner pressure and a second pocket having a second inner pressure higher than the first inner pressure; a rotation shaft radially supported by the main bearing and the sub bearing; a roller rotatably supported within the cylinder between the main bearing and the sub bearing, the roller being configured such that an outer circumferential surface of one side of the roller is positioned in close proximity with an inner circumferential surface of the cylinder at a contact point, the roller including a plurality of vane slots formed along a circumferential direction of the roller, with each of the vane slots including one end opened toward the outer circumferential surface of the roller, and a back pressure chamber formed at the opposite end of the vane slot and in fluid communication with the divided back pressure pocket; and a plurality of vanes slidably supported in the vane slots of the roller, and protruding in a direction toward the inner circumferential surface of the cylinder with the plurality of vanes dividing the compression space into a plurality of compression chambers, wherein the compression space is provided with an inlet port and an outlet port formed at both sides of the contact point, and wherein each of the vane slots includes a stepped portion adjacent to the back pressure chamber, wherein the stepped portion forms a vane stop surface configured to restrict the vane from moving backwards into the back pressure chamber in contact with the rear surface of the vane when a compression chamber formed ahead of the vane slidably supported in the vane slot in a direction of rotation of the roller is at its highest pressure prior to discharge of fluid from the compression chamber through the outlet port. ### Claim 16 (depends on 15) The compressor of claim 15, wherein a width of the back pressure chamber is less than a width of the vane slot so that the stepped portion defining a vane stop surface is formed between a front end of the back pressure chamber and a rear end of the vane slot. ### Claim 17 (depends on 16) The compressor of claim 16, wherein during rotation of the roller each of the vanes located at a position between the inlet port and the outlet port is configured such that a front gap between a front surface of the vane and an inner circumferential surface of the cylinder is smaller than a rear gap between a rear surface of the vane and an inner surface of the back pressure chamber facing the rear surface of the vane, and the front gap is larger than a lateral gap between a side of the inner surface of the back pressure chamber and a side surface of the vane. ### Claim 18 (depends on 15) The compressor of claim 15, wherein each of the first and second pockets includes a bearing protrusion portion formed on an inner circumferential side of the pocket and forming a radial bearing surface with respect to the outer circumferential surface of the rotation shaft. ### Claim 19 (depends on 18) The compressor of claim 18, wherein the bearing protrusion portion of the second pocket includes a communication flow path extending through the bearing protrusion portion and in fluid communication with an inner circumferential surface of the bearing protrusion portion facing the outer circumferential surface of the rotation shaft, and wherein at least a part of the communication flow path overlaps an oil groove formed on a radial bearing surface of one of the main bearing or the sub bearing. ### Claim 20 (depends on 19) The compressor of claim 19, wherein the rotation shaft includes an oil flow path formed in a central portion thereof along an axial direction, wherein the oil flow path includes an oil passage hole extending through the rotation shaft from the oil flow path to the outer circumferential surface of the rotation shaft, and wherein the oil passage hole is formed within a range of the radial bearing surface.