Device for compressing a gaseous fluid and method for operating the device
AssigneeHanon Systems
InventorsAyhan Ayar, Gerd Vondahlen, Alex Rybski
Life of this patent
Estimating the term…
Abstract
A device for compressing a gaseous fluid, in particular a refrigerant in a refrigerant circuit, specifically of an air-conditioning system of a motor vehicle. The device has a housing, a compression mechanism for compressing the gaseous fluid, and an electric motor for driving the compression mechanism. The housing is formed with a suction-pressure chamber and a high-pressure chamber.
Claims12
A device for compressing a gaseous fluid comprising:
- a housing;
- a compression mechanism for compressing the gaseous fluid;
- and
- an electric motor for driving the compression mechanism, the housing formed with a suction-pressure chamber and a high-pressure chamber, wherein the suction-pressure chamber is disposed upstream of the compression mechanism and includes the gaseous fluid prior to compression within the compression mechanism, and wherein the high-pressure chamber is disposed downstream of the compression mechanism and receives the gaseous fluid following compression thereof within the compression mechanism, wherein a bypass flow path and a device for controlling a through-flow of the gaseous fluid through the bypass flow path are formed, wherein the bypass flow path directly fluidly couples the suction-pressure chamber to the high-pressure chamber, and wherein the device for controlling the through-flow is designed to open the bypass flow path solely for the gaseous fluid to flow therethrough in a flow direction from the suction-pressure chamber into the high-pressure chamber in reaction to a pressure of the gaseous fluid within the suction-pressure chamber being greater than a pressure of the gaseous fluid within the high-pressure chamber, wherein the compression mechanism has a stationary spiral and an orbiting spiral, wherein the stationary spiral and the orbiting spiral are each formed with a baseplate and a spiral-shaped wall extending from the baseplate, wherein the spiral shaped wall of the stationary spiral and the spiral shaped wall of the orbiting spiral are arranged to engage in one another and to form working chambers, and wherein the bypass flow path is formed inside the stationary spiral or inside a wall of the housing, or outside the housing, wherein the device for controlling the through-flow is a lamellar valve.
A device for compressing a gaseous fluid comprising:
- a housing:
- a compression mechanism for compressing the gaseous fluid;
- and
- an electric motor for driving the compression mechanism, the housing formed with a suction-pressure chamber and a high-pressure chamber, wherein the suction-pressure chamber is disposed upstream of the compression mechanism and includes the gaseous fluid prior to compression within the compression mechanism, and wherein the high-pressure chamber is disposed downstream of the compression mechanism and receives the gaseous fluid following compression thereof within the compression mechanism, wherein a bypass flow path and a device for controlling a through-flow of the gaseous fluid through the bypass flow path are formed, wherein the bypass flow path directly fluidly couples the suction-pressure chamber to the high-pressure chamber, and wherein the device for controlling the through-flow is designed to open the bypass flow path solely for the gaseous fluid to flow therethrough in a flow direction from the suction-pressure chamber into the high-pressure chamber in reaction to a pressure of the gaseous fluid within the suction-pressure chamber being greater than a pressure of the gaseous fluid within the high-pressure chamber, wherein the compression mechanism has a stationary spiral and an orbiting spiral, wherein the stationary spiral and the orbiting spiral are each formed with a baseplate and a spiral-shaped wall extending from the baseplate, wherein the spiral shaped wall of the stationary spiral and the spiral shaped wall of the orbiting spiral are arranged to engage in one another and to form working chambers, wherein the device for controlling the through-flow is a lamellar valve, and wherein the device for controlling the through-flow is arranged to bear against a surface, facing the high-pressure chamber, of the baseplate of the stationary spiral and to close the bypass flow path when in the closed state.
A device for compressing a gaseous fluid comprising:
- a housing;
- a compression mechanism for compressing the gaseous fluid;
- and
- an electric motor for driving the compression mechanism, the housing formed with a suction-pressure chamber and a high-pressure chamber, wherein the suction-pressure chamber is disposed upstream of the compression mechanism and includes the gaseous fluid prior to compression within the compression mechanism, and wherein the high-pressure chamber is disposed downstream of the compression mechanism and receives the gaseous fluid following compression thereof within the compression mechanism, wherein a bypass flow path and a device for controlling a through-flow of the gaseous fluid through the bypass flow path are formed, wherein the bypass flow path directly fluidly couples the suction-pressure chamber to the high-pressure chamber, and wherein the device for controlling the through-flow is designed to open the bypass flow path solely for the gaseous fluid to flow therethrough in a flow direction from the suction-pressure chamber into the high-pressure chamber in reaction to a pressure of the gaseous fluid within the suction-pressure chamber being greater than a pressure of the gaseous fluid within the high-pressure chamber, wherein the device for controlling the through-flow is a lamellar valve, wherein the compression mechanism has a stationary spiral and an orbiting spiral, wherein the stationary spiral and the orbiting spiral are each formed with a baseplate and a spiral-shaped wall extending from the baseplate, wherein the spiral shaped wall of the stationary spiral and the spiral shaped wall of the orbiting spiral are arranged to engage in one another and to form working chambers, wherein the device for controlling the through-flow has a fastening region and a closing region, which are connected to one another via a neck-like connecting region, and wherein the device for controlling the through-flow in the form of the lamellar valve and at least one outlet valve in the form of a lamellar valve are connected to one another at first ends, forming the fastening region, to form an integral unit, wherein the device for controlling the through-flow and the at least one outlet valve are arranged oriented in a common plane.
A device for compressing a gaseous fluid comprising:
- a housing;
- a compression mechanism for compressing the gaseous fluid;
- and
- an electric motor for driving the compression mechanism, the housing formed with a suction-pressure chamber and a high-pressure chamber, wherein the suction-pressure chamber is disposed upstream of the compression mechanism and includes the gaseous fluid prior to compression within the compression mechanism, and wherein the high-pressure chamber is disposed downstream of the compression mechanism and receives the gaseous fluid following compression thereof within the compression mechanism, wherein a bypass flow path and a device for controlling a through-flow of the gaseous fluid through the bypass flow path are formed, wherein the bypass flow path directly fluidly couples the suction-pressure chamber to the high-pressure chamber, and wherein the device for controlling the through-flow is designed to open the bypass flow path solely for the gaseous fluid to flow therethrough in a flow direction from the suction-pressure chamber into the high-pressure chamber in reaction to a pressure of the gaseous fluid within the suction-pressure chamber being greater than a pressure of the gaseous fluid within the high-pressure chamber, wherein the compression mechanism has a stationary spiral and an orbiting spiral, wherein the stationary spiral and the orbiting spiral are each formed with a baseplate and a spiral-shaped wall extending from the baseplate, wherein the spiral shaped wall of the stationary spiral and the spiral shaped wall of the orbiting spiral are arranged to engage in one another and to form working chambers, wherein the device for controlling the through-flow has a fastening region and a closing region, which are connected to one another via a neck-like connecting region, and wherein the device for controlling the through-flow is fixed at a first end with the fastening region to the baseplate of the stationary spiral and is arranged so as to be able to close the bypass flow path with a free second end, formed distally from the first end, with the closing region.
A device for compressing a gaseous fluid comprising:
- a housing;
- a compression mechanism for compressing the gaseous fluid;
- and
- an electric motor for driving the compression mechanism, the housing formed with a suction-pressure chamber and a high-pressure chamber, wherein the suction-pressure chamber is disposed upstream of the compression mechanism and includes the gaseous fluid prior to compression within the compression mechanism, and wherein the high-pressure chamber is disposed downstream of the compression mechanism and receives the gaseous fluid following compression thereof within the compression mechanism, wherein a bypass flow path and a device for controlling a through-flow of the gaseous fluid through the bypass flow path are formed, wherein the bypass flow path directly fluidly couples the suction-pressure chamber to the high-pressure chamber, and wherein the device for controlling the through-flow is designed to open the bypass flow path solely for the gaseous fluid to flow therethrough in a flow direction from the suction-pressure chamber into the high-pressure chamber in reaction to a pressure of the gaseous fluid within the suction-pressure chamber being greater than a pressure of the gaseous fluid within the high-pressure chamber, wherein the compression mechanism has a stationary spiral and an orbiting spiral, wherein the stationary spiral and the orbiting spiral are each formed with a baseplate and a spiral-shaped wall extending from the baseplate, wherein the spiral shaped wall of the stationary spiral and the spiral shaped wall of the orbiting spiral are arranged to engage in one another and to form working chambers, wherein the device for controlling the through-flow has a fastening region and a closing region, which are connected to one another via a neck-like connecting region, wherein the connecting region is formed over a length with a constant width which is smaller than a diameter of the substantially circular closing region, and wherein the connecting region has a constant outer radius such that the connecting region is a section of a circular ring.
Dependencies are inferred from the claim text.