Oil separator
US-9656198-B2 · May 23, 2017 · US
US2016290693A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016290693-A1 |
| Application number | US-201415038234-A |
| Country | US |
| Kind code | A1 |
| Filing date | Nov 19, 2014 |
| Priority date | Nov 25, 2013 |
| Publication date | Oct 6, 2016 |
| Grant date | — |
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The present application provides a compressor for use with a flow of carbon dioxide. The compressor may include a first stage compression mechanism for compressing the flow of carbon dioxide from a low pressure to an intermediate pressure, an oil separator downstream of the first stage compression mechanism, and a second stage compression mechanism positioned downstream of the oil separator for compressing the flow of carbon dioxide from the intermediate pressure to a high pressure.
Opening claim text (preview).
1 . A compressor for use with a flow of carbon dioxide, comprising: a first stage compression mechanism for compressing the flow of carbon dioxide from a low pressure to an intermediate pressure; an oil separator downstream of the first stage compression mechanism; and a second stage compression mechanism downstream of the oil separator for compressing the flow of carbon dioxide from the intermediate pressure to a high pressure. 2 . The compressor of claim 1 , wherein the first stage compression mechanism comprises a first stage input in communication with the flow of carbon dioxide at low pressure. 3 . The compressor of claim 1 , further comprising a shell casing and wherein the first stage compression mechanism and the second stage compression mechanism are positioned within the shell casing. 4 . The compressor of claim 3 , further comprising a motor positioned within the shell casing and in communication with the first stage compression mechanism and the second stage compression mechanism. 5 . The compressor of claim 3 , wherein the first stage compression mechanism comprises a first stage output in communication within the shell casing for the flow of carbon dioxide at intermediate pressure. 6 . The compressor of claim 3 , wherein the shell casing comprises a second stage pathway in communication with the second stage compression mechanism. 7 . The compressor of claim 1 , wherein the second stage compression mechanism comprises a second stage input in communication with the flow of carbon dioxide at intermediate pressure. 8 . The compressor of claim 1 , wherein the second stage compression mechanism comprises a second stage output in communication with the flow of carbon dioxide at high pressure. 9 . The compressor of claim 1 , wherein the oil separator comprises an expansion chamber. 10 . The compressor of claim 9 , wherein the oil separator comprises a J-tube within the expansion chamber. 11 . The compressor of claim 9 , wherein the oil separator comprises an oil pan and a wire mesh within the expansion chamber. 12 . The compressor of claim 1 , further comprising a check valve upstream of the oil separator. 13 . The compressor of claim 1 , wherein the oil separator comprises an oil drain in communication with a shell casing. 14 . The compressor of claim 13 , wherein the oil separator comprises a check valve on the oil drain. 15 . A method of compressing a flow of carbon dioxide for use in a refrigeration system, comprising: compressing the flow of carbon dioxide from a low pressure to an intermediate pressure in a first stage compressor; passing the flow of carbon dioxide at the intermediate pressure through an oil separator; and compressing the flow of carbon dioxide from the intermediate pressure to a high pressure in a second stage compressor. 16 . A compressor for use with a flow of a refrigerant, comprising: a shell casing; a first stage compression mechanism for compressing the flow of the refrigerant from a low pressure to an intermediate pressure positioned within the shell casing; an oil separator downstream of the first stage compression mechanism and positioned outside the shell casing; a second stage compression mechanism downstream of the oil separator for compressing the flow of the refrigerant from the intermediate pressure to a high pressure positioned within the shell casing; and a motor to drive the first stage compression mechanism and the second stage compression mechanism positioned within the shell casing. 17 . The compressor of claim 16 , wherein the oil separator comprises an expansion chamber. 18 . The compressor of claim 17 , wherein the oil separator comprises a J-tube positioned within the expansion chamber. 19 . The compressor of claim 16 , wherein the oil separator comprises an oil drain in communication with the shell casing. 20 . The compressor of claim 16 , wherein the refrigerant comprises a flow of carbon dioxide.
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