System and method for liquefying natural gas
US-2015338161-A1 · Nov 26, 2015 · US
US9927170B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9927170-B2 |
| Application number | US-201213433802-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 29, 2012 |
| Priority date | Mar 29, 2011 |
| Publication date | Mar 27, 2018 |
| Grant date | Mar 27, 2018 |
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The invention relates to a heat exchanger system ( 1 ) for heat exchange between at least a first medium (M), in particular in the form of a hydrocarbon-rich phase, and a second medium (K), with at least first and second pipe space sections ( 101, 103; 103, 105 ) for accommodating the first medium (M), and with a first pipe space section connecting means ( 102; 104 ), via which the two pipe space sections ( 101, 103; 103, 105 ) are connected to one another in a flow-guiding manner. The first pipe space section ( 101; 103 ) is surrounded by a first shell space ( 201, 203 ), and the second pipe space section ( 103; 105 ) is surrounded by a second shell space ( 203, 205 ) for accommodating the second medium (K). The first shell space ( 201; 203 ) is defined by a first shell ( 301; 303 ) and the second shell space ( 203; 205 ) is defined by a second shell ( 303; 305 ).
Opening claim text (preview).
The invention claimed is: 1. A heat exchanger system ( 1 ) for heat exchange between at least a first medium (M), and a second medium (K), said system comprising: at least two first pipe space sections ( 101 , 103 ; 103 , 105 ) for accommodating the first medium (M), and a first pipe space section connecting means ( 102 ; 104 ), via which the two first pipe space sections ( 101 , 103 ; 103 , 105 ) are connected to one another in a flow-guiding manner, wherein said first pipe space section connecting means is in the form of at least one pipeline; wherein one of said two first pipe space sections ( 101 ; 103 ) is surrounded by a first shell space ( 201 , 203 ) for accommodating the second medium (K), and the other of said two first pipe space section ( 103 ; 105 ) is surrounded by a second shell space ( 203 , 205 ) for accommodating the second medium (K), wherein each of said first shell space ( 201 , 203 ) and said second shell space ( 203 , 205 ) has a longitudinal axis, wherein said one of said two first pipe space sections is in the form of a wound pipe bundle in which individual pipes are wound around a central pipe extending along the longitudinal axis of said first shell space, and said other of said first two pipe space sections is in the form of a wound pipe bundle in which individual pipes are wound around a central pipe extending along the longitudinal axis of said second shell space, wherein said first shell space ( 201 ; 203 ) is defined by a first shell ( 301 ; 303 ) and said second shell space ( 203 ; 205 ) is defined by a second shell ( 303 ; 305 ), and said first shell space and said second shell space are separate from one another, wherein said second shell ( 303 ; 305 ) is arranged in the vertical direction (Z) a distance above said first shell ( 301 ; 303 ), and said first and second shell spaces ( 201 , 203 ; 203 , 205 ) are connected to one another in a flow-guiding manner by a first shell space connecting means ( 202 ; 204 ), wherein said second shell ( 303 ) has a means for separating the second medium (K) flowing through said second shell space ( 203 ) into a liquid fraction of the second medium (K) and a gaseous fraction of the second medium (K), and said means for separating is (a) an expanded region in a lower section of said second shell space ( 203 ), or (b) a separator arranged below said wound pipe bundle in said second shell space, wherein said first shell space connecting means ( 202 ; 204 ) is in the form of pipelines, said first shell space connecting means provides for transport of the gaseous fraction of second medium (K) and transport of the liquid fraction of second medium (K) from a lower section of said second shell space ( 203 , 205 ) to an upper section of said first shell space ( 201 , 203 ), wherein the gaseous fraction of second medium (K) is transported separately from the liquid fraction of second medium (K) via said first shell space connecting means. 2. The heat exchanger system according to claim 1 , wherein said first shell ( 301 ) provides heat exchange for pre-cooling of the first medium (M) in said one of said two first pipe space section ( 101 ) within said first shell ( 301 ), and wherein said second shell ( 303 ) provides heat exchange for liquefying the first medium (M) in said other of said two first pipe space section ( 103 ) within said second shell ( 303 ). 3. The heat exchanger system according to claim 1 , wherein said first shell ( 303 ) provides heat exchange for liquefying the first medium (M) that is guided in said one of said two first pipe space section within said first shell ( 303 ), and said second shell ( 305 ) provides heat exchange for subcooling first medium (M) that is guided in said other of said two first pipe space section ( 105 ) within said second shell ( 305 ), said first shell ( 303 ) further comprises a second pipe space section ( 123 ), which is surrounded by said first shell space ( 203 ), wherein a gaseous fraction of second medium (K) can be introduced into said second pipe space section ( 123 ) of said first shell ( 303 ) via a first inlet ( 122 b ) of said first shell ( 303 ), and said second pipe space section ( 123 ) within said first shell ( 303 ) runs along said first pipe space section ( 103 ) within said first shell ( 303 ), said first shell ( 303 ) further comprises a third pipe space section ( 124 ), which is surrounded by said first shell space ( 203 ), wherein a liquid fraction of second medium (K) can be introduced into said third pipe space section ( 124 ) via a second inlet ( 122 c ) of said first shell ( 303 ), and said third pipe space section ( 124 ) within said first shell ( 303 ) runs along said first pipe space section ( 103 ) within said first shell ( 303 ), said third pipe space section ( 124 ) of said first shell ( 303 ) is connected at the upper end of said first shell ( 303 ) to introduce the liquid fraction of second medium (K) into said first shell space ( 203 ), said second pipe space section ( 123 ) within said first shell ( 303 ) is connected in a flow-guiding manner via a second pipe space section connecting means ( 126 ), in the form of at least one pipeline, to a second pipe space section ( 127 ) within said second shell space ( 205 ) surrounded by said second shell ( 305 ), said second pipe space section ( 127 ) within said second shell ( 305 ) runs along said first pipe space section ( 105 ) within said second shell ( 305 ), and said second pipe space section ( 127 ) within said second shell ( 305 ) is connected at the upper end of said second shell ( 305 ) to introduce a gaseous fraction of second medium (K) into said second shell space ( 205 ), and said first shell ( 303 ) has an expanded region ( 320 ). 4. The heat exchanger system according to claim 1 , wherein said second shell ( 303 ) has an expanded region in a lower section thereof. 5. The heat exchanger system according to claim 1 , further comprising a separate third shell ( 305 ), said third shell ( 305 ) having therein a further first pipe space section ( 105 ) for accommodating flow of the first medium (M), said further first pipe space section ( 105 ) of said third shell ( 305 ) being connected in a flow-guiding manner to said first pipe space section ( 103 ) of said second shell ( 303 ) via a second pipe space section connecting means ( 104 ) in the form of at least one pipeline, said one of said two first pipe space section ( 105 ) within said third shell ( 305 ) is surrounded by a related third shell space ( 205 ) for accommodating second medium (K), wherein said third shell ( 305 ) provides heat exchange for subcooling the first medium (M), and said third shell ( 305 ) is arranged at some distance from said first shell and/or second shell ( 301 , 303 ), whereby said third shell ( 305 ) is arranged along the vertical (Z) above said second shell ( 303 ), and said second and third shell spaces ( 203 , 205 ) are connected to one another in a flow-guiding manner by a second shell space connecting means ( 204 ), in particular in the form of at least one pipeline, and said third shell ( 305 ) has a first outlet (A) for removing the first medium (M) from the heat exchanger system ( 1 ) in the form of a liquid phase. 6. The heat exchanger system according to claim 1 , wherein said first shell ( 301 ) has a first inlet (E) for admitting the first medium (M), in the form of a gaseous phase, into said first pipe space section ( 101 ) within said first shell ( 301 ). 7. The heat exchanger system according to claim 1 , wherein said first shell ( 301 ) further comprises therein a second pipe space section for accommodating second medium (K) in the form of a liquid fraction, said second pipe space section within said first shell ( 301 ) runs along said first p
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