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公开(公告)号:US12061044B2
公开(公告)日:2024-08-13
申请号:US17639570
申请日:2019-10-09
申请人: JGC CORPORATION
发明人: Akito Hirai , Nobuhiro Kimura , Hideto Hagiya , Shinichi Tojo , Junichi Nishida , Tomoaki Matsuo , Ayaka Uemura
CPC分类号: F25J1/0022 , F25J1/0052 , F25J1/0259 , F25J1/0283 , F25J1/0292 , F25J1/0294 , F25J1/0296 , F25J2210/60
摘要: A natural gas liquefying apparatus is provided. At least a part of a cooling region, in which a precooling unit and a liquefaction unit are arranged, and at least a part of a compression region, in which first and second compressors compressing refrigerants to be used in the precooling unit and the liquefaction unit are arranged, are arranged to be opposed to each other across a long side of a second refrigerant cooler group arrangement region in which a liquefying refrigerant is cooled. A first refrigerant cooler group arrangement region, in which a precooling refrigerant is cooled, is arranged so that a long side of the first refrigerant cooler group arrangement region is opposed to one side of a rectangular region including the compression region, the one side being different from a side of the rectangular region opposed to a long side of the second refrigerant cooler group arrangement region.
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公开(公告)号:US20240255216A1
公开(公告)日:2024-08-01
申请号:US18565968
申请日:2022-05-27
申请人: ENGIE
发明人: Florian JALIA , Rémi LINOTTE , Hamza FILALI , Davide DURI , Loïc PENIN , Pierre CHABERNAUD
CPC分类号: F25J1/001 , F25J1/005 , F25J1/0055 , F25J1/0062 , F25J1/0065 , F25J1/0067 , F25J1/0072 , F25J1/0077 , F25J1/0205 , F25J1/0265 , F25J1/0292 , F25J1/0218 , F25J1/0291 , F25J2230/04 , F25J2240/60 , F25J2270/16
摘要: Method for hydrogen liquefaction comprising at least one precooling step, wherein a hydrogen feed flow is cooled by a first refrigerant, a cooling step, wherein the hydrogen feed flow is cooled by a second refrigerant, and a step of expanding the hydrogen feed flow. Each of the first and second refrigerants is successively subjected to at least one compression and to at least one expansion in order to cool it, and a liquid phase of the first refrigerant cools the second refrigerant between at least three stages of said compression so that the second refrigerant does not exceed a temperature of 150 K, optionally 113 K, during said compression of the second refrigerant.
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3.
公开(公告)号:US20240230221A1
公开(公告)日:2024-07-11
申请号:US18402076
申请日:2024-01-02
申请人: Brian R. Kromer , Seth A. Potratz , Sean M. Kelly
发明人: Brian R. Kromer , Seth A. Potratz , Sean M. Kelly
CPC分类号: F25J1/0215 , F25J1/0017 , F25J1/0022 , F25J1/0057 , F25J1/0062 , F25J1/0072 , F25J1/0229 , F25J1/0234 , F25J1/0292 , F25J2215/04 , F25J2215/50 , F25J2215/60 , F25J2230/42 , F25J2245/42 , F25J2260/50 , F25J2260/60 , F25J2270/60 , F25J2270/66
摘要: A system and method for the co-production of a densified, liquid oxidant and a densified liquid methane fuel to a space vehicle launch facility is provided. In one embodiment, a low pressure gaseous oxygen stream is piped from a nearby air separation unit to the space vehicle launch facility where it is then liquefied and densified in a two-stage, integrated liquefaction/densification system that also densifies a source of liquid methane. In an alternate embodiment, a liquid oxygen stream produced at an air separation unit is densified in a two-stage, integrated densification system configured to densify both the liquid oxygen as well a source of liquid methane at or near the air separation unit with the resulting densified liquid products transported via truck/trailer to a nearby space vehicle launch facility.
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公开(公告)号:US20190242645A1
公开(公告)日:2019-08-08
申请号:US16390687
申请日:2019-04-22
发明人: John MAK , Jacob THOMAS , Curt Graham
CPC分类号: F25J1/0228 , F25J1/0022 , F25J1/0035 , F25J1/004 , F25J1/0052 , F25J1/0055 , F25J1/0212 , F25J1/0216 , F25J1/0239 , F25J1/0291 , F25J1/0292 , F25J3/0209 , F25J3/0233 , F25J3/0238 , F25J3/0242 , F25J2200/02 , F25J2200/04 , F25J2200/08 , F25J2200/70 , F25J2200/76 , F25J2200/78 , F25J2205/50 , F25J2210/06 , F25J2215/04 , F25J2215/60 , F25J2215/62 , F25J2215/64 , F25J2230/30 , F25J2230/60 , F25J2235/60 , F25J2240/02 , F25J2260/20 , F25J2270/12 , F25J2270/18 , F25J2270/60 , F25J2270/66
摘要: A LNG liquefaction plant includes a propane recovery unit including an inlet for a feed gas, a first outlet for a LPG, and a second outlet for an ethane-rich feed gas, an ethane recovery unit including an inlet coupled to the second outlet for the ethane-rich feed gas, a first outlet for an ethane liquid, and a second outlet for a methane-rich feed gas, and a LNG liquefaction unit including an inlet coupled to the second outlet for the methane-rich feed gas, a refrigerant to cool the methane-rich feed gas, and an outlet for a LNG. The LNG plant may also include a stripper, an absorber, and a separator configured to separate the feed gas into a stripper liquid and an absorber vapor. The stripper liquid can be converted to an overhead stream used as a reflux stream to the absorber.
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公开(公告)号:US20180356149A1
公开(公告)日:2018-12-13
申请号:US15781490
申请日:2016-12-06
申请人: SHELL OIL COMPANY
CPC分类号: F25J1/0022 , F25J1/0052 , F25J1/0055 , F25J1/0212 , F25J1/0214 , F25J1/0216 , F25J1/0252 , F25J1/0284 , F25J1/0292
摘要: The present invention relates to a method of controlling the production of a liquefied natural gas product stream (31) obtained by removing heat from natural gas by indirect heat exchange with an expanded heavy mixed refrigerant and an expanded light mixed refrigerant. The method comprises executing a control loop comprising maintaining the flow rate of the liquefied natural gas product stream (31) at a dependent set point and maintaining the flow rates of the heavy mixed refrigerant (60a) and the light mixed refrigerant (65) at operator manipulated set points (80, 81). The method further comprises executing an override control loop comprising: determining an override set point (95′) for the flow rate of the liquefied natural gas and computing an override set point (80′) for the flow rate of the heavy mixed refrigerant and an override set point (81′) to reduce residual available power of the electric motor.
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公开(公告)号:US20180313603A1
公开(公告)日:2018-11-01
申请号:US15771731
申请日:2015-10-28
发明人: Daisuke NAGATA , Shinji TOMITA
CPC分类号: F25J1/0015 , F01K25/00 , F17C2221/033 , F17C2223/0161 , F17C2223/033 , F17C2225/0123 , F17C2225/035 , F17C2227/0316 , F17C2227/0323 , F17C2227/0393 , F17C2265/05 , F17C2270/0136 , F25J1/004 , F25J1/0045 , F25J1/0222 , F25J1/0224 , F25J1/0265 , F25J1/0281 , F25J1/0292 , F25J2210/62 , F25J2230/20 , F25J2230/30 , F25J2230/42
摘要: An apparatus for producing a liquefied gas using a Rankine cycle is provided. The apparatus includes a first compression means for adiabatically compressing a heat transfer medium; a first heat exchanger for constant pressure heating the adiabatically compressed heat transfer medium; a plurality of parallelly arranged expansion means for adiabatically expanding the heated heat transfer medium; a second heat exchanger for constant pressure cooling the adiabatically expanded heat transfer medium; and a flow passageway for guiding the heat transfer medium that has been guided out from the second heat exchanger to the first compression means.
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公开(公告)号:US20180209337A1
公开(公告)日:2018-07-26
申请号:US15881438
申请日:2018-01-26
发明人: Alessandro RUSSO , Alessandro DEL BONO , Luciano MEI , Maurizio CIOFINI , Abdus SHAMIM , Mehdi Milani BALADI , Alessio POSTACCHINI , Bernard W. DUMM , Jason HAYDEN , Gabriele CARTOCCI , Francesco CARATELLI
CPC分类号: F02C3/10 , F01D25/28 , F01D25/285 , F02C7/143 , F05D2240/54 , F05D2240/91 , F05D2260/207 , F25J1/0022 , F25J1/0052 , F25J1/0055 , F25J1/0082 , F25J1/0085 , F25J1/0087 , F25J1/0209 , F25J1/0214 , F25J1/0216 , F25J1/0217 , F25J1/0283 , F25J1/029 , F25J1/0292 , F25J1/0294 , Y02T50/671
摘要: The gas turbine system comprises an aeroderivative gas turbine engine and a load having a shaft line drivingly coupled to the gas turbine engine. The gas turbine engine comprises a high-pressure turbine section and a high-pressure compressor section, drivingly coupled to one another by a first turbine shaft. The gas turbine engine further comprises an intermediate-pressure turbine section and a low-pressure compressor section, drivingly coupled to one another by a second turbine shaft, coaxial to the first turbine shaft (91). Furthermore, a combustor section is provided, fluidly coupled to the high-pressure compressor section and to the high-pressure turbine section. A free power turbine, supported by a third turbine shaft which is mechanically uncoupled from the first turbine shaft and the second turbine shaft, and is directly coupled to the shaft line, such that the shaft line and the third turbine shaft rotate at the same rotational speed. The free power turbine is adapted to generate a mechanical power rating of at least 65 MW under ISO day conditions.
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公开(公告)号:US10012432B2
公开(公告)日:2018-07-03
申请号:US12668553
申请日:2008-07-10
CPC分类号: F25J1/0022 , F25B9/006 , F25J1/0042 , F25J1/0052 , F25J1/0055 , F25J1/0057 , F25J1/0214 , F25J1/0244 , F25J1/0283 , F25J1/0292 , F25J1/0295
摘要: A mixed refrigerant stream (10) comprising a first mixed refrigerant is passed through one or more heat exchangers (12) to provide a cooled mixed refrigerant stream (20). At least a fraction of a cooling stream (30) comprising a second mixed refrigerant is expanded (14) to provide one or more expanded cooling streams (40a), at least one of which may be passed through one or more of the heat exchangers (12), to cool the mixed refrigerant stream (10) thereby providing the cooled mixed refrigerant stream (20) which is used to cool (22) a hydrocarbon stream (70). The temperature (T1) and the flow (F1) of at least part of the cooled mixed refrigerant stream (20) is monitored, and the flow (F2) of the cooling stream (30) is controlled using the flow F1 and the temperature T1.
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公开(公告)号:US20180038643A1
公开(公告)日:2018-02-08
申请号:US15414100
申请日:2017-01-24
CPC分类号: F25J1/0231 , C01B3/34 , C01B3/384 , C01B3/56 , C01B2203/0205 , C01B2203/0233 , C01B2203/0244 , C01B2203/042 , C01B2203/0475 , C01B2203/0495 , C01B2203/061 , C01B2203/1241 , C01B2203/84 , F25J1/0022 , F25J1/0035 , F25J1/0037 , F25J1/005 , F25J1/0052 , F25J1/0072 , F25J1/0204 , F25J1/0229 , F25J1/023 , F25J1/0232 , F25J1/0282 , F25J1/0288 , F25J1/0292 , F25J1/0294 , F25J2210/06 , F25J2210/60 , F25J2230/20 , F25J2230/30 , F25J2230/60 , F25J2240/02 , F25J2240/04 , F25J2240/12 , F25J2240/70 , F25J2260/60 , F25J2270/04 , F25J2270/12 , F25J2270/16
摘要: An integrated method for the production of liquefied natural gas (LNG) and syngas is provided. The method can include the steps of: utilizing letdown energy of a high pressure natural gas stream that is withdrawn from a natural gas pipeline to provide a warm temperature cooling; utilizing a refrigeration cycle to provide a cold temperature cooling, wherein the refrigeration cycle comprises a refrigerant recycle compressor that is powered utilizing a steam turbine; and cooling a second high pressure natural gas stream using the warm temperature cooling and the cold temperature cooling to produce an LNG product stream. The second high pressure natural gas stream is withdrawn from the natural gas pipeline, and the steam turbine is powered by high pressure steam that is produced from a syngas production facility.
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10.
公开(公告)号:US20180017320A1
公开(公告)日:2018-01-18
申请号:US15538940
申请日:2015-12-24
申请人: SHELL OIL COMPANY
CPC分类号: F25J1/0022 , F25J1/0052 , F25J1/0055 , F25J1/0212 , F25J1/0216 , F25J1/0247 , F25J1/0249 , F25J1/0292
摘要: The present invention relates to a method and apparatus for cooling down a cryogenic heat exchanger adapted to liquefy a hydrocarbon stream, such as a natural gas stream. The method comprises: (i) receiving one or more refrigerant temperature indications, providing an indication of the temperature of the refrigerant, (ii) comparing the one or more refrigerant temperature indications with one or more associated predetermined threshold values, and (iii) based on the outcome of the comparison under (ii) selecting one of an automated warm cooling down procedure of the cryogenic heat exchanger and an automated cold cooling down procedure of the cryogenic heat exchanger.
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