A system and method is provided for increasing the capacity and efficiency of natural gas liquefaction processes by debottlenecking the refrigerant compression system. A secondary compression circuit comprising at least one double flow compressor is provided in parallel fluid flow communication with at least a portion of a primary compression circuit.

A liquefied natural gas production plant comprising a carbon capture unit wherein the refrigerant fluid thermodynamic refrigeration cycle of the carbon capture system and the refrigerant fluid thermodynamic refrigeration cycle of the liquefied natural gas production plant are integrated by using the same refrigerant fluid and sharing at least some apparatuses, thus reducing the overall number of apparatuses and in particular the overall number of compressors and consequently reducing the emissions of carbon dioxide produced by the compressors.

Methods for increasing ethane and non-freezing heavier hydrocarbons recovery in natural gas streams for the liquefaction of natural gas to form liquefied natural gas (LNG), and in particular, utilizing scrub columns to treat the natural gas feedstreams, are provided. Other independent variations of the methods are disclosed herein.

A liquefied natural gas production plant for producing a product stream of liquefied natural gas installed at a production location and a process for producing liquefied natural gas includes a plurality of modules and an air-cooled heat exchanger bank designed for the installed production train. The heat exchanger bank includes a first row of air-cooled heat exchanger bays, and an adjacent parallel second row of air-cooled heat exchanger bays.

A process is described herein for the production of a selected quantity of ethane as a component of a production inventory of mixed refrigerant for an LNG production plant prior to start-up of the LNG production plant.

An LNG production plant and a method of constructing the LNG production plant is disclosed. The LNG production plant includes at least one plant module and a support structure to support the plant module. Each plant module is dry transported by a heavy lift vessel and subsequently transferred to the support structure without lifting the plant module from a deck of the vessel. The support structure includes a landing substructure onto which the plant module is transferred from the vessel. Landing substructure may be onshore or offshore. The support structure may also include one or more onshore support substructures and a transfer path enabling a plant module to be moved from the landing substructure to a corresponding onshore support substructure.

The LNG plant comprises a compression train and a further compression. The compression train (100) comprises comprising an engine and a compressor driven by the engine; the compressor is an axial compressor and comprises a first set of axial compression stages and a second set of axial compression stages arranged downstream the first set of axial compression stages; at least the first set and the second set of axial compression stages are housed inside one case. The further compression train comprises a further engine and a further compressor driven by the further engine; the further compressor is a centrifugal compressor and comprises a first set of impellers and a second set of impellers arranged downstream or upstream the first set of impellers.

Compression train for a natural gas liquefaction process. The compression train includes a driver machine and only one centrifugal compressor machine driven in rotation by the driver machine; the compressor is configured to compress a refrigerant gas with a molecular weight less than 30 g/mol from a suction pressure to a discharge pressure; the ratio between discharge and suction pressures is higher than 10. A LNG plant including a compression train.

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.

The present invention relates to a method of cooling and separating a hydrocarbon stream: (a) passing an hydrocarbon feed stream (7) through a first cooling and separation stage to provide a methane enriched vapour overhead stream (110) and a methane depleted liquid stream (10); (b) passing the methane depleted liquid stream (10) to a fractionation column (200) to obtain a bottom condensate stream (210), a top stream enriched in C1-C2 (220) and a midstream enriched in C3-C4 (230), (c) cooling the upper part of the fractionation column (201) by a condenser (206), (d) obtaining a split stream (112) from the methane enriched vapour overhead stream (110) and obtaining a cooled split stream (112) by expansion-cooling the split stream (112), (e) providing cooling duty to the top of the fractionation column (201) using the cooled split stream (112).