Abstract: An integrated gas turbine cycle and liquid air energy conversion system is provided that utilizes very high pressure air stream(s) produced from vaporization of a supercritical liquid air against a low pressure cryogenic gas. The cooled, low pressure cryogenic gas is then cold compressed to yield a moderate pressure cryogenic gas stream(s). Both the very high pressure air stream(s) and the moderate pressure air stream(s) are warmed in the flue gas heat exchanger associated with the gas turbine cycle. A source of electrical power is produced from the expansion of combustion gas in a gas turbine while auxiliary sources of electrical power are produced from the turbine expansion of the warmed very high pressure air streams and moderate pressure cryogenic gas streams. The combustion gas includes a moderate pressure supplemental stream originating from the supercritical liquid air or from the cold compressed cryogenic gas.

Abstract: A liquid air energy conversion system is provided that integrates three subsystems or unit operations, namely a deep sub-ambient gas compression subsystem, a power expansion and heat recovery subsystem, and an external heat source.

Abstract: A liquid air energy conversion system is provided that is a variant of conventional gas turbine combined cycle (GTCC) that integrates three subsystems or unit operations, namely a main air compression and pre-purification subsystem, a deep sub-ambient gas compression subsystem, and a power expansion and waste heat recovery subsystem. The disclosed liquid air energy conversion system enhances and optimizes the energy extraction from liquid air by avoiding main air compression directly associated with the gas turbine and the air fed to the overall system and process is limited to the air flow required to vaporize the liquid air.

Abstract: An integrated gas turbine cycle and liquid air energy conversion system is provided that utilizes very high pressure air stream(s) produced from vaporization of a supercritical liquid air against a low pressure cryogenic gas. The cooled, low pressure cryogenic gas is then cold compressed to yield a moderate pressure cryogenic gas stream(s). Both the very high pressure air stream(s) and the moderate pressure air stream(s) are warmed in the flue gas heat exchanger associated with the gas turbine cycle. A source of electrical power is produced from the expansion of combustion gas in a gas turbine while auxiliary sources of electrical power are produced from the turbine expansion of the warmed very high pressure air streams and moderate pressure cryogenic gas streams. The combustion gas includes a moderate pressure supplemental stream originating from the supercritical liquid air or from the cold compressed cryogenic gas.

Abstract: A liquid air energy conversion system is provided that recovers energy not by direct expansion of the liquid air stream, but rather by vaporization of the liquid air to form a first stream of very high pressure gaseous air via indirect heat exchange against a low pressure, cryogenic gas and subsequent sub-ambient or cold compression of the cooled, low pressure cryogenic gas to form a stream of moderate pressure gas. Both the stream of very high pressure gaseous air and the stream of moderate pressure gas are then warmed and expanded in one or more turbine expanders for production of shaft work and/or electrical energy.

Abstract: A system and method of optimizing the production of argon in a cryogenic air separation unit using a temperature profile of a distillation column or distillation column section obtained via fiber optic temperature measurements on the exterior surface of the distillation column or the distillation column section is provided. The temperature profiles are used to determine the vertical location and/or spatial movement of the maximum argon concentration in the distillation column or the distillation column section. Distillation column operation is then adjusted such that the vertical location or spatial movement of the maximum argon concentration is aligned proximate with the location of an argon-rich draw from the distillation column.

Abstract: A system and method of ultra-high purity (UHP) oxygen production from an argon and oxygen producing cryogenic air separation unit incorporating a dedicated methane rejection column or column section having a liquid to vapor (L/V) ratio lower than the L/V ratio in the associated argon rectifier is provided.

Abstract: An integrated gas turbine cycle and liquid air energy conversion system is provided that utilizes very high pressure air stream(s) produced from vaporization of a supercritical liquid air against a low pressure cryogenic gas. The cooled, low pressure cryogenic gas is then cold compressed to yield a moderate pressure cryogenic gas stream(s). Both the very high pressure air stream(s) and the moderate pressure air stream(s) are warmed in the flue gas heat exchanger associated with the gas turbine cycle. A source of electrical power is produced from the expansion of combustion gas in a gas turbine while auxiliary sources of electrical power are produced from the turbine expansion of the warmed very high pressure air streams and moderate pressure cryogenic gas streams. The combustion gas includes a moderate pressure supplemental stream originating from the supercritical liquid air or from the cold compressed cryogenic gas.

Abstract: A system and method for the liquefaction and densification of oxygen for use in space vehicle applications is provided that uses high pressure air or synthetic air as the refrigerant source. The disclosed system and method employs a heat exchanger arrangement comprising a first heat exchange device configured to liquefy the high pressure gaseous oxygen stream and at least a portion of the high pressure gaseous air stream via indirect heat exchange with a refrigerant stream to yield a liquid oxygen stream and a liquid air stream. The heat exchanger arrangement also includes a second heat exchange device configured to densify the liquified oxygen stream via indirect heat exchange with the liquid air stream which yields the densified liquid oxygen and a cold vaporized air stream. The refrigerant stream comprises a mixture of the exhaust streams from one or more turbines with the cold vaporized air stream.

Abstract: Enhancements to the distillation column system and cycles for an argon and nitrogen producing cryogenic air separation unit are provided. The enhancements include systems and methods for: (i) recovery of xenon and krypton; (ii) production of oxygen product substantially free of hydrocarbons; and (iii) improvement in the design and performance of the super-stage argon column. The present systems and methods are further characterized in an oxygen enriched stream from the lower pressure column of the air separation unit is an oxygen enriched condensing medium used in the argon condenser.

Abstract: A system and method for argon and nitrogen extraction and liquefaction from a low-pressure tail gas of an ammonia production plant is provided. The preferred tail gas of the ammonia production plant comprises methane, nitrogen, argon, and hydrogen. The disclosed system and method provides for the methane rejection via rectification and hydrogen rejection by way of a side stripper column or phase separator. The resulting nitrogen and argon containing stream is separated and liquefied in a double column distillation system.

Abstract: A moderate pressure, argon and nitrogen producing cryogenic air separation unit and air separation cycle having a higher pressure column, a lower pressure column and an argon column arrangement is disclosed. The moderate pressure, argon and nitrogen producing cryogenic air separation unit is configured to take a first portion of an oxygen enriched stream from the lower pressure column, which together with an external source of liquid nitrogen is used as the boiling side refrigerant to condense the argon in the argon condenser. Use of the external source of liquid nitrogen in the argon condenser allows a second portion of the oxygen enriched stream from the lower pressure column to be taken as a liquid oxygen product stream.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.

Abstract: A method for compression of an incoming feed air stream using at least two variable speed compressor drive assemblies controlled in tandem is provided. The first variable speed drive assembly drives at least one compression stage in the lower pressure compressor unit driven while the second variable speed drive assembly drives higher pressure compression stage disposed either in the common air compression train or the split functional compression train of the air separation plant. The first and second variable speed drive assemblies are preferably high speed, variable speed electric motor assemblies each having a motor body, a motor housing, and a motor shaft with one or more impellers directly and rigidly coupled to the motor shaft via a sacrificial rigid shaft coupling.