This invention relates in general to LNG liquefaction systems or plants that include a gas turbine fueled by vaporized LNG and which receive compressed air, via an air compressor, as an input, and in particular this invention relates to a means and method to use relatively colder LNG vapor to remove heat from the air being inputted to the turbines' air compressors to improve overall efficiency of the systems or plants. As used herein the term “LNG” refers to liquid natural gas (primarily methane) which has been liquefied by refrigeration below the boiling point (e.g. −161,5° C., 111,7K depending on constituents of the gas) for storage and transport.
Other advantages and attributes of this invention will be readily discernable upon a reading of the text hereinafter.
An object of this invention is to provide a means and method to improve overall efficiency of LNG liquefaction systems.
These objects, and other objects expressed or implied in this document, are accomplished by a means and method incorporated in an LNG liquefaction system or plant that includes a gas turbine fueled by vaporized LNG and which receives compressed air, via an air compressor, as an input, the means and method using relatively colder LNG vapor produced by an LNG expander or a Joule-Thomson valve to cool the air in a heat exchanger disposed before the inlet to the air compressor, to improve the compressor, gas turbine and overall plant efficiency.
Referring to
Certain conventional LNG liquefaction systems and plants are powered by gas turbines. The fuel gas for the gas turbines is in many case clean vaporized LNG. The vaporized LNG is preferably produced by a two-phase LNG expander or alternatively by a Joule-Thomson valve. The vaporized LNG in the PHS is at its cold boiling temperature, as mentioned above, which is considerably colder than ambient air. Feeding some of the cold LNG vapor, depending on the settings of the CV1 and CV2 valves, can be used in the AHE to remove heat form the air at the inlet 16 of the air compressor 12 of the gas turbine GT.
The foregoing description and drawings were given for illustrative purposes only, it being understood that the invention is not limited to the embodiments disclosed, but is intended to embrace any and all alternatives, equivalents, modifications and rearrangements of elements falling within the scope of the invention as defined by the following claims.
This application claims the benefit of U.S. Provisional Application No. 60/793,964 filed Apr. 22, 2006.
Number | Date | Country | |
---|---|---|---|
60793964 | Apr 2006 | US |