FUEL SUPPLY SYSTEM FOR A POWER GENERATION SYSTEM

Abstract: the present invention relates to a fuel supply system (10) for a power generation system (1), in particular for a micro gas turbine system. the fuel supply system (10) comprises a fuel supply line (110), a fuel main line (120) and a fuel distribution line (130), a fuel compressor (200), and a decoupling vessel (300). the fuel supply line (110) is fluidically connected to the fuel compressor (200) and is able to be connected to a fuel source (11) in order to supply fuel from the fuel source (11) to the fuel compressor (200). the decoupling vessel (300) is disposed downstream of the fuel compressor (200) and is fluidically connected to the fuel compressor (200) by way of the fuel main line (120). the fuel distribution line (130) is disposed downstream of the decoupling vessel (300) and is fluidically connected to the latter. the fuel distribution line (130) is able to be fluidically connected to at least one combustion unit (20) of the power generation system (1), and is conceived to supply the at least one combustion unit (20) with fuel from the decoupling vessel (300).

Inventor(s): Mathias Kosch

CPC Classification: F02C9/40 (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines ; jet-propulsion plants ; construction of compressors or fans ; generating combustion products of high pressure or high velocity ; using gas turbines in compression refrigeration plants ))

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