SYSTEMS AND METHODS FOR OPERATING A TURBOCHARGED GAS TURBINE ENGINE
A power generation system (100) includes a combustion system (102), a turbocharger (106), and a heat recovery system (104). The combustion system (102) is configured to combust a fuel with a flow of air. The combustion system (102) is further configured to generate an exhaust stream. The turbocharge...
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| creator | SAMMAK, Majed PRABHUDHARWADKAR, Deoras ZIA, Jalal Hunain |
| description | A power generation system (100) includes a combustion system (102), a turbocharger (106), and a heat recovery system (104). The combustion system (102) is configured to combust a fuel with a flow of air. The combustion system (102) is further configured to generate an exhaust stream. The turbocharger (106) is configured to compress a flow of compressed air and to channel the flow of compressed air to the combustion system (102). The combustion system (102) is configured to combust the fuel with the flow of compressed air and an additional flow of air. The heat recovery system (104) is configured to recover heat from the exhaust stream and to drive the turbocharger (106). The heat recovery system (104) uses a supercritical working fluid to absorb heat from the exhaust stream and to drive the turbocharger (106). |
| format | Patent |
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The combustion system (102) is configured to combust a fuel with a flow of air. The combustion system (102) is further configured to generate an exhaust stream. The turbocharger (106) is configured to compress a flow of compressed air and to channel the flow of compressed air to the combustion system (102). The combustion system (102) is configured to combust the fuel with the flow of compressed air and an additional flow of air. The heat recovery system (104) is configured to recover heat from the exhaust stream and to drive the turbocharger (106). 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The combustion system (102) is configured to combust a fuel with a flow of air. The combustion system (102) is further configured to generate an exhaust stream. The turbocharger (106) is configured to compress a flow of compressed air and to channel the flow of compressed air to the combustion system (102). The combustion system (102) is configured to combust the fuel with the flow of compressed air and an additional flow of air. The heat recovery system (104) is configured to recover heat from the exhaust stream and to drive the turbocharger (106). 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The combustion system (102) is configured to combust a fuel with a flow of air. The combustion system (102) is further configured to generate an exhaust stream. The turbocharger (106) is configured to compress a flow of compressed air and to channel the flow of compressed air to the combustion system (102). The combustion system (102) is configured to combust the fuel with the flow of compressed air and an additional flow of air. The heat recovery system (104) is configured to recover heat from the exhaust stream and to drive the turbocharger (106). The heat recovery system (104) uses a supercritical working fluid to absorb heat from the exhaust stream and to drive the turbocharger (106).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | SYSTEMS AND METHODS FOR OPERATING A TURBOCHARGED GAS TURBINE ENGINE |
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