Turbine to operate at part-load

A turbine includes a compressor (10) to intake a fluid and to compress the fluid, a combustion chamber (20) to heat the fluid from the compressor, a turbine section (30) to rotate a shaft with the heated fluid from the combustion chamber, and a bypass circuit (50) to generate a bypass flow by removi...

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Bibliographische Detailangaben
Hauptverfasser:	Garg, Umesh, Valliappan, Lakshmanan, John, Joshy, Subramaniyan, Moorthi
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	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
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Beschreibung
Zusammenfassung:	A turbine includes a compressor (10) to intake a fluid and to compress the fluid, a combustion chamber (20) to heat the fluid from the compressor, a turbine section (30) to rotate a shaft with the heated fluid from the combustion chamber, and a bypass circuit (50) to generate a bypass flow by removing a portion of the fluid from the compressor (10), to heat (54) the bypass flow, and to insert the bypass flow to the turbine section (30).