COMBUSTOR DEVICE FOR A GAS TURBINE FOR BEING COUPLED TO AN OXYGEN GENERATION UNIT

The present invention relates to a combustor device (100) for a gas turbine (150). The combustor device (100) comprises an inner shell (110) which forms a combustion chamber (111) and an outer shell (120) surrounding the inner shell (110) such that an outer channel (101) is formed between the inner...

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Bibliographische Detailangaben
1. Verfasser:	SJÖDIN, MATS
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CHEMISTRY COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES COMPOUNDS THEREOF CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INORGANIC CHEMISTRY LIGHTING MECHANICAL ENGINEERING METALLURGY NON-METALLIC ELEMENTS WEAPONS
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