COMBUSTOR WITH STAGED FUEL PREMIXER

PROBLEM TO BE SOLVED: To provide a combustor 120 for mixing a flow 150 of compressed air from a compressor 110 and a flow 170 of fuel from a fuel source 160. SOLUTION: This combustor 120 may include a first swirler 180 for mixing the flow 150 of compressed air and the flow 170 of fuel into a first f...

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Bibliographische Detailangaben
Hauptverfasser:	SIMONS GIRARD A, VANDALE DANIEL D
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a combustor 120 for mixing a flow 150 of compressed air from a compressor 110 and a flow 170 of fuel from a fuel source 160. SOLUTION: This combustor 120 may include a first swirler 180 for mixing the flow 150 of compressed air and the flow 170 of fuel into a first fuel-air flow 190, a second flow source 200 for providing a second flow 210 to downstream of the first swirler 180, and a second swirler 220 for mixing the first fuel-air flow 190 and the second flow 210. COPYRIGHT: (C)2007,JPO&INPIT