Combustor with lean material opening

A turbine engine and a method of operating with the combustor shown and described. The turbine engine includes a combustor including an annular array of rich material cups and an annular array of lean material cups. A method for controlling nitrogen oxides includes injecting a fuel/air mixture from...

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Bibliographische Detailangaben
Hauptverfasser:	MOHAN SRIPATHY, GIRIDHARAN MANNANPATHY G, NAIK PRADEEP, NARASIMHA HIRASIMHA RAMANUJAM, BACCARO MICHAEL T, UKANTI PARUMARU, PATRA AJOY, BENJAMIN MICHAEL A, VISE STEVEN C
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES 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 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A turbine engine and a method of operating with the combustor shown and described. The turbine engine includes a combustor including an annular array of rich material cups and an annular array of lean material cups. A method for controlling nitrogen oxides includes injecting a fuel/air mixture from a lean cup and a rich cup. 一种涡轮发动机以及利用所示和所述的燃烧器操作的方法。涡轮发动机包括燃烧器，燃烧器包括环形阵列的富料杯和环形阵列的贫料杯。一种用于控制氮氧化物的方法，包括从贫料杯和富料杯喷射燃料/空气混合物。