Method and apparatus to facilitate reducing NOx emissions in turbine engines

Method and apparatus to facilitate reducing NOx emissions in turbine engines

A combustor liner includes an annular shell including a plurality of circumferentially extending panels, wherein the plurality of circumferentially extending panels includes a first panel positioned at an upstream end of the shell and a second panel positioned downstream from, and adjacent to, the f...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BURRUS, DAVID L, STICKLES, RICHARD W, DODDS, WILLARD J, JOHNSON, ARTHUR WESLEY
Format: Patent
Sprache:eng ; fre ; ger
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:A combustor liner includes an annular shell including a plurality of circumferentially extending panels, wherein the plurality of circumferentially extending panels includes a first panel positioned at an upstream end of the shell and a second panel positioned downstream from, and adjacent to, the first panel, a plurality of primary dilution holes (98) formed in the first panel (82), and a plurality of secondary dilution holes (100) formed in the second panel (86), the dilution holes configured to discharge dilution air into the shell.