INTEGRATED COMBUSTOR NOZZLE FOR A SEGMENTED ANNULAR COMBUSTION SYSTEM

INTEGRATED COMBUSTOR NOZZLE FOR A SEGMENTED ANNULAR COMBUSTION SYSTEM

The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner s...

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Hauptverfasser: BERRY, Jonathan, Dwight, HUGHES, Michael, John, CITENO, Joseph, Vincent, WIDENER, Stanley, Kevin, HAFNER, Matthew, Troy
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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creator BERRY, Jonathan, Dwight
HUGHES, Michael, John
CITENO, Joseph, Vincent
WIDENER, Stanley, Kevin
HAFNER, Matthew, Troy
description The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner segment. The fuel injection panel includes a first side wall, a second side wall, and a plurality of premixing channels between the first and second side walls, each of the premixing channels having an outlet on one of the first and second side walls. The aft end of the fuel injection panel defines a turbine nozzle.
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subjects BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title INTEGRATED COMBUSTOR NOZZLE FOR A SEGMENTED ANNULAR COMBUSTION SYSTEM
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