COUNTER-SWIRL DOUBLET COMBUSTOR WITH PLUNGED HOLES

COUNTER-SWIRL DOUBLET COMBUSTOR WITH PLUNGED HOLES

An improved system, apparatus and method may comprise an inner liner (104) and an outer liner (102) extending circumferentially around an engine centerline axis (28) thereby forming a combustion chamber therebetween. The system, apparatus, and method may include a front end (130) extending between t...

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Hauptverfasser: Woubshet, Afework, Yount, Randall E, Graves, Charles B, Moore, Mindi D
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 Woubshet, Afework
Yount, Randall E
Graves, Charles B
Moore, Mindi D
description An improved system, apparatus and method may comprise an inner liner (104) and an outer liner (102) extending circumferentially around an engine centerline axis (28) thereby forming a combustion chamber therebetween. The system, apparatus, and method may include a front end (130) extending between the inner and outer liners (102, 104) and having a plurality of fuel nozzle ports (108) configured to each receive a fuel nozzle (110). First and second outer plunged inlet holes (140) may be formed in the outer liner (102) and extending in a first radial direction toward the engine centerline axis (28) and into at least a portion of the combustion chamber. First and second inner plunged inlet holes (140) may be formed in the inner liner (104) and extending in a second radial direction away from the engine centerline axis (28) and into at least a portion of the combustion chamber.
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The system, apparatus, and method may include a front end (130) extending between the inner and outer liners (102, 104) and having a plurality of fuel nozzle ports (108) configured to each receive a fuel nozzle (110). First and second outer plunged inlet holes (140) may be formed in the outer liner (102) and extending in a first radial direction toward the engine centerline axis (28) and into at least a portion of the combustion chamber. 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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 COUNTER-SWIRL DOUBLET COMBUSTOR WITH PLUNGED HOLES
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