SYSTEM COMPRISING A COMBUSTOR AND TURBINE INLET STATOR VANES

A system includes a combustor (102). The combustor (102) has a combustor wall (104) with a combustor dome (106) at an upstream end (114) of the combustor wall (104), and an outlet (108) at a downstream end (116) of the combustor wall (104) opposite the upstream end (114). The combustor wall (104) in...

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Bibliographische Detailangaben
Hauptverfasser:	PROCIW, Lev A, RYON, Jason
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 system includes a combustor (102). The combustor (102) has a combustor wall (104) with a combustor dome (106) at an upstream end (114) of the combustor wall (104), and an outlet (108) at a downstream end (116) of the combustor wall (104) opposite the upstream end (114). The combustor wall (104) includes an inner wall portion (120) and an outer wall portion (122) defining an interior of the combustor therebetween. Each of the inner wall portion (120) and outer wall portion (122) extends from the combustor dome (106) to the downstream end (116) of the combustor wall (104). The combustor wall (104) includes an air cooling passage (112) embedded inside at least one of the inner wall portion (120) and the outer wall portion (122). The air cooling passage (112) extends from the upstream end (114) of the combustor wall (104) to the downstream end (116) of the combustor wall (104).