Gas turbine combustors

A centerbody construction for use in a gas turbine combustor includes a pair of inner (98) and outer (96) generally cylindrical members, the inner member having a diverging cup portion (110,114) attached to its forward end extending toward the outer cylindrical member, and a coolant manifold (120) a...

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Bibliographische Detailangaben
Hauptverfasser:	BEAUDOIN, ELIZABETH BYRNE, THIBAULT, BERNARD ANDRE, JR
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 centerbody construction for use in a gas turbine combustor includes a pair of inner (98) and outer (96) generally cylindrical members, the inner member having a diverging cup portion (110,114) attached to its forward end extending toward the outer cylindrical member, and a coolant manifold (120) arranged between the inner and outer cylindrical members radially adjacent the centerbody cup portion.