Combustor assembly for a turbomachine

A combustor assembly for a turbomachine includes combustor housing (20) and a flow sleeve (50) arranged between the combustor housing (20) and a combustor line (34). The flow sleeve (50) defines a first annular fluid passage (59), and a second annular fluid passage (60). A quaternary cap (64) is mou...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Rohrssen, Robert Joseph, Charters, Erich Daniel, Khan, Abdul Rafey, Vanselow, John Drake, Melton, Patrick Benedict
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS 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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