MIXING SYSTEM

This application describes a mixing system 32 for a gas turbine combustor arrangement, the mixing system 32 comprising a lobed mixer 10 and a wall 40, 42 enclosing a fluid flow path 34, wherein the lobed mixer 10 is arranged in the wall 40, 42 between a first part of the wall 40 and a second part of...

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Bibliographische Detailangaben
Hauptverfasser:	Wysocki, Stefan, Luebcke, Holger
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:	This application describes a mixing system 32 for a gas turbine combustor arrangement, the mixing system 32 comprising a lobed mixer 10 and a wall 40, 42 enclosing a fluid flow path 34, wherein the lobed mixer 10 is arranged in the wall 40, 42 between a first part of the wall 40 and a second part of the wall 42, and wherein the first part of the wall 40 and the second part of the wall 42 are spaced apart in the direction of a lobed mixer axis 50. Details of the lobed mixer 10 and a method of mixing two flows in a mixing system are also described.