Annular combustor for a gas turbine

The invention relates to an annular combustor ( 13 ) for a gas turbine ( 10 ), into which combustor ( 13 ) burners ( 14, 15 ) open on an inlet side, and which combustor ( 13 ) extends in the axial direction from the inlet side to an outlet side ( 33 ) and is lined on the insides with cooled liner se...

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Bibliographische Detailangaben
Hauptverfasser:	GRAF PETER, TSCHIRREN STEFAN, WUNDERLE HELMAR
Format:	Patent
Sprache:	eng
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:	The invention relates to an annular combustor ( 13 ) for a gas turbine ( 10 ), into which combustor ( 13 ) burners ( 14, 15 ) open on an inlet side, and which combustor ( 13 ) extends in the axial direction from the inlet side to an outlet side ( 33 ) and is lined on the insides with cooled liner segments ( 16, 17 ) for protection from the hot gases. In such a combustor, increased mechanical stability and flexibility in design and also simplification in manufacture and fitting are achieved by the liner segments ( 16, 17 ) being subdivided in the axial direction into a plurality of parts ( 16, 17 ) arranged one behind the other.