HEAT SHIELD ARRANGEMENT FOR A HIGH TEMPERATURE GAS CONVEYING COMPONENT, IN PARTICULAR FOR A GAS TURBINE COMBUSTION CHAMBER

The heat shield for gas turbine combustion chambers comprises a series of tiles (26A, 26B) arranged side-by-side with gaps (45) between. These are mounted on a support plate (31) and enclose chambers (37) for cooling gas. The gaps between the plates form outlets (43) for coolant (K). Independent cla...

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Bibliographische Detailangaben
Hauptverfasser:	DAHLKE, STEFAN, PUETZ, HEINRICH
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES COMBUSTION APPARATUS COMBUSTION PROCESSES DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS WEAPONS
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Beschreibung
Zusammenfassung:	The heat shield for gas turbine combustion chambers comprises a series of tiles (26A, 26B) arranged side-by-side with gaps (45) between. These are mounted on a support plate (31) and enclose chambers (37) for cooling gas. The gaps between the plates form outlets (43) for coolant (K). Independent claims are included for: (a) combustion chambers fitted with the heat shield; and (b) gas turbines incorporating the combustion chamber.