Damper arrangement for reducing combustion-chamber pulsations
AssigneeAlstom (Switzerland) Ltd
InventorsJaan Hellat, Stefan Tschirren, Peter Stuber, Christian Oliver Paschereit
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AssigneeAlstom (Switzerland) Ltd
InventorsJaan Hellat, Stefan Tschirren, Peter Stuber, Christian Oliver Paschereit
Estimating the term…
The invention relates to a damper arrangement for reducing combustion-chamber pulsations arising inside a gas turbine (1), having a combustion-chamber housing (8) which upstream comprises a front plate (2) with a plurality of individual burners (6) and damping elements (7, 7a, 7b) projecting through the front plate (2) and downstream is connected to a turbine stage (9) and is surrounded by a turbine housing (3) which comprises first openings (5a) which are adapted to the burners (6) and through which the burners (6) project upstream. The invention is characterized in that closable second openings (5b), through which it is possible to insert and tune the damping elements (7, 7a, 7b), are provided inside the turbine housing (9) adjacent to the first openings (5a) adapted to the burners (6).
A damper arrangement for reducing combustion-chamber pulsations arising inside a gas turbine, comprising:
Dependencies are inferred from the claim text.