초록 ▼

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 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).

대표청구항 ▼

1. A damper arrangement for reducing combustion-chamber pulsations arising inside a gas turbine, comprising: a combustion-chamber housing, said combustion-chamber housing having a front plate at an upstream side; a plurality of individual burners and damping elements projecting through the front

1. A damper arrangement for reducing combustion-chamber pulsations arising inside a gas turbine, comprising: a combustion-chamber housing, said combustion-chamber housing having a front plate at an upstream side; a plurality of individual burners and damping elements projecting through the front plate; said combustion-chamber housing being connected at a downstream side to a turbine stage and being surrounded by a turbine housing; said turbine housing having first openings through which the burners project in an upstream direction, and closable second openings adjacent to the first openings and through which the damping elements are adapted to be inserted and tuned. 2. The damper arrangement according to claim 1, wherein the first openings and the closable second openings in the turbine housing are substantially the same configuration. 3. The damper arrangement according to claim 1 or 2, wherein third openings are provided through the front plate, said burners and said damping elements projecting through said third openings. 4. The damper arrangement according to claim 3, wherein the third openings through the front plate are each of substantially the same configuration. 5. The damper arrangement according to claim 1 or 2, wherein a distance provided between the front plate and the closable second openings of the turbine housing is sufficient such that a damping element can be inserted completely between the front plate and the turbine housing. 6. The damper arrangement according to claim 1 or 2, wherein the damping elements each project upstream through a corresponding closable second opening in the turbine housing and are releasably connected thereto. 7. The damper arrangement according to claim 3, wherein the combustion chamber is an annular combustion chamber, the front plate is annular, and the third openings in the front plate are arranged adjacent to one another in at least one of the peripheral direction and the radial direction with respect to the annular front plate. 8. The damper arrangement according to claim 3, wherein the third openings through the front plate and the first and second openings in the turbine housing are arranged coaxially with one another. 9. The damper arrangement according to claim 1 or 2, wherein the damping elements each have a damping volume and are designed in the manner of at least one of a Helmholtz resonator and a λ/4 tube. 10. The damper arrangement according to claim 9, wherein at least part of the damping volume of a damping element projects beyond the turbine housing to the outside of the turbine housing. 11. The damper arrangement according to claim 10, wherein a tuning device that influences the damping behavior of a respective damping element is provided outside the turbine housing. 12. The damper arrangement according to claim 11, wherein the tuning device can be operated in at least one of an open regulating circuit, independently of combustion-chamber pulsations which arise, and a closed regulating circuit, in direct dependence upon combustion-chamber pulsations which arise. 13. The damper arrangement according to claim 12, wherein the oscillation frequency (fp) of the combustion-chamber pulsations can be supplied to said tuning device operating in a closed regulating circuit. 14. The damper arrangement according to claim 1 or 2, wherein each damping element is connected to a flushing line for cooling purposes.