| 摘要 |
The present invention provides a damper for a gas turbine. The damper (1) for a gas turbine combustion chamber, in figure 1, comprises a damper capacity unit wall (3) and a main neck unit. The damper capacity unit wall (3) limits a damper capacity unit (2) in the damper capacity unit wall (3), and the main deck unit includes a main neck unit wall (4) limiting a neck unit capacity unit (5) in the main neck unit wall (4). The main neck unit is connected to the damper capacity unit (2) for fluid connection between the damper capacity unit (2) and the gas turbine combustion chamber (6). Moreover, the damper comprises a gap (7) between the main neck unit wall (4) and the damper capacity unit wall (3). The main neck unit limits a main neck unit axis (8). Desirably, the gap (7) is a second neck unit. According to an additional embodiment of the present invention, a plurality of damper capacity units are provided. |
