| 发明名称 |
DAMPER FOR A GAS TURBINE |
| 摘要 |
A damper for a gas turbine combustion chamber as shown in FIG. 1 includes a damper volume wall and a main neck. The damper volume wall defines a damper volume inside the damper volume wall. The main neck includes a main neck wall defining a main neck volume inside the main neck wall. The main neck is associated with the damper volume for fluid communication between the damper volume and the gas turbine combustion chamber. In addition, the damper includes a gap between the main neck wall and the damper volume wall. The main neck defines a main neck axis. For example, the gap is a second neck, and in further embodiments, multiple damper volumes are provided. |
| 申请公布号 |
US2016161118(A1) |
申请公布日期 |
2016.06.09 |
| 申请号 |
US201514958386 |
申请日期 |
2015.12.03 |
| 申请人 |
General Electric Technology GmbH |
发明人 |
TONON Devis;BOTHIEN Mirko Ruben |
| 分类号 |
F23M20/00;F23R3/00 |
主分类号 |
F23M20/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A damper for a gas turbine combustion chamber, comprising:
a damper volume wall defining a damper volume inside the damper volume wall, and a main neck,
the main neck including a main neck wall defining a main neck volume inside the main neck wall, andthe main neck being associated with the damper volume for fluid communication between the damper volume and the gas turbine combustion chamber, the damper including a gap between the main neck wall and the damper volume wall. |
| 地址 |
Baden CH |
