| 发明名称 |
COMBUSTION CHAMBER OF A GAS TURBINE |
| 摘要 |
A combustion chamber of a gas turbine, including an external combustion chamber wall as well as an internal combustion chamber wall, wherein the internal combustion chamber wall, at its frontal end area as it appears with respect to the flow direction of the combustion chamber, is supported in a longitudinally slidable manner inside a groove of a base plate that is arranged in the area of a combustion chamber head, and is fixedly attached at the external combustion chamber wall at its back end area. |
| 申请公布号 |
US2015260401(A1) |
申请公布日期 |
2015.09.17 |
| 申请号 |
US201514641883 |
申请日期 |
2015.03.09 |
| 申请人 |
Rolls-Royce Deutschland Ltd & Co KG |
发明人 |
GERENDÁS Miklós;CLEMEN Carsten;DOERR Thomas |
| 分类号 |
F23R3/00 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustion chamber of a gas turbine, comprising an external combustion chamber wall as well as an internal combustion chamber wall, wherein the internal combustion chamber wall, at its frontal end area as it appears with respect to the flow direction of the combustion chamber, is supported in a longitudinally slidable manner inside a groove of a base plate that is arranged in the area of a combustion chamber head, and is fixedly attached at the external combustion chamber wall at its back end area. |
| 地址 |
Blankenfelde-Mahlow DE |
