| 发明名称 |
GAS TURBINE COMBUSTION CHAMBER WITH INTEGRATED TURBINE INLET GUIDE VANE RING AS WELL AS METHOD FOR MANUFACTURING THE SAME |
| 摘要 |
A gas turbine combustion chamber with an outer combustion chamber wall and an inner combustion chamber wall, wherein the outer combustion chamber wall and the inner combustion chamber wall are respectively formed in one piece with an outer or an inner ring-shaped platform that are connected in one piece with turbine inlet guide vanes which are arranged around the circumference, wherein the gas turbine combustion chamber is mounted only by means of a suspension device that is formed in one piece at the outer platform, as well as a method for manufacturing the same. |
| 申请公布号 |
US2017009989(A1) |
申请公布日期 |
2017.01.12 |
| 申请号 |
US201615202102 |
申请日期 |
2016.07.05 |
| 申请人 |
Rolls-Royce Deutschland Ltd & Co KG |
发明人 |
CLEMEN Carsten |
| 分类号 |
F23R3/00;B23P15/00 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine combustion chamber with an outer combustion chamber wall and an inner combustion chamber wall, wherein the outer combustion chamber wall and the inner combustion chamber wall are respectively formed in one piece with an outer or an inner ring-shaped platform which are connected in one piece with turbine inlet guide vanes that are arranged around the circumference, wherein the gas turbine combustion chamber is mounted only by means of a suspension device that is formed in one piece at the outer platform. |
| 地址 |
Blankenfelde-Mahlow DE |
