发明名称 |
Axially segmented guide vane mount for a gas turbine |
摘要 |
A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety. |
申请公布号 |
US2011268580(A1) |
申请公布日期 |
2011.11.03 |
申请号 |
US200913127295 |
申请日期 |
2009.09.10 |
申请人 |
|
发明人 |
BRYK RODERICH;DUNGS SASCHA;HARTMANN MARTIN;KAHLSTORF UWE;KLEIN KARL;LUESEBRINK OLIVER;MILAZAR MIRKO;SAVILIUS NICOLAS;SCHNEIDER OLIVER;SHENG SHILUN;SHEVCHENKO VADIM;SIMON GERHARD;THAMM NORBERT |
分类号 |
F04D29/00 |
主分类号 |
F04D29/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|