Title:
ガスタービン
Document Type and Number:
Japanese Patent JP2005538310
Kind Code:
A
Abstract:
The gas turbine combustion chamber (4) is made of coolant tubes (24) defining the combustion chamber wall (23). The coolant pipes can be cast and have a trapezoidal cross section. The coolant pipes can be attached to multiple similar support rings (36). The coolant pipes can be attached to the rings by screws.
More Like This:
| WO/2020/127800 | ANTI-COKING |
| WO/2009/107311 | GAS TURBINE AND METHOD OF OPENING CASING OF GAS TURBINE |
| JP2016006374 | IMPINGEMENT COOLED WALL ARRANGEMENT |
Inventors:
Schulten, Wilhelm
Yeppel, Paul-Heinz
Yeppel, Paul-Heinz
Application Number:
JP2004540568A
Publication Date:
December 15, 2005
Filing Date:
September 01, 2003
Export Citation:
Assignee:
Siemens Aktiengesellschaft
International Classes:
F02C7/18; F02C7/00; F23R3/00; F23R3/42; (IPC1-7): F02C7/18; F02C7/00; F23R3/42
Attorney, Agent or Firm:
Iwao Yamaguchi