Gas turbine and associated cooling method
US7040097B2 · kind B2 · utility
15Cited by
6References
11Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Aug 6, 2004 |
| Grant date | May 9, 2006 |
| Priority date | — |
| Expiry date | Aug 6, 2024 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/2322
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine (1), in particular in a power plant, has at least one combustion chamber (2) and an enclosed inner liner (3) which surrounds the combustion chamber (2) and an enclosed outer liner (4), having a stator (5) which has at least one vane row (6) with a plurality of vanes (7), a rotor (8) which has at least one blade row (9) with a plurality of blades (10), an air cooling arrangement (31) which is designed for cooling parts of the gas turbine (1) with air (L), and a steam cooling arrangement (32) which is designed for cooling parts of the gas turbine (1) with steam (D).
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.