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US 2006/0207263 A1Published application
Combustion chamber
AssigneeSiemens Aktiengesellschaft
InventorsBernd Stöcker, Marc Tertilt
Life of this patent
Estimating the term…
Abstract
A combustion chamber (4) for a gas turbine (1), the combustion chamber wall (24) of which is furnished on the inside with a lining formed of a number of heat shield elements (26), is to be designed for a particularly high level of operating safety. To this end, one or a number of temperature sensors (28) is/are located according to the invention between combustion chamber wall (24) and heat shield elements (26).
Claims15
1-13. (canceled)
A combustion chamber for a gas turbine, comprising:
- a combustion chamber wall;
- a lining formed from a plurality of heat shield elements furnished on the inside of the combustion chamber;
- and
- a number of temperature sensors are arranged between combustion chamber wall and heat shield elements.
1 more element
A gas turbine, comprising:
- a turbine section;
- a compressor section;
- and
- a combustion chamber, comprising:
- a combustion chamber wall;
- a lining formed from a plurality of heat shield elements furnished on the inside of the combustion chamber;
- a number of temperature sensors are arranged between combustion chamber wall and heat shield elements.
4 more elements
Dependencies are inferred from the claim text.