| 摘要 |
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 ).
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