| 摘要 |
Combustion chamber (4) for a gas turbine comprises a combustion chamber wall (24) provided on the inside with a lining formed by a number of thermal shield elements (26). Each thermal shield element forms with the combustion chamber wall an inner chamber (27) loaded with a coolant (K) and containing a coolant distributor connecting a coolant feed line to a number of coolant outlet openings. An Independent claim is also included for a gas turbine comprising the above combustion chamber. Preferred Features: The coolant outlet openings are dimensioned so that the sum of the cross-sectional areas of all the coolant outlet openings of a coolant distributor is less than the cross-sectional area of the appropriate coolant feed line. |
