| 摘要 |
A combustion chamber of a gas turbine assembly comprises: a casing (8), defining a combustion volume (8a) therein; a heat shield (10), which lines the inside of the casing (8) and comprises a plurality of tiles (12, 12a, 12b) of a refractory material; structural elements (15) shaped so as to define housing seats (26) of the tiles (12, 12a, 12b) and withhold the tiles (12, 12a, 12b) in the respective housing seats (26); and thermal protection elements (22), arranged so as to cover portions of the structural elements (15) facing the inside of the casing (8). |
