Semi-detached houses of a combustion chamber

摘要

The present invention relates to a combustion chamber for a turbojet comprising a structural wall (2, 3) covered on one of its faces by at least one ring (12) of tiles (13) juxtaposed circumferentially, said ring (12) being fastened by its upstream and downstream edges in two opposite grooves (10a, 10b) each delimited by an annular wing (11a, 11b) at a spacing from the structural wall (2, 3), characterised in that at least one of said wings (11b) comprises a circumferential cutout (15) adapted to allow the mounting of said ring (12) of tiles (13) by successive introduction of the tiles (13) of said ring (12) via said cutout (15) and engagement by rotation in said two grooves (10a, 10b) and in that two adjacent tiles of said ring are positioned overlapping facing said cutout (15) so as to prevent a tile (13) coming out via said cutout (15). IMAGE