Patent ID: 7017350

Claim:
An annular combustion chamber for a turbomachine of axis X, the chamber comprising a radially-inner side wall, a radially-outer side wall, and a chamber end wall disposed between said inner and outer side walls in the upstream region of said chamber, said chamber end wall being fixed to said inner and outer side walls by means of a plurality of radially-inner attachment fittings and by means of a plurality of radially-outer attachment fittings disposed upstream from said chamber end wall by bolting a zone of each of said fittings to said side walls, wherein at least one of said pluralities of attachment fittings is integrated in a ring secured to the chamber end wall and comprises a plurality of pairs of tabs which extend upstream beyond the bolting zones, the two tabs in each pair being disposed circumferentially on either side of a bolting zone and being interconnected at their upstream end to the upstream end of a fixing plate which extends between said two tabs and which presents a bolting zone for being fixed to the adjacent side wall.