Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members

A gas turbine having an annular combustion chamber with walls made of ceramic matrix composite material mounted inside a metal casing by linking members fastened to the chamber by brazing and connecting the chamber to inner and outer metal shrouds of the casing,

• wherein the linking members comprise a plurality of inner linking tabs and a plurality of outer linking tabs which connect the combustion chamber to the inner and outer metal shrouds respectively, each linking tab having a first portion fastened to the outside surface of a wall of the combustion chamber by brazing, the first portions of said linking tabs being spaced apart from one another circumferentially so that the brazed connections between the chamber and the linking members are provided via a set of limited zones that are spaced apart from one another.