Combustion chamber with shroud for a gas turbine engine

摘要

The combustion chamber, comprising outer (31) and inner (32) annular walls and a gas flow separating fairing with an annular wall (21) having rear (22) and forward (24) sections, has the forward section extended rearwards to provide an additional fixing to the combustion chamber's outer wall. The rear section (22) of the fairing wall is fixed to the combustion chamber wall outer surface and the rearward extension on the forward section is fixed to an inner surface flange (34).