Annular combustion chamber for a turbomachine with an improved inner fastening flange
View Patent ↗An annular combustion chamber for a turbomachine comprises inner and outer annular walls united by a transverse wall, the inner and outer walls are extended at their downstream ends by inner and outer fastener flanges for fastening respectively to inner and outer shells of a turbomachine casing in order to hold the combustion chamber in position, the inner flange being provided with a plurality of holes for feeding cooling air to a high pressure turbine of the turbomachine, the air feed holes through the inner flange being distributed circumferentially over at least two rows disposed in a staggered configuration.
1. An annular combustion chamber for a turbomachine, the chamber comprising inner and outer annular walls united by a transverse wall, the inner and outer walls being extended at their downstream ends by inner and outer fastener flanges for being fastened respectively to inner and outer shells of a casing of the turbomachine in order to hold the combustion chamber in position, the inner flange being provided with a plurality of holes for feeding cooling air to a high pressure turbine of the turbomachine, wherein the air feed holes through the inner flange are distributed circumferentially over at least two rows disposed in a staggered configuration.
2. A combustion chamber according to claim 1 , in which the inner and outer walls are provided with a plurality of holes for feeding the chamber with air, wherein the air feed holes through the inner flange are radially offset relative to the air feed holes through the inner wall.
3. A combustion chamber according to claim 1 , in which the inner shell of the turbomachine casing is provided with a plurality of orifices, wherein the air feed holes through the inner flange are radially offset relative to the orifices through the inner shell of the casing.
4. An inner flange for holding a turbomachine combustion chamber in position, wherein said combustion chamber comprises inner and outer annular walls united by a transverse wall, the inner and outer walls being extended at their downstream ends by said inner flange and by an outer flange, wherein said inner flange is configured to fasten to an inner shell of a casing of the turbomachine in order to hold the combustion chamber in position, the inner flange being provided with a plurality of holes for feeding cooling air to a high pressure turbine of the turbomachine, wherein the air feed holes through the inner flange are distributed circumferentially over at least two rows disposed in a staggered configuration.