Separator for feeding cooling air to a turbine
View Patent ↗A combustion chamber which is fitted with a separator disposed between the radially inner wall of the chamber and the inner flange of the chamber is disclosed. The separator includes a tubular portion and a fastener portion. The tubular portion is centered on the main axis of the combustion chamber, with the upstream end thereof being situated upstream from orifices in the radially inner wall of the chamber. The fastener portion is secured to the combustion chamber. The tubular portion splits the flow of air running along the radially inner wall into an inner air flow passing between the tubular portion and the inner flange of the chamber, and an outer air flow passing between the radially inner wall and the tubular portion.
1. An annular combustion chamber comprising:
a radially inner wall;
an inner flange; and
a separator disposed between the radially inner wall and the inner flange, said separator including a tubular portion and a fastener portion, the tubular portion being centered on a main axis of said combustion chamber and having an upstream end that is situated upstream from orifices in said radially inner wall of the chamber, and the fastener portion being secured to said combustion chamber,
wherein said inner flange extends from a downstream part of the radially inner wall inwards towards the main axis and then upstream such that said inner flange is coaxial with the radially inner wall, and a radius of said inner flange is smaller than a radius of the radially inner wall, and
wherein said upstream end of said tubular portion splits a flowsection situated between said radially inner wall of the chamber and said inner flange into an inner annular flowsection and an outer annular flowsection such that the flow of air passing along the radially inner wall is split into an inner air flow passing between said tubular portion and said inner flange of said chamber, and an outer air flow passing between said radially inner wall and said tubular portion, and
wherein said tubular portion is substantially parallel to said radially inner wall of said chamber such that said outer annular flowsection is of substantially constant cross-section.
2. A combustion chamber according to claim 1 , wherein said fastener portion is a downstream end of the tubular portion, said downstream end being rigidly fastened to said inner flange.
3. A combustion chamber according to claim 1 , wherein said fastener portion is a radial portion that extends from said tubular portion towards said main axis, and in that said fastener portion is pierced by main holes for passing the air of said inner air flow from upstream to downstream.
4. A combustion chamber according to claim 3 , wherein said separator is fastened to said inner flange by a radially inner end of said radial portion.
5. A combustion chamber according to claim 4 , wherein the radially inner end of said radial portion is pierced by holes suitable for receiving a fastener device for fastening said radial portion on said inner flange.
6. A combustion chamber according to claim 3 , wherein said separator is in contact with said inner flange via a downstream end of said tubular portion.
7. A combustion chamber according to claim 3 , wherein the area of said main holes occupies 60% to 80% of the area of an effective section of said radial portion.
8. A combustion chamber according to claim 3 , wherein said main holes are distributed over the entire circumference of said radial portion.
9. A combustion chamber according to claim 1 , wherein said fastener portion of the separator is connected to said tubular portion in the upstream half of said tubular portion.
10. A combustion chamber according to claim 1 , wherein a leading edge of said upstream end of the tubular portion is rounded.
11. A turbomachine provided with said combustion chamber according to claim 1 .
12. A combustion chamber according to claim 2 , wherein said downstream end of the tubular portion is brazed to said inner flange.