Turbomachine casing with treatment, a compressor, and a turbomachine including such a casing
View Patent ↗A casing supporting a series of stationary vanes between which there are disposed series of moving blades movable in rotation about a longitudinal axis in which the radially outer ends of the moving blades being close to the inside face of the casing is disclosed. The casing includes, at least over an annulus situated facing one of the series of moving blades, at least one casing treatment zone facing towards the blades and including a surface relief disturbance in the form of a groove of closed outline. The invention is applicable to controlling rotating separation in a turbomachine compressor.
1. A casing supporting a series of stationary vanes between which vanes there are located series of moving blades that are movable in rotation about a longitudinal axis, radially outer ends of said moving blades being close to an inside face of the casing, the casing comprising, in at least an annulus situated facing one of the series of moving blades:
at least one casing treatment zone facing the blades,
wherein the treatment zone includes at least one groove defining a closed outline with an outer perimeter and an inner perimeter, the outer and inner perimeter are both continuous, and a shape of the outer perimeter and a shape of the inner perimeter are similar.
2. A casing according to claim 1 , wherein said zone is localized over an angular sector corresponding to 1.5 to 2.5 times the pitch of the moving blades.
3. A casing according to claim 1 , wherein said treatment zone extends axially over a distance representing at least ⅔ of the length of the moving blades in the axial direction.
4. A casing according to claim 1 , wherein said treatment zone comprises a groove of which the closed outline is generally curved.
5. A casing according to claim 4 , wherein said treatment zone comprises an oval groove.
6. A casing according to claim 1 , wherein said treatment zone comprises a groove defined by a step of rectilinear segments interconnected to form an irregular geometrical figure.
7. A casing according to claim 6 , wherein said geometrical figure has eight sides.
8. A casing according to claim 1 , wherein said casing treatment zone is formed in a plate fitted to the casing.
9. A casing according to claim 8 , wherein said plate is made of an abradable material.
10. A casing according to claim 1 , further including a cavity formed radially outside the treatment zone.
11. A casing according to claim 10 , including a plurality of treatment zones and wherein said cavity of each treatment zone is in communication with said cavity of another treatment zone.
12. A casing according to claim 10 , wherein the depth of said cavity lies in the range 1 to 4 times the depth of the treatment zone.
13. A casing according to claim 10 , wherein the extent in the axial direction of said cavity lies in the range 10% to 20% greater than the extent in the axial direction of the treatment zone.
14. An axial compressor comprising:
a casing; the casing supporting a series of stationary vanes between which vanes there are located series of moving blades that are movable in rotation about a longitudinal axis, radially outer ends of said moving blades being close to an inside face of the casing, the casing including, in at least an annulus situated facing one of the series of moving blades:
at least one casing treatment zone facing the blades,
wherein the treatment zone includes at least one groove defining a closed outline with an outer perimeter and an inner perimeter, the outer and inner perimeter are both continuous, and a shape of the outer perimeter and a shape of the inner perimeter are similar.
15. A turbomachine comprising:
an axial compressor including a casing, the casing supporting a series of stationary vanes between which vanes there are located series of moving blades that are movable in rotation about a longitudinal axis, radially outer ends of said moving blades being close to an inside face of the casing, the casing including, in at least an annulus situated facing one of the series of moving blades:
at least one casing treatment zone facing the blades,
wherein the treatment zone includes at least one groove defining a closed outline with an outer perimeter and an inner perimeter, the outer and inner perimeter are both continuous, and a shape of the outer perimeter and a shape of the inner perimeter are similar.
16. A casing according to claim 1 , wherein a start point and an end point of the groove are coincident.