Turbine engine combustion chamber with tangential slots
View Patent ↗A turbine engine annular combustion chamber, including longitudinal walls connected by a transverse chamber bottom and a single-piece cowling, the chamber bottom and the cowling each including an inner flange and an outer flange each with a plurality of holes made in it for the passage of fixing systems for fixing the cowling on the chamber bottom. Each fixing system has associated with it at least one tangential slot formed on the corresponding flange of the chamber bottom and/or on the corresponding flange of the cowling, each slot being formed in the immediate vicinity of the corresponding fixing system.
1. A turbine engine annular combustion chamber having a longitudinal axis, said annular combustion chamber comprising longitudinal walls connected by a transverse chamber bottom and a single-piece cowling, the chamber bottom and the cowling each comprising an inner flange and an outer flange, each of said inner and outer flanges extending in a circumferential direction around said longitudinal axis of said annular combustion chamber, and each of said inner and outer flanges including a plurality of holes for the passage of fixing systems for fixing the cowling on the chamber bottom, wherein each fixing system is associated with at least one tangential slot formed on the corresponding flange of the chamber bottom and/or on the corresponding flange of the cowling, each slot being formed in the immediate vicinity of the corresponding fixing system,
wherein each slot substantially extends in said circumferential direction.
2. A turbine engine comprising an annular combustion chamber according to claim 1 and a turbine downstream of said annular combustion chamber.
3. A turbine engine annular combustion chamber as in claim 1 , wherein each fixing system is associated with at least one tangential slot formed on the corresponding flange of the chamber bottom.
4. A turbine engine annular combustion chamber as in claim 1 , wherein each fixing system is associated with at least one tangential slot formed on the corresponding flange of the cowling.
5. A turbine engine annular combustion chamber as in claim 4 , wherein each fixing system is associated with at least one tangential slot formed on the corresponding flange of the cowling.
6. A turbine engine annular combustion chamber as in claim 1 , wherein the inner and outer flanges are free of any slots between two adjacent tangential slots.
7. A turbine engine annular combustion chamber as in claim 1 , wherein each slot is located entirely upstream of an associated fixing system.
8. A turbine engine annular combustion chamber as in claim 1 , wherein the longitudinal walls are devoid of any tangential slots.
9. A turbine engine annular combustion chamber as in claim 1 , wherein each slot extends over a same distance on either side of the associated fixing system.
10. A turbine engine annular combustion chamber as in claim 1 , wherein each slot has two ends, each end on each side of the associated fixing system.
11. A turbine engine annular combustion chamber as in claim 10 , wherein each slot has a portion between said two ends, said portion being located upstream relative to said two ends.
12. A turbine engine annular combustion chamber as in claim 1 , wherein each slot has two ends, each end being located upstream of the associated fixing system.