Annular combustion chamber for a turbomachine
View Patent ↗An annular combustion chamber for a turbomachine is disclosed. The chamber includes an inner wall, an outer wall, and a chamber end wall disposed between the inner and outer walls in the upstream region of the chamber. The chamber end wall presents an outer fastener rim and/or an inner fastener rim, and the outer and/or inner wall presents a respective upstream fastener rim. The chamber end wall and the outer and/or inner wall are fastened together via their fastener rims. Cooling channels are made between the fastener rims and open out to the inside of the combustion chamber. Advantageously, a spacer is placed between the fastener rims, and the channels are formed in the thickness or in the sides of the spacer.
1. An annular combustion chamber for a turbomachine, the chamber comprising:
an inner wall with an axially extending upstream fastener rim integrally made therewith and an outer wall with an axially extending upstream fastener rim integrally made therewith, downstream ends of the inner wall and the outer wall defining an outlet of the combustion chamber; and
a chamber end wall disposed between said inner and outer walls in an upstream region of said chamber, the chamber end wall presenting a central portion provided with a plurality of orifices, an axially extending outer fastener rim, and an axially extending inner fastener rim, the outer and inner fastener rims being integrally made with the central portion of the chamber end wall, and the chamber end wall and the inner wall being fastened together via the inner fastener rim of the chamber end wall and the upstream fastener rim of the inner wall, the chamber end wall and the outer wall being fastened together via the outer fastener rim of the chamber end wall and the upstream fastener rim of the outer wall, with the inner fastener rim of the chamber end wall and the upstream fastener rim of the inner wall being in direct contact with each other and the outer fastener rim of the chamber end wall and the upstream fastener rim of the outer wall being in direct contact with each other,
wherein cooling channels extend between the inner fastener rim of the chamber end wall and the upstream fastener rim of the inner wall, and between the outer fastener rim of the chamber end wall and the upstream fastener rim of the outer wall, from outside to inside of the combustion chamber, a first set of cooling channels being defined by an outer circumferential surface of the upstream fastener rim of the inner wall and an inner circumferential surface of the inner fastener rim of the chamber end wall, and a second set of cooling channels being defined by an inner circumferential surface of the upstream fastener rim of the outer wall and an outer circumferential surface of the outer fastener rim of the chamber end wall.
2. A combustion chamber according to claim 1 , wherein the cooling channels are formed by grooves made in the fastener rim of the chamber end wall, and/or in the fastener rim of said inner or outer wall.
3. A combustion chamber according to claim 2 , wherein said grooves are made by removing material of the fastener rim.
4. A combustion chamber according to claim 3 , wherein said grooves be made by machining the fastener rim.
5. A combustion chamber according to claim 2 , wherein said grooves are made by deforming the fastener rim.
6. A combustion chamber according to claim 5 , wherein said grooves are made by stamping the fastener rim.
7. A combustion chamber according to claim 2 , wherein the cooling channels are made by grooves formed both in the outer and inner fastener rims of the chamber end wall, and the fastener rim of the outer and inner walls.
8. A turbomachine including a combustion chamber according to claim 1 .
9. A combustion chamber according to claim 1 , wherein the outer and inner fastener rims of the chamber end wall are substantially parallel with the upstream fastener rims integrally made with the outer and inner walls.
10. An annular combustion chamber for a turbomachine, the chamber comprising:
an inner wall;
an outer wall with a radially extending upstream fastener rim; and
a chamber end wall disposed between said inner and outer walls in an upstream region of said chamber, the chamber end wall integrally made with the inner wall and presenting a radially extending outer fastener rim integrally made with the end wall, the chamber end wall and the outer wall being fastened together via the outer fastener rim of the chamber end wall and the upstream fastener rim of the outer wall, with the fastener rims being in direct contact with each other,
wherein cooling channels extend between the fastener rims, from outside to inside of the combustion chamber, the cooling channels being defined by a downstream surface of the outer fastener rim of the chamber end wall and an upstream surface of the upstream fastener rim of the outer wall, and
wherein the turbomachine presents a main axis and the upstream fastener rim of the outer wall and the outer fastener rim of the chamber end wall extend substantially perpendicularly to said main axis.
11. A combustion chamber according to claim 10 , wherein the fastener rims are scalloped.
12. A combustion chamber according to claim 1 , wherein the chamber end wall and the outer and inner walls are fastened together by bolts passing through their fastener rims.
13. A combustion chamber according to claim 10 , wherein a spacer is provided between the outer fastener rim of the chamber end wall and the upstream fastener rim of the outer wall.
14. A combustion chamber according to claim 13 , wherein the spacer is in the form of a ring and is provided with scallops.