Sealing a hub cavity of an exhaust casing in a turbomachine
View Patent ↗The exhaust casing of a turbomachine includes a cylindrical jacket for guiding a flow of exhaust gas and for defining a hub cavity inside the casing, the jacket including at its ends an annular flange and a radial annular portion extending inwards and formed with an annular rim that is designed to be received in an annular groove of the inner wall of the exhaust casing to close the hub cavity in substantially sealed manner.
1. A turbomachine exhaust casing, comprising:
two coaxial cylindrical walls, respectively a radially inner wall and a radially outer wall, the walls being interconnected by radial arms; and
a cylindrical jacket secured to a downstream end of the radially inner wall and co-operating with the radially inner wall to define a hub cavity and co-operating with the radially outer wall to define a flow space for exhaust gas, an upstream end of the cylindrical jacket including a radial annular portion extending toward an axis of the turbomachine,
wherein the radial annular portion of the cylindrical jacket includes at its radially inner end an annular rim that co-operates with the radially inner wall of the exhaust casing by sliding radially in a substantially sealed manner.
2. The exhaust casing according to claim 1 , wherein:
an upstream end of the radially inner wall has two annular flanges, respectively an upstream flange and a downstream flange,
the two annular flanges extend radially outward and face each other in such a manner as to form an annular groove for receiving the annular rim of the cylindrical jacket with axial clearance, and
the annular rim is disposed within the annular groove to provide a sealed connection between the cylindrical jacket and the radially inner wall that allows the annular rim of the cylindrical jacket to move radially.
3. The exhaust casing according to claim 2 , wherein each of the two flanges of the inner wall of the exhaust casing presents a radial dimension that is greater than a maximum acceptable amplitude for radial displacement of the annular rim of the cylindrical jacket caused by thermal expansion thereof.
4. The exhaust casing according to claim 2 , wherein the annular rim of the cylindrical jacket extends substantially to a bottom of the annular groove in the inner wall of the exhaust casing when the turbomachine is stopped.
5. The exhaust casing according to claim 2 , wherein the cylindrical jacket is prestressed when the turbomachine is in a stopped condition, in such a manner as to press an upstream face of the annular rim of its radial annular portion against the upstream annular flange of the inner wall of the exhaust casing as to provide sealing for the hub cavity.
6. The exhaust casing according to claim 2 , wherein the cylindrical jacket is prestressed, when the turbomachine is in a stopped condition, in such a manner as to press a downstream face of the annular rim of its radial annular portion against the downstream annular flange of the inner wall of the exhaust casing, in order to provide sealing for the hub cavity.
7. The exhaust casing according to claim 1 , wherein the annular rim of the radial annular portion of the cylindrical jacket includes a cylindrical collar at its radially outer end, the collar extending upstream and forming a radial abutment for bearing against the upstream annular flange of the inner wall of the exhaust casing.
8. The exhaust casing according to claim 1 , wherein the radial annular portion of the cylindrical jacket includes orifices for passing a stream of ventilation air.
9. The exhaust casing according to claim 1 , wherein:
the cylindrical jacket includes at one of its ends an annular rim and includes at its other end a radial annular portion that extends inward, and
the radial annular portion includes at its radially inner end a radial annular rim formed with a cylindrical collar.
10. A turbomachine, including an exhaust casing according to claim 1 .