Attachment of a discharge conduit of a turbine engine

1. A discharge conduit for a turbine engine, comprising:

an air intake end;

an air outlet end; and

a tubular duct configured for guiding air between said ends,

wherein said air intake end being configured for attachment to an intermediate casing of the turbine engine,

wherein said air intake end comprises a tubular sleeve which is attached to an end of said tubular duct, said tubular sleeve comprising elastically deformable, resilient snap-in tabs, and

wherein the resilient snap-in tabs each have a free end having a retaining lip, each lip having a section which has a rounded convex profile extending over an angle of at least 180°.

2. The discharge conduit according to claim 1 , wherein the resilient snap-in tabs are designed to be fitted into an opening in the intermediate casing and to cooperate by resiliently snapping onto a peripheral edge of said opening.

3. The discharge conduit according to claim 1 , wherein the tubular sleeve defines a substantially rectangular cross section and has four sides, on each of which a resilient snap-in tab is provided.

4. The discharge conduit according to claim 1 , wherein said resilient snap-in tabs are independent of one another.

5. The discharge conduit according to claim 1 wherein said angle is greater than 220°.

6. An assembly comprising;

a discharge conduit according to claim 1 ; and

an intermediate casing, the intermediate casing comprising a hub having a substantially radial annular wall which comprises at least one discharge air passage opening which is designed to cooperate with said resilient snap-in tabs for attaching the conduit by resiliently snapping into said opening.

7. A turbine engine comprising:

an assembly that includes a discharge conduit according to claim 1 and an intermediate casing, the intermediate casing comprising a hub having a substantially radial annular wall which comprises at least one discharge air passage opening which is designed to cooperate with said resilient snap-in tabs for attachment of the conduit by resiliently snapping into said opening.

8. An assembly comprising:

a discharge conduit comprising an air intake end, an air outlet end, and a tubular duct configured for guiding air between said ends, wherein said air intake end being equipped with attachment elements for attachment to an intermediate casing of the turbine engine, said attachment elements are of the resilient snap-in type; and

an intermediate casing, the intermediate casing comprising a hub having a substantially radial annular wall which comprises at least one discharge air passage opening which is designed to cooperate with said attachment elements for attaching the conduit by resiliently snapping into said opening,

wherein said opening in the intermediate casing has a peripheral edge having a lead-in chamfer at the downstream end and a lead-out chamfer at the upstream end in order to make it easier to mount and dismount the conduit respectively.

9. A method for mounting a discharge conduit according to claim 1 , the method comprising the steps of:

attaching the air intake end of the discharge conduit to the intermediate casing by engaging the resilient snap-in elements of the discharge conduit in a corresponding opening in the intermediate casing such that the discharge conduit adopts a pre-mounting position, and

attaching the air outlet end of the discharge conduit such that the discharge conduit is in a final position which is different from the pre-mounting position, the movement of the discharge conduit from its pre-mounting position into its final position being carried out by the discharge conduit engaging further in the opening in the casing.

10. The method according to claim 9 , wherein the movement of the discharge conduit in the step of attaching the air outlet end of the discharge conduit causes a peripheral seal to be compressed between the discharge conduit and the casing.