Turbine exhaust case duct

1. An exhaust duct comprising:

a shroud body having a forward shroud end and an aft shroud end;

a forward flange assembly extending radially inward from the forward shroud end for securing the forward shroud end downstream of a final turbine stage;

an aft flange assembly extending circumferentially around and radially inward from the aft shroud end for securing the aft shroud end to an engine tail cone;

an intermediate flange assembly disposed forward of the aft flange assembly, and extending circumferentially around and radially inward from the shroud body for securing the shroud body to an engine bearing housing; and

a first plurality of bleed ports disposed on the shroud body forward of a junction with the intermediate flange assembly.

2. The exhaust duct of claim 1 , wherein the first plurality of bleed ports are circumferentially distributed equally around the shroud body.

3. The exhaust duct of claim 1 , wherein the first plurality of bleed ports include at least one hole disposed radially outward from at least one surface of the shroud body.

4. The exhaust duct of claim 3 , wherein the at least one hole is shaped to impinge exhaust gas flow onto the at least one surface of the intermediate flange assembly.

5. The exhaust duct of claim 4 , wherein the at least one surface of the intermediate flange assembly is an obtuse surface angled axially forward and radially inward from the shroud body.

6. The exhaust duct of claim 4 , wherein at least one of the first plurality of bleed ports further includes a scoop arranged over the at least one hole, the scoop having an opening for facing the direction of oncoming exhaust gas flow.

7. The exhaust duct of claim 1 , further comprising a second plurality of bleed ports circumferentially intermediate adjacent ones of the first plurality of bleed ports.

8. The exhaust duct of claim 1 , wherein the forward shroud end includes a plurality of circumferentially distributed strut cutouts, each strut cutout shaped to engage with an aft portion of a corresponding turbine exhaust case support strut.

9. The exhaust duct of claim 8 , wherein at least one of the plurality of circumferentially distributed strut cutouts includes a stiffener rib secured around a perimeter thereof.

10. The exhaust duct of claim 8 , wherein at least one of the first plurality of bleed ports is circumferentially aligned with a corresponding at least one of the plurality of circumferentially distributed strut cutouts.

11. The exhaust duct of claim 1 , further comprising a flange connector disposed radially inward of the shroud body, the connector joining the intermediate flange assembly and the aft flange assembly.

12. The exhaust duct of claim 11 , further comprising an outer stiffener ring disposed axially around the shroud body aft of the first plurality of bleed ports, and over the flange connector.

13. A turbine exhaust case (TEC) duct assembly comprising:

a forward TEC duct;

an aft TEC duct including a shroud body with a first plurality of bleed ports, an inwardly extending forward flange assembly securing a forward shroud end to the forward TEC duct, an inwardly extending aft flange assembly, and an inwardly extending intermediate flange assembly for securing the aft TEC duct to an engine bearing housing, the first plurality of bleed ports disposed on the shroud body forward of a junction with the intermediate flange assembly; and

an engine tail cone secured to the aft TEC duct at the aft flange assembly.

14. The assembly of claim 13 , wherein respective outer surfaces of the forward TEC duct shroud body, the aft TEC duct shroud body, and the engine tail cone cooperate to define an inner exhaust gas path boundary.

15. The assembly of claim 14 , wherein the forward TEC duct includes a first plurality of strut cutouts circumferentially distributed around an aft shroud end, and the aft TEC duct includes a second plurality of strut cutouts circumferentially distributed around the forward shroud end, and wherein respective ones of the first and second pluralities of shroud body strut cutouts cooperate to form passages through the inner exhaust gas path boundary for circumferentially distributed TEC struts operating as exhaust guide vanes.

16. The assembly of claim 13 , wherein the intermediate flange assembly extends circumferentially around and radially inward from the aft TEC duct shroud body, and at least one surface of the intermediate flange is an obtuse surface angled axially forward and radially inward from the shroud body.

17. The assembly of claim 16 , wherein the first plurality of bleed ports are circumferentially distributed equally around the shroud body and include at least one hole in the shroud body disposed radially outward of at least one surface of the intermediate flange assembly, the at least one hole shaped to impinge exhaust gas flow onto the at least one surface of the intermediate flange assembly.

18. The assembly of claim 17 , wherein at least one of the plurality of bleed ports further includes a scoop arranged over the at least one hole.

19. The assembly of claim 18 , wherein the scoop has an opening for facing the direction of oncoming exhaust gas flow.

20. The assembly of claim 13 , further comprising a flange connector disposed radially inward of the shroud body, the connector joining the intermediate flange assembly and the aft flange assembly.