Film-cooling augmentation device and turbine airfoil incorporating the same
A turbine airfoil is disclosed. The airfoil includes one of a turbine shroud, liner, vane or blade, including an airfoil sidewall having a film-cooling hole that extends between an airfoil cooling circuit and an airfoil surface. The airfoil also includes an insert disposed in the film-cooling channel having a body. The body has a proximal end configured for disposition proximate the airfoil surface and a distal end. The body is also configured to define a passageway that extends between the distal end and proximal end upon disposition in the film-cooling hole.
1. A turbine airfoil, comprising:
an airfoil sidewall having a film-cooling hole that extends between an airfoil cooling circuit and an airfoil surface; and
an insert disposed in the film-cooling hole having a body, the body having a proximal end configured for disposition proximate the airfoil surface and a distal end, the body also configured to define a passageway that extends between the distal end and proximal end upon disposition in the film-cooling hole.
2. The turbine airfoil of claim 1 , wherein the airfoil comprises a turbine blade or vane comprising a pressure sidewall and an opposing suction sidewall joined together at chordally opposite leading and trailing edges and extending longitudinally in span from a first end to a second end, the cooling circuit is disposed within the pressure sidewall or suction sidewall, and the film-cooling hole extends through one of pressure sidewall, suction sidewall, trailing edge or leading edge.
3. The turbine airfoil of claim 1 , wherein the insert comprises a plurality of passageways.
4. The turbine airfoil of claim 3 , wherein the insert comprises a sintered powder compact having a porous structure comprising a network of interconnected particles and a corresponding network of interconnected interstitial spaces, the interconnected interstitial spaces comprising the plurality of passageways.
5. The turbine airfoil of claim 1 , wherein the passageway has a central axis and the axis is non-linear.
6. The turbine airfoil of claim 5 , wherein the passageway is one of a stepped or an arcuate passageway.
7. The turbine airfoil of claim 1 , wherein the insert has a longitudinal axis and comprises a laterally extending protrusion exposed to the passageway.
8. The turbine airfoil of claim 3 , wherein the insert comprises a longitudinally extending rib, and wherein the passageway is defined by the rib.
9. The turbine airfoil of claim 1 , wherein the body comprises a generally tubular structure having an inner and an outer surface.
10. The turbine airfoil of claim 9 , wherein the passageways are defined along an inner or an outer surface of the generally tubular structure.
11. The turbine airfoil of claim 9 , wherein the passageways are defined by a protruding structure that protrudes from the inner surface or the outer surface of the generally tubular structure.
12. An insert for a film-cooling hole of a turbine airfoil, comprising a body that is configured for disposition in the film-cooling hole, the body having a proximal end configured for disposition proximate an airfoil surface and a distal end, the body also configured to define a passageway that extends between the distal end and proximal end upon disposition in the film-cooling hole.
13. The insert of claim 12 , wherein the body comprises a plurality of passageways.
14. The insert of claim 13 , wherein the body comprises a sintered powder compact having a porous structure comprising a network of interconnected particles and a corresponding network of interconnected interstitial spaces, the interconnected interstitial spaces comprising the plurality of passageways.
15. The insert of claim 12 , wherein the passageway has a central axis and the axis is non-linear.
16. The insert of claim 15 , wherein the passageway is one of a stepped or an arcuate passageway.
17. The insert of claim 12 , wherein the body comprises a longitudinally extending rib, and wherein the passageway is defined by the rib.
18. The insert of claim 12 , wherein the body comprises a generally tubular structure having an inner and an outer surface.
19. The insert of claim 12 , wherein the insert has a first melting point and the sidewall has a second melting point, and wherein the first melting point is less than the second melting point.
20. The insert of claim 13 , wherein the insert comprises a metal foam having a porous structure comprising an open cell foam network of interconnected, interstitial pores within a matrix metal, the interconnected, interstitial pores and open cell network comprising the plurality of passageways.