End wall contour for an axial flow turbine stage

Patent metadata

Field	Value
Publication number	US-10240462-B2
Application number	US-201615010145-A
Country	US
Kind code	B2
Filing date	Jan 29, 2016
Priority date	Jan 29, 2016
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

A turbine stage includes a row of airfoils joined to corresponding platforms to define flow passages therebetween. Each airfoil includes opposite pressure and suction sides and extends in chord between opposite leading and trailing edges. Each platform has a contoured flow surface including a purge valley, an elevated bulge and a bowl. The purge valley has a maximum depth at an elevation equal to or greater than a nominal axisymmetric platform surface of the corresponding platform. The purge valley extending tangentially against a purge cavity wall and into the blend area and extending axially from proximate the leading edge of a first airfoil toward the suction side of the first airfoil, and toward the leading edge of a second adjacent airfoil to channel a purge flow. The elevated bulge adjoins the pressure side aft of the leading edge and the bowl adjoins the suction side aft of the leading edge.

First claim

The invention claimed is:

1. A turbine stage comprising:
a row of airfoils integrally joined to corresponding platforms and spaced laterally apart to define respective flow passages therebetween for channeling gases, each flow passage having a width;
each of the airfoils including a concave pressure side and a laterally opposite convex suction side extending in chord between opposite leading and trailing edges; and
at least some of the platforms having a contoured flow surface including a purge valley having maximum depth at an elevation equal or greater than a nominal axisymmetric platform surface of the corresponding platform;
an elevated bulge extending along a portion of the airfoils and coupled to the at least some platforms, the elevated bulge adjoining the pressure side of each respective airfoil and having a maximum elevation at the airfoil pressure side surface;
an elevated region extending along a portion of the airfoils and coupled to the at least some platforms, the elevated region adjoining the suction side of each respective airfoil and having a maximum elevation at the airfoil suction side surface,
the purge valley formed between the elevated bulge and the elevated region and extending tangentially against a purge cavity wall and into a blend area and extending axially from proximate the leading edge of a first airfoil toward the suction side of the first airfoil, and toward the leading edge of a second adjacent airfoil to channel a purge flow.

2. The turbine stage according to claim 1 , wherein the purge valley is configured having a maximum depth laterally at a location −10% to 60% of the width of the flow passage formed between the leading edges of adjacent airfoils, wherein such measurement is measured commencing from the leading edge of the first airfoil extending laterally toward the convex suction side of the first airfoil and toward the leading edge of the second adjacent airfoil at the concave pressure side of the second adjacent airfoil.

3. The turbine stage according to claim 2 , wherein the purge valley is configured having a maximum depth laterally at a location substantially midway between the leading edges of adjacent airfoils.

4. The turbine stage according to claim 1 , wherein the purge valley is configured having a maximum depth axially at a location forward the leading edge of the airfoil.

5. The turbine stage according to claim 1 , wherein at least some platforms further include:
a bowl extending along a portion of the airfoils and coupled to the at least some platforms and having a maximum depth lower than a nominal axisymmetric platform surface of the corresponding platform, the bowl adjoining the purge valley, the elevated bulge and the suction side aft of the leading edge of each respective airfoil with the respective platforms,
the purge valley, the elevated bulge, the elevated region and the bowl form an arcuate channel extending axially along the platform between adjacent airfoils.

6. The turbine stage according to claim 5 , wherein at least some of the platforms include a trailing edge ridge structure extending along a portion of the airfoils and coupled to the at least some platforms, the trailing edge ridge structures adjoining at least one of the pressure side and the suction side at the trailing edge of each respective airfoil with the respective platforms.

7. The turbine stage according to claim 6 , wherein each of the trailing edge ridge structures adjoins the pressure side, the suction side, and the trailing edge of each respective airfoil with the respective platforms.

8. The turbine stage according to claim 5 , wherein the elevated bulge is centered at the pressure side aft of the leading edge, and decreases in height forward, aft, and laterally therefrom and the bowl is centered at the suction side commencing near the maximum thickness of the airfoils, and blends in a forward direction with the purge valley and the elevated bulge, and decreases in depth in an aft direction and laterally therefrom.

9. The turbine stage according to claim 5 , wherein the elevated bulge decreases in height in a forward direction, aft of the leading edge and decreases to the trailing edge and blends with the purge valley near the leading edge and with the bowl near the trailing edge.

10. The turbine stage according to claim 5 , wherein the purge valley is concave laterally, the elevated bulge is convex forward and aft and the bowl is concave laterally.

11. A turbine stage comprising:
a row of airfoils integrally joined to corresponding platforms and spaced laterally apart to define respective flow passages therebetween for channeling gases, each flow passage having a defined width;
each of the airfoils including a concave pressure side and a laterally opposite convex suction side extending in chord between opposite leading and trailing edges; and
at least some of the platforms having a contoured flow surface including a purge valley having maximum depth at an elevation equal or greater than a nominal axisymmetric platform surface of the corresponding platform, the purge valley extending tangentially against a purge cavity wall and into a blend area, an elevated bulge adjoining the pressure side aft of the leading edge of the respective airfoils and having a maximum elevation at the airfoil pressure side surface, an elevated region extending along a portion of the airfoils and coupled to the at least some platforms, the elevated region adjoining the suction side aft of the leading edge of each respective airfoil and having a maximum elevation at the airfoil suction side surface, and a bowl having a maximum depth lower than a nominal axisymmetric platform surface of the corresponding platform, the bowl adjoining the purge valley, the elevated bulge, the elevated region and the suction side aft of the leading edge of the respective airfoils,
the purge valley formed between the elevated bulge and the elevated region and extending axially from proximate the leading edge of a first airfoil toward the suction side of the first airfoil and laterally toward the leading edge of a second adjacent airfoil to channel a purge flow.

12. The turbine stage according to claim 11 , wherein at least some platforms having a trailing edge ridge structure extending along a portion of the airfoils and coupled to the at least some platforms, the trailing edge ridge structures adjoining at least one of the pressure side and the suction side at the trailing edge of each respective airfoil with the respective platforms.

13. The turbine stage according to claim 11 , wherein at least some platforms having a trailing edge ridge structure extending along a portion of the airfoils and coupled to the at least some platforms, the trailing edge ridge structures adjoining the pressure side and the suction side at the trailing edge of each respective airfoil with the respective platforms.

14. The turbine stage according to claim 11 , wherein the purge valley is configured having a maximum depth laterally at a location −10% to 60% of the width of the passage formed between the leading edges of adjacent airfoils, wherein such measurement is measured commencing from the leading edge of the first airfoil extending laterally toward the convex suction side of the first airfoil and toward the leading edge of the second adjacent airfoil at the concave pressure side of the second adjacent airfoil.

15. The turbine stage according to claim 11 , wherein the purge valley is configured having a maximum depth laterally at a location forward the leading edge of the airfoil.

16. The turbine stage according to claim 11 , wh

Assignees

• Gen Electric

Inventors

• Venugopal Prem
• Stein Alexander
• Otta Shourya Prakash
• Suresh Ambady

Classifications

• F05D2240/81

  Cooled platforms · CPC title

• F05D2240/24

  for turbines · CPC title

• F05D2250/711

  convex · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F01D5/145 Primary

  Means for influencing boundary layers or secondary circulations (for compressors F04D29/68) · CPC title