Turbine blade with chamfered squealer tip and convective cooling holes

• US 8,684,691 B2
• Filed: 05/03/2011
• Issued: 04/01/2014
• Est. Priority Date: 05/03/2011
• Status: Active Grant

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Energy Incorporated (Siemens AG)
• Inventors: Lee, Ching-Pang, Mhetras, Shantanu P., Brown, Glenn E.
• Primary Examiner(s): EDGAR, RICHARD A
• Application Number:
  US13/099,521
• Publication Number:
  US 20120282108A1
• Time in Patent Office: 1,064 Days
• Field of Search: 416/224, 416/92, 416/90.R, 416/228
• US Class Current: 416/92
• CPC Class Codes: F01D 5/20 Specially-shaped blade tips to seal space between tips and stator F01D5/225 takes precedence

Abstract

A squealer tip formed from a pressure side rib and a suction side rib extending radially outward from a tip of the turbine blade is disclosed. The pressure and suction side ribs may be positioned along the pressure side and the suction side of the turbine blade, respectively. The pressure and suction side ribs may include chamfered leading edges with film cooling holes having exhaust outlets positioned therein. The film cooling holes may be configured to be diffusion cooling holes with one or more tapered sections for reducing the velocity of cooling fluids and increasing the size of the convective surfaces.

Claims

1. A turbine blade, comprising:

a generally elongated blade having a leading edge, a trailing edge, a tip at a first end, a root coupled to the blade at a second end generally opposite the first end for supporting the blade and for coupling the blade to a disc, and an internal cooling system formed from at least one cavity positioned within the generally elongated blade; and

at least one pressure side rib extending radially from an outer surface of the tip, wherein the at least one pressure side rib includes a chamfered surface positioned at an acute angle relative to an outer surface of the generally elongated blade forming a pressure side;

at least one film cooling hole positioned in the at least one pressure side rib with an outlet in an outer surface in the at least one pressure side rib and an inlet that couples the at least one film cooling hole with the at least one cavity forming the internal cooling system

wherein the outlet of the at least one film cooling hole is positioned in the chamfered surface of the at least one pressure side rib;

wherein the at least one film cooling hole in the chamfered surface of the at least one pressure side rib is formed from a compound diffuser film cooling hole having at least one tapered section with an increasing cross-sectional area;

at least one suction side rib extending radially from an outer surface of the tip, wherein the at least one suction side rib includes a chamfered surface positioned at an acute angle relative to an outer surface of the tip of the generally elongated blade;

at least one film cooling hole positioned in the at least one suction side rib with an outlet in an outer surface in the at least one suction side rib and an inlet that couples the at least one film cooling hole with the at least one cavity forming the internal cooling system;

wherein the at least one pressure side rib and the at least one suction side rib are separated by a linear tip surface in which a plurality of outlets of film cooling holes reside.

2. The turbine blade of claim 1, wherein the chamfered surface of the at least one pressure side rib only extends for a portion of an entire length of the at least one pressure side rib.

3. The turbine blade of claim 1, wherein the at least one pressure side rib extends from the leading edge and terminates at the trailing edge.

4. The turbine blade of claim 1, wherein the at least one pressure side rib has an outer side surface that is aligned with the outer surface of the generally elongated blade forming the pressure side.

5. The turbine blade of claim 1, wherein the chamfered surface of the at least one suction side rib extends for a portion of an entire length of the at least one suction side rib.

6. The turbine blade of claim 1, wherein the at least one suction side rib has an outer side surface that is aligned with an outer surface of the generally elongated blade forming a suction side.

7. The turbine blade of claim 6, wherein the at least one suction side rib extends from the trailing edge toward the leading edge of the generally elongated blade, terminates at the leading edge and is coupled to the at least one pressure side rib.

8. The turbine blade of claim 7, wherein the at least one pressure side rib and the at least one suction side rib are separated by a tip slot positioned at the trailing edge.

9. The turbine blade of claim 1, wherein the outlet of the at least one film cooling hole is positioned in the chamfered surface of the at least one suction side rib.

10. The turbine blade of claim 9, wherein the at least one film cooling hole is formed from a compound diffuser film cooling hole having at least one tapered section having an increasing cross-sectional area moving downstream.

11. The turbine blade of claim 1, further comprising a thermal barrier coating on the outer surfaces forming the pressure and suction sides, on chamfered surfaces of the pressure and suction side ribs, on the outer surface of the tip and on an interior surface of the at least one pressure side rib.

12. The turbine blade of claim 1, wherein the at least one pressure side rib has a height to width ratio of between 2:

1 and 1;

2.

13. The turbine blade of claim 1, wherein the at least one suction side rib has a height to width ratio of between 2:

1 and 1;

2.

14. A turbine blade, comprising:

a generally elongated blade having a leading edge, a trailing edge, a tip at a first end, and a root coupled to the blade at a second end generally opposite the first end for supporting the blade and for coupling the blade to a disc, an internal cooling system formed from at least one cavity positioned within the generally elongated blade; and

at least one pressure side rib extending radially from an outer surface of the tip, wherein the at least one pressure side rib includes a chamfered surface positioned at an acute angle relative to an outer surface of the generally elongated blade forming a pressure side;

wherein the chamfered surface of the at least one pressure side rib extends for a portion of an entire length of the at least one pressure side rib;

wherein the at least one pressure side rib extends from the leading edge and terminates at the trailing edge;

wherein the at least one pressure side rib has an outer side surface that is aligned with the outer surface of the generally elongated blade forming the pressure side;

at least one suction side rib extending radially from an outer surface of the tip, wherein the at least one suction side rib includes a chamfered surface positioned at an acute angle relative to an outer surface of the tip of the generally elongated blade;

wherein the chamfered surface of the at least one suction side rib only extends for a portion of an entire length of the at least one suction side rib;

wherein the at least one suction side rib has an outer side surface that is aligned with an outer surface of the generally elongated blade forming a suction side;

wherein the at least one suction side rib extends from the trailing edge toward the leading edge of the generally elongated blade, terminates at the leading edge and is coupled to the pressure side rib;

wherein the at least one pressure side rib and the at least one suction side rib are separated by a linear tip surface;

wherein the at least one pressure side rib has a height to width ratio of between 2;

1 and 1;

2 and the at least one suction side rib has a height to width ratio of between 2;

1 and 1;

2.

15. The turbine blade of claim 14, further comprising at least one film cooling hole positioned in the at least one pressure side rib with an outlet in an outer surface in the at least one pressure side rib and an inlet that couples the at least one film cooling hole with the at least one cavity forming the internal cooling system.

16. The turbine blade of claim 15, wherein the outlet of the at least one film cooling hole is positioned in the chamfered surface of the at least one pressure side rib and wherein the at least one film cooling hole is formed from a compound diffuser film cooling hole having at least one tapered section with an increasing cross-sectional area.

17. The turbine blade of claim 14, further comprising at least one film cooling hole positioned in the at least one suction side rib with an outlet in an outer surface in the at least one suction side rib and an inlet that couples the at least one film cooling hole with the at least one cavity forming the internal cooling system, wherein the outlet of the at least one film cooling hole is positioned in the chamfered surface of the at least one suction side rib, and wherein the at least one film cooling hole is formed from a compound diffuser film cooling hole having at least one tapered section having an increasing cross-sectional area moving downstream.

18. The turbine blade of claim 14, wherein the at least one pressure side rib and the at least one suction side rib are separated by a tip slot positioned at the trailing edge.

19. A turbine blade, comprising:

a generally elongated blade having a leading edge, a trailing edge, a tip at a first end, a root coupled to the blade at a second end generally opposite the first end for supporting the blade and for coupling the blade to a disc, and an internal cooling system formed from at least one cavity positioned within the generally elongated blade; and

at least one pressure side rib extending radially from an outer surface of the tip, wherein the at least one pressure side rib includes a chamfered surface positioned at an acute angle relative to an outer surface of the generally elongated blade forming a pressure side;

wherein the chamfered surface of the at least one pressure side rib extends for a portion of an entire length of the at least one pressure side rib;

wherein the at least one pressure side rib extends from the leading edge and terminates at the trailing edge;

wherein the at least one pressure side rib has an outer side surface that is aligned with the outer surface of the generally elongated blade forming the pressure side;

at least one suction side rib extending radially from an outer surface of the tip, wherein the at least one suction side rib includes a chamfered surface positioned at an acute angle relative to an outer surface of the tip of the generally elongated blade;

wherein the chamfered surface of the at least one suction side rib only extends for a portion of an entire length of the at least one suction side rib;

wherein the at least one suction side rib has an outer side surface that is aligned with an outer surface of the generally elongated blade forming a suction side;

wherein the at least one suction side rib extends from the trailing edge toward the leading edge of the generally elongated blade and terminates at the leading edge and is coupled to the pressure side rib;

at least one film cooling hole positioned in the at least one pressure side rib with an outlet in an outer surface in the at least one pressure side rib and an inlet that couples the at least one film cooling hole with the at least one cavity forming the internal cooling system;

wherein the outlet of the at least one film cooling hole is positioned in the chamfered surface of the at least one pressure side rib;

at least one film cooling hole positioned in the at least one suction side rib with an outlet in an outer surface in the at least one suction side rib and an inlet that couples the at least one film cooling hole with the at least one cavity forming the internal cooling system;

wherein the outlet of the at least one film cooling hole is positioned in the chamfered surface of the at least one suction side rib;

wherein the at least one pressure side rib and the at least one suction side rib are separated by a linear tip surface;

wherein the at least one pressure side rib and the at least one suction side rib are separated by a tip slot positioned at the trailing edge.

20. The turbine blade of claim 19, wherein the at least one pressure side rib has a height to width ratio of between 2:

1 and 1;

2 and wherein the at least one suction side rib has a height to width ratio of between 2;

1 and 1;

2.