Turbine blades

• US 8,137,069 B2
• Filed: 12/15/2009
• Issued: 03/20/2012
• Est. Priority Date: 06/15/2007
• Status: Active Grant

• Current Assignee: Ansaldo Energia Switzerland AG (Ansaldo Energia SPA)
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: Khanin, Alexander, Sloutski, Edouard, Morozov, Andrey
• Primary Examiner(s): Look, Edward
• Assistant Examiner(s): ELLIS, RYAN H
• Application Number:
  US12/638,580
• Publication Number:
  US 20100158701A1
• Time in Patent Office: 826 Days
• Field of Search: 415/115, 416/96.R, 416/97.R, 416/96.A, 416/224
• US Class Current: 416/97.R
• CPC Class Codes: F01D 5/147 Construction, i.e. structural features, e.g. of weight-saving hollow blades F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18
• CPC Class Codes: F01D 5/187 Convection cooling
• CPC Class Codes: F05D 2230/21 by casting
• CPC Class Codes: F05D 2250/185 serpentine-like
• CPC Class Codes: Y10T 29/49336 Blade making
• CPC Class Codes: Y10T 29/49988 Metal casting

Abstract

A cast turbine blade is disclosed and includes an internal cooling passage that passes (e.g., zig-zags or meanders) through the blade from an inlet in the blade root to an outlet in the blade tip. The cooling passage can have a zone at a bend that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured around the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line. During casting of the blade, the cooling passage can be defined by a core or cores having a leachable material, the cores being removed after casting by a chemical leaching process. A supplementary passage is also provided for connecting the remote zone to the inlet during the leaching process. The supplementary passage can likewise be defined by a leachable core, or it may be machined into the blade after casting. During the service life of the blade, a plug can be used to obturate the supplementary passage to prevent leakage of cooling air from the cooling passage through the supplementary passage.

Claims

1. A cast turbine blade comprising:

a blade root and a blade tip;

at least one internal cooling passage that passes from an inlet in the blade root to an outlet in the blade tip, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the cooling passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line;

a supplementary passage that extends between the zone and the inlet through an internal wall of the cooling passage, wherein the supplementary passage is elongate and passes in a straight line from an aperture in an external surface of a base of the blade root, through the blade root, the inlet and the internal wall, to the zone; and

a plug which obturates the supplementary passage, wherein the plug is elongate and substantially co-extensive with the supplementary passage.

2. A cast turbine blade according to claim 1, wherein the zone of the cooling passage is at a bend in the cooling passage.

3. A cast turbine blade according to claim 1, wherein the plug is metallic, and comprises:

a shoulder for retaining the plug in a desired position in the supplementary passage to resist forces into the blade, the shoulder being configured to bear against a complementary feature in the supplementary passage.

4. A cast turbine blade according to claim 1, wherein the plug comprises:

an interference fit between the plug and the supplementary passage to retain the plug in position against forces tending to remove the plug from the blade.

5. A cast turbine blade according to claim 4, wherein the interference fit is configured as a deformation of a feature on the plug to make the plug project into a recess of the supplementary passage.

6. A cast turbine blade according to claim 5, wherein the feature on the plug is a collar and the recess comprises:

at least one of a wider part of the supplementary passage, and an undercut in a wall of the supplementary passage.

7. A cast turbine blade according to claim 1, comprising:

an abutment at an external end of the plug with a surface of the rotor to retain the plug in position against forces tending to remove it from the blade after assembly of the blade into a turbine rotor.

8. A method of manufacturing a turbine blade using the lost wax casting process, the method comprising:

casting a cooling passage that extends from an inlet in a root portion of the blade to an outlet in a tip portion of the blade, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line;

casting a supplementary passage for connecting the zone to the inlet during the manufacture of the blade, wherein the supplementary passage extends from an external surface of a base of the blade root, through the blade root, the inlet and an internal wall defining the cooling passage, to the zone, and wherein the cooling passage and the supplementary passage are defined by at least one core comprising a leachable material; and

obturating the supplementary passage after removal of the core material by inserting a metallic plug into the supplementary passage to prevent leakage of cooling air through the supplemental passage, from the zone into the inlet, and leakage of cooling air through supplemental passage blade root portion from the inlet to an exterior.

9. The method of claim 8, comprising:

leaching the core material from the cooling passage, but removing the core material from the supplementary passage before the core material is leached from the remote zone.

10. The method of claim 9, wherein the removing of the core material from the supplementary passage is performed by a leaching process.

11. The method of claim 9, wherein the removing of the core material from the supplementary passage is performed by a mechanical process.

12. The method of claim 8, comprising:

configuring the supplementary passage to facilitate efficient leaching of core material from the zone of the cooling passage.

13. A method of manufacturing a turbine blade using the lost wax casting process, the method comprising:

casting a cooling passage that extends from an inlet in a root portion of the blade to an outlet in a tip portion of the blade, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line;

machining a supplementary passage for connecting the zone to the inlet during the manufacture of the blade, wherein the supplementary passage extends from an external surface of a base of the blade root, through the blade root, the inlet and an internal wall defining the cooling passage, to the zone, and wherein the cooling passage and the supplementary passage are defined by at least one core comprising a leachable material; and

obturating the supplementary passage after removal of the core material by inserting a metallic plug into the supplementary passage to prevent leakage of cooling air through the supplemental passage, from the zone into the inlet, and leakage of cooling air through supplemental passage blade root portion from the inlet to an exterior.