Crack arresting rotor blade

• US 5,902,093 A
• Filed: 08/22/1997
• Issued: 05/11/1999
• Est. Priority Date: 08/22/1997
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Freeman, Leston M. Jr., Manning, Robert F., Liotta, Gary C., Acquaviva, Paul J.
• Primary Examiner(s): Verdier, Christopher
• Assistant Examiner(s): NGUYEN, NINH H
• Application Number:
  US08/916,386
• Time in Patent Office: 627 Days
• Field of Search: 416/90 R, 416/92, 416/97 R, 415/115, 415/121.2, 415/169.1
• US Class Current: 416/97.00R
• CPC Class Codes: F01D 5/187 Convection cooling
• CPC Class Codes: F01D 5/20 Specially-shaped blade tips to seal space between tips and stator F01D5/225 takes precedence

Abstract

A rotor blade includes a dovetail and an airfoil joined thereto. The airfoil includes first and second spaced apart sides joined together laterally at opposite leading and trailing edges, and spanwise at a root and opposite tip. A serpentine cooling circuit extends inside the airfoil for channeling air therethrough for cooling the blade. The serpentine circuit includes first and second passes and a first bend therebetween for firstly receiving the cooling air in turn from the dovetail. A tip circuit is disposed between the tip and the serpentine circuit at the first bend for separating the tip from the first bend and providing cooling thereof near the trailing edge.

Claims

1. A turbine rotor blade comprising:

a dovetail for mounting said blade to a rotor disk;

an airfoil joined to said dovetail, and having spaced apart first and second sides joined together laterally at opposite leading and trailing edges and spanwise at a root and an opposite tip;

a serpentine cooling circuit extending spanwise inside said airfoil for channeling air therethrough for cooling said blade, said serpentine circuit having first and second passes and a first bend therebetween for firstly receiving said cooling air in turn from said dovetail; and

a tip circuit disposed between said tip and said serpentine circuit at said first bend, and solely between said second pass and said trailing edge, and having an inlet disposed in flow communication with said first bend for receiving a portion of said cooling air therefrom, and an outlet at said trailing edge for discharging said air therethrough for separating said tip from said first bend and providing cooling thereof near said trailing edge.

2. A blade according to claim 1 wherein said serpentine circuit further includes a third pass joined in flow communication with said second pass at a second bend therebetween, and extending to said tip forwardly of said tip circuit.

3. A blade according to claim 2 wherein said tip circuit inlet is sized to meter a portion of said air from said first bend to said tip circuit, with said second pass being joined to said first bend to receive a remainder of said air therefrom.

4. A blade according to claim 3 wherein said tip circuit inlet is sized to remove dust entrained with said air from said first bend, and said tip is characterized by the absence of dust holes disposed in flow communication with said tip circuit.

5. A blade according to claim 3 wherein said tip includes a plurality of cooling holes disposed in flow communication with said tip circuit along said airfoil first side for discharging said air in addition to said tip circuit outlet.

6. A blade according to claim 5 wherein said tip includes a squealer rib extending outwardly therefrom along said first and second sides between said leading and trailing edges, and said tip holes are aligned with said airfoil first side to effect cooling thereof.

7. A blade according to claim 3 wherein:

said serpentine circuit is defined by a plurality of legs extending between said root and tip; and

said airfoil further includes a tip septum spaced inwardly from said tip, and joined to a pair of said legs at said first bend.

8. A blade according to claim 7 wherein said serpentine circuit further includes a fourth pass disposed in flow communication with said third pass at a third bend therebetween, and a fifth pass disposed in flow communication with said fourth pass at a fourth bend therebetween, with said fourth and fifth passes being disposed between said leading edge and said tip circuit.

9. A blade according to claim 8 further comprising a trailing edge cooling circuit extending from said dovetail to said tip septum, and said tip circuit outlet is disposed at said trailing edge outwardly of said trailing edge cooling circuit.

10. A blade according to claim 9 wherein said trailing edge cooling circuit includes a plurality of outlets along said trailing edge aligned with said tip circuit outlet.

11. A blade according to claim 3 wherein said tip circuit includes a single inlet.

12. A blade according to claim 11 wherein said tip circuit inlet is disposed at a forwardmost end of said tip circuit.

13. A blade according to claim 7 wherein said septum is imperforate except for a single tip circuit inlet at a forwardmost end thereof.