Turbine airfoil for gas turbine engine

• US 6,551,062 B2
• Filed: 08/30/2001
• Issued: 04/22/2003
• Est. Priority Date: 08/30/2001
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: McRae, Ronald Eugene Jr., Keith, Sean Robert, Albrecht, Richard William Jr., Leeke, Leslie Eugene, Frey, David Alan
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): NGUYEN, NINH H
• Application Number:
  US09/943,526
• Publication Number:
  US 20030044275A1
• Time in Patent Office: 600 Days
• Field of Search: 415/115, 416/97.R, 416/96.R, 416/96.A
• US Class Current: 416/97.00R
• CPC Class Codes: F01D 5/186 Film cooling F01D5/187 takes precedence
• CPC Class Codes: F05D 2250/71 curved
• CPC Class Codes: F05D 2260/202 by film cooling
• CPC Class Codes: F05D 2260/94 Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
• CPC Class Codes: F05D 2260/941 particularly aimed at mechanical or thermal stress reduction
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A hollow cooled turbine airfoil is provided having pressure and suction side walls and a plurality of trailing edge cooling passages that feed cooling air bleed slots at the trailing edge. The suction side wall has a selectively reduced thickness, which allows shortened trailing edge slots, improving trailing edge cooling.

Claims

1. An airfoil having a leading edge and a trailing edge, comprising:

a pressure side wall extending from said leading edge to said trailing edge;

a suction side wall extending from said leading edge to said trailing edge;

an internal cavity;

a slot disposed in said pressure side wall adjacent said trailing edge; and

a passage disposed between said internal cavity and said slot, said passage having an inlet in fluid communication with said internal cavity and an exit in fluid communication with said slot, said passage being bounded by said pressure side wall and said suction side wall,

wherein said suction side wall has an inner surface and a varying thickness, wherein the value of said thickness at said inlet and said trailing edge is greater than said thickness near said exit, wherein said thickness is at a minimum aft of said exit.

2. An airfoil having a leading edge and a trailing edge, comprising:

a suction side wall extending from said leading edge to said trailing edge;

a pressure side wall extending from said leading edge to said trailing edge and having an aft-facing lip near an aft end thereof;

an internal cavity;

a slot disposed in said pressure side wall adjacent said trailing edge; and

a passage disposed between said internal cavity and said slot, said passage having an inlet in fluid communication with said internal cavity and an exit in fluid communication with said slot, said passage being bounded by said pressure side wall and said suction side wall,

wherein said suction side wall has a curved inner surface such that the distance between said lip and said trailing edge is minimized for a given thickness of said lip and a given width of said passage at said exit, wherein the thickness of said suction side wall at said inlet and said trailing edge is greater than the thickness of said suction side wall near said exit.

3. An airfoil having a leading edge and a trailing edge, comprising:

a suction side wall extending from said leading edge to said trailing edge;

a pressure side wall extending from said leading edge to said trailing edge and having an aft-facing lip near an aft end thereof;

an internal cavity;

a slot disposed in said pressure side wall adjacent said trailing edge; and

a passage disposed between said internal cavity and said slot, said passage having an inlet in fluid communication with said internal cavity and an exit in fluid communication with said slot, said passage being bounded by said pressure side wall and said suction side wall,

wherein said suction side wall has a curved inner surface such that the distance between said lip and said trailing edge is minimized for a given thickness of said lip and a given width of said passage at said exit, wherein said thickness of said suction side wall is at a minimum at said exit.

4. An airfoil having a leading edge and a trailing edge, comprising:

a suction side wall extending from said leading edge to said trailing edge;

a pressure side wall extending from said leading edge to said trailing edge and having an aft-facing lip near an aft end thereof;

an internal cavity;

a slot disposed in said pressure side wall adjacent said trailing edge; and

a passage disposed between said internal cavity and said slot, said passage having an inlet in fluid communication with said internal cavity and an exit in fluid communication with said slot, said passage being bounded by said pressure side wall and said suction side wall,

wherein said suction side wall has a curved inner surface such that the distance between said lip and said trailing edge is minimized for a given thickness of said lip and a given width of said passage at said exit, wherein said thickness of said suction side wall is at a minimum aft of said exit.

5. An airfoil having a leading edge and a trailing edge, comprising:

a suction side wall extending from said leading edge to said trailing edge;

a pressure side wall extending from said leading edge to said trailing edge and having an aft-facing lip near an aft end thereof;

an internal cavity;

a slot disposed in said pressure side wall adjacent said trailing edge; and

a passage disposed between said internal cavity and said slot, said passage having an inlet in fluid communication with said internal cavity and an exit in fluid communication with said slot, said passage being bounded by said pressure side wall and said suction side wall,

wherein said suction side wall has a curved inner surface such that the distance between said lip and said trailing edge is minimized for a given thickness of said lip and a given width of said passage at said exit, wherein said thickness of said suction side wall is at a minimum forward of said exit.