Multiple piece turbine airfoil

• US 7,828,515 B1
• Filed: 05/19/2009
• Issued: 11/09/2010
• Est. Priority Date: 05/19/2009
• Status: Expired due to Fees

• Current Assignee: Florida Turbine Technologies, Inc. (Kratos Defense & Security Solutions Incorporated)
• Original Assignee: Florida Turbine Technologies, Inc. (Kratos Defense & Security Solutions Incorporated)
• Inventors: Kimmel, Keith D
• Primary Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US12/468,349
• Time in Patent Office: 539 Days
• Field of Search: 415/115, 415/116, 415/134, 415/136, 415/138, 416/96.R, 416/96.A, 416/97.R, 416/226
• US Class Current: 415/115
• CPC Class Codes: F01D 5/189 the insert having a tubular cross-section, e.g. airfoil shape
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A turbine airfoil, such as a rotor blade or a stator vane, for a gas turbine engine, the airfoil formed as a shell and spar construction with a plurality of hook shaped struts each mounted within channels extending in a spanwise direction of the spar and the shell to allow for relative motion between the spar and shell in the airfoil chordwise direction while also fanning a seal between adjacent cooling channels. The struts provide the seal as well as prevent bulging of the shell from the spar due to the cooling air pressure. The hook struts have a hooked shaped end and a rounded shaped end in order to insert the struts into the spar.

Claims

1. An air cooled turbine airfoil comprising:

a shell having an airfoil shape with a leading edge, a trailing edge, and a pressure side wall and a suction side wall extending between the leading edge and the trailing edge;

a spar forming an internal cooling air supply channel;

a plurality of rounded channels on an inner surface of the shell;

a plurality of hook shaped channels on an outer surface of the spar;

the shell channels and the spar channels being opposed to one another;

a hook shaped strut having a rounded end and a hook end;

a rounded end of the hook shaped strut being inserted into the rounded channel of the shell; and

,

the hook shaped end of the hook shaped strut being inserted into a hook shaped channel of the spar to retain the shell to the spar.

2. The air cooled turbine airfoil of claim 1, and further comprising:

the hook shaped strut forms a seal being adjacent cooling air channels formed between the spar and the shell.

3. The air cooled turbine airfoil of claim 1, and further comprising:

the rounded end of the hook shaped strut and the rounded channel on the shell allow for the hook shaped strut to pivot within the shell channel without being pulled out from the shell channel.

4. The air cooled turbine airfoil of claim 1, and further comprising:

the hook shaped struts are formed from a high temperature metallic material that can be extruded to form the hook shaped struts.

5. The air cooled turbine airfoil of claim 1, and further comprising:

the shell is formed from one of tungsten, molybdenum and columbium.

6. The air cooled turbine airfoil of claim 5, and further comprising:

the shell is a thin walled shell.

7. The air cooled turbine airfoil of claim 1, and further comprising:

the airfoil is a rotor blade for use in an industrial gas turbine engine.

8. The air cooled turbine airfoil of claim 1, and further comprising:

the airfoil is a stator vane for use in an industrial gas turbine engine.

9. The air cooled turbine airfoil of claim 1, and further comprising:

the rounded channel and the hook shaped channel extend substantially along an entire airfoil spanwise direction.

10. The air cooled turbine airfoil of claim 1, and further comprising:

the hook end extends substantially perpendicular to a central axis passing through the rounded end and a middle section of the hook shaped strut.