The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 06, 2007

Filed:

Sep. 09, 2005
Applicants:

Mark Edward Stegemiller, Franklin, OH (US);

Chander Prakash, Cincinnati, OH (US);

Leslie Eugene Leeke, Burlington, KY (US);

Kevin Samuel Klasing, Springboro, OH (US);

Ching-pang Lee, Cincinnati, OH (US);

Inventors:

Mark Edward Stegemiller, Franklin, OH (US);

Chander Prakash, Cincinnati, OH (US);

Leslie Eugene Leeke, Burlington, KY (US);

Kevin Samuel Klasing, Springboro, OH (US);

Ching-Pang Lee, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/20 (2006.01);
U.S. Cl.
CPC ...
Abstract

An airfoil for a gas turbine engine includes a root, a tip, a leading edge, a trailing edge, and opposed pressure and suction sidewalls extending generally along a radial axis. The airfoil includes a tip cap extending between the pressure and suction sidewalls; and spaced-apart suction-side and pressure-side tip walls extending radially outward from the tip cap to define a tip cavity therebetween. The pressure-side tip wall includes a continuously concave curved arcuate portion, at least a section of which extends circumferentially outward from a radial axis of the airfoil.


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