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:
Sep. 18, 2007

Filed:

Nov. 12, 2002
Applicants:

Aspi R. Wadia, Loveland, OH (US);

Rolf Hetico, Cincinnati, OH (US);

Robert Bruce Dickman, Cincinnati, OH (US);

Hsin-yi Yen, Fairfield, OH (US);

Peter Wood, Loveland, OH (US);

Inventors:

Aspi R. Wadia, Loveland, OH (US);

Rolf Hetico, Cincinnati, OH (US);

Robert Bruce Dickman, Cincinnati, OH (US);

Hsin-Yi Yen, Fairfield, OH (US);

Peter Wood, Loveland, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/10 (2006.01);
U.S. Cl.
CPC ...
Abstract

An airfoil for a gas turbine engine includes a leading edge, a trailing edge, a tip, a first side wall that extends in radial span between an airfoil root and the tip, wherein the first side wall defines a first side of said airfoil, and a second side wall connected to the first side wall at the leading edge and the trailing edge, wherein the second side wall extends in radial span between the airfoil root and the tip, such that the second side wall defines a second side of the airfoil. The airfoil also includes a rib extending outwardly from at least one of the first side wall and the second side wall, wherein the rib is configured to reduce airflow spillage past the tip.


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