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:
May. 19, 2015

Filed:

Jun. 15, 2012
Applicants:

Sheo Narain Giri, Karnataka, IN;

Harish Bommanakatte, Karnataka, IN;

Mohankumar Banakar, Karnataka, IN;

John David Ward, Jr., Woodruff, SC (US);

Jonathan Matthew Lomas, Simpsonville, SC (US);

Inventors:

Sheo Narain Giri, Karnataka, IN;

Harish Bommanakatte, Karnataka, IN;

Mohankumar Banakar, Karnataka, IN;

John David Ward, Jr., Woodruff, SC (US);

Jonathan Matthew Lomas, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/143 (2013.01); F01D 5/147 (2013.01); F05D 2240/80 (2013.01);
Abstract

A rotating airfoil component of a turbomachine, in which the component has an airfoil aligned in a spanwise direction of the component, a shank, and a platform therebetween oriented transverse to the spanwise direction. The platform has an outer radial surface adjacent the airfoil, and at least one recessed region defined in its outer radial surface. The recessed region extends opposite the spanwise direction from a platform plane that contains portions of the outer radial surface that are upstream and downstream from the recessed region. The recessed region is contiguous with an end wall of the platform and extends therefrom toward the airfoil. The recessed region defines a surface shape whose boundary is contained by the platform plane, and has a profile shape that extends from the end wall toward the airfoil. The recessed region is sized and shaped to increase the stiffness of the platform.


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