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:
Mar. 31, 2020

Filed:

Jul. 31, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Zachary James Taylor, Greenville, SC (US);

Lucas Seth Wedmore, Greenville, SC (US);

Hiteshkumar Rameshchandra Mistry, Bangalore, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 11/08 (2006.01); F01D 5/22 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/225 (2013.01); F01D 11/08 (2013.01); F05D 2220/32 (2013.01); F05D 2240/307 (2013.01); F05D 2260/202 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

A rotor blade () for a turbine of a gas turbine that includes an airfoil (). The airfoil may have a leading edge, a trailing edge, an outboard tip, and an inboard end where the airfoil attaches to a root configured to couple the turbine blade to a rotor disc. The airfoil () may include a tip shroud () at an outboard tip. The rotor blade may have a cooling configuration that includes: elongated cooling channels () for receiving and directing a coolant through the airfoil (); and branching passages () formed through the tip shroud (), each of which elongates between a connection with one of the cooling channels () and an outlet port () formed on a surface of the tip shroud (). The branching passages () may have a canted orientation relative the outboard surface of the tip shroud ().


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