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:
Jan. 29, 2019

Filed:

Feb. 09, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Neil Ristau, Simpsonville, SC (US);

Zachary James Taylor, Greenville, SC (US);

David Wayne Weber, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/18 (2006.01); F01D 5/22 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/225 (2013.01); F01D 5/141 (2013.01); F01D 5/143 (2013.01); F01D 5/145 (2013.01); F05D 2220/32 (2013.01); F05D 2240/307 (2013.01); F05D 2250/74 (2013.01); Y02T 50/673 (2013.01);
Abstract

Various embodiments of the invention include turbine buckets and systems employing such buckets. Various particular embodiments include a turbine bucket having: an airfoil having: a suction side; a pressure side opposing the suction side; a leading edge spanning between the pressure side and the suction side; and a trailing edge opposing the leading edge and spanning between the pressure side and the suction side; a base connected with a first end of the airfoil along the suction side, pressure side, trailing edge and the leading edge; and a tip shroud connected with a second end of the airfoil along the suction side, pressure side, trailing edge and the leading edge, the tip shroud including a tip shroud fillet connecting the airfoil and the tip shroud and having a non-uniform thickness across an axial length of the airfoil.


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