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:
Oct. 04, 2016

Filed:

Oct. 25, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Kevin Weston McMahan, Greer, SC (US);

Carl Gerard Schott, Simpsonville, SC (US);

Clint Luigie Ingram, Simpsonville, SC (US);

Gunnar Leif Siden, Greenville, SC (US);

Sylvain Pierre, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 9/023 (2013.01); F01D 5/141 (2013.01); F05D 2240/122 (2013.01); F05D 2250/182 (2013.01); F05D 2250/183 (2013.01); F05D 2250/71 (2013.01);
Abstract

Transition duct assemblies for turbine systems and turbomachines are provided. In one embodiment, a transition duct assembly includes a plurality of transition ducts disposed in a generally annular array and comprising a first transition duct and a second transition duct. Each of the plurality of transition ducts includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of each transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct assembly further includes an aerodynamic structure defined by the passages of the first transition duct and the second transition duct. The aerodynamic structure includes a pressure side, a suction side, and a trailing edge, the trailing edge having a modified aerodynamic contour.


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