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. 21, 2021

Filed:

Aug. 07, 2019
Applicants:

General Electric Company, Schenectady, NY (US);

GE Avio S.r.l., Rivalta di Torino, IT;

Inventors:

Francesco Bertini, Frossasco, IT;

Aspi Rustom Wadia, Loveland, OH (US);

Lyle D. Dailey, Maineville, OH (US);

Andrea Arnone, Florenece, IT;

Filippo Rubechini, Florence, IT;

Matteo Giovannini, Pratovecchio, IT;

Paul Hadley Vitt, Liberty Township, OH (US);

Jeffrey Donald Clements, Mason, OH (US);

Assignees:

General Electric Company, Schenectady, NY (US);

GE Avio S.r.l., Rivolta di Torino, IT;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/147 (2013.01); F01D 5/145 (2013.01); F05D 2240/122 (2013.01); F05D 2240/128 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2250/712 (2013.01);
Abstract

A turbomachinery apparatus includes: a turbine, including: a turbine component defining an arcuate flowpath surface; an array of axial-flow turbine airfoils extending from the flowpath surface, the turbine airfoils defining spaces therebetween; and a plurality of fences extending from the flowpath surface, in the spaces between the turbine airfoils, each fence having opposed concave and convex sides extending between a leading edge and a trailing edge, wherein the fences have a nonzero camber and a constant thickness, are axially located near the leading edges of adjacent turbine airfoils, and wherein at least one of a chord dimension of the fences and a span dimension of the fences is less than the corresponding dimension of the turbine airfoils.


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