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:
Jun. 08, 2021

Filed:

Sep. 19, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nathan Evan McCurdy Gibson, West Chester, OH (US);

Darek Tomasz Zatorski, Fort Wright, KY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/10 (2006.01); F01D 5/03 (2006.01); F01D 11/06 (2006.01); F01D 5/22 (2006.01); F01D 25/24 (2006.01); F01D 1/26 (2006.01); F02C 3/067 (2006.01); F01D 11/14 (2006.01); F01D 11/16 (2006.01); F02K 3/072 (2006.01); F01D 11/02 (2006.01); F04D 29/54 (2006.01); F04D 27/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/06 (2013.01); F01D 1/26 (2013.01); F01D 5/03 (2013.01); F01D 5/225 (2013.01); F01D 11/025 (2013.01); F01D 11/14 (2013.01); F01D 11/16 (2013.01); F01D 25/24 (2013.01); F02C 3/067 (2013.01); F02K 3/072 (2013.01); F04D 27/009 (2013.01); F04D 29/545 (2013.01); F05D 2220/32 (2013.01); F05D 2240/24 (2013.01); F05D 2240/55 (2013.01); F05D 2260/52 (2013.01);
Abstract

The present disclosure is directed to a gas turbine engine including a turbine rotor, a turbine frame at least partially surrounding the turbine rotor, and an outer diameter seal assembly. The turbine rotor includes an inner shroud, an outer shroud, and at least one connecting airfoil coupling the inner shroud and the outer shroud. The outer shroud includes a plurality of outer shroud airfoils extended inward along a radial direction. The outer diameter seal assembly includes a sliding portion disposed between the turbine frame and the outer shroud of the turbine rotor. The outer diameter seal assembly defines a secondary tooth at the outer shroud radially inward of a longitudinal face of the sliding portion, and a primary tooth defined axially adjacent to a radial face of the sliding portion.


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