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:
Jul. 02, 2019

Filed:

Feb. 20, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Omprakash Samudrala, Clifton Park, NY (US);

Fernando Jorge Casanova, Simpsonville, SC (US);

Edip Sevincer, Watervliet, NY (US);

Jonathan Michael Webster, Travelers Rest, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F01D 5/06 (2006.01); F01D 5/30 (2006.01); F01D 5/12 (2006.01); F01D 11/02 (2006.01);
U.S. Cl.
CPC ...
F01D 11/006 (2013.01); F01D 5/06 (2013.01); F01D 5/12 (2013.01); F01D 5/3007 (2013.01); F01D 11/001 (2013.01); F01D 11/005 (2013.01); F01D 11/02 (2013.01); F05D 2220/30 (2013.01); F05D 2230/60 (2013.01); F05D 2240/24 (2013.01); F05D 2240/55 (2013.01); F05D 2260/97 (2013.01);
Abstract

A sealing system for a multi-stage turbine includes multiple interstage seal segments disposed circumferentially about a turbine rotor wheel assembly and extending axially between a forward turbine stage and an aft turbine stage. Each of the interstage seal segments includes a forward end portion including an outer seal surface and an inner support face, an aft end portion, including an outer seal surface and an inner support face and a main body portion extending axially from the forward end portion to the aft end. The main body portion includes at least two support webs coupling the outer seal surfaces and the inner support faces. The outer seal surfaces are configured to be retained in a radial direction by a land support on each of a forward and aft stage turbine buckets, such that substantially all the centrifugal load from the multiple interstage seal segments is transferred to the forward and aft stage turbine buckets. A method of assembling the sealing system is disclosed.


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