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. 11, 2019

Filed:

May. 31, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jagata Laxmi Narasimharao, Karnataka, IN;

Thomas Ory Moniz, Loveland, OH (US);

Mohamed Musthafa Thoppil, Karnataka, IN;

Bhaskar Nanda Mondal, Karnataka, IN;

Atanu Saha, Karnataka, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/02 (2006.01); F01D 11/04 (2006.01); F01D 5/12 (2006.01); F01D 25/12 (2006.01); F01D 5/08 (2006.01); F01D 3/00 (2006.01); F01D 11/00 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F01D 11/04 (2013.01); F01D 5/082 (2013.01); F01D 5/085 (2013.01); F01D 5/12 (2013.01); F01D 11/02 (2013.01); F01D 25/12 (2013.01); F01D 3/00 (2013.01); F01D 11/001 (2013.01); F02C 7/28 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/55 (2013.01);
Abstract

A turbine assembly includes a rotor assembly including a shaft coupled to a plurality of rotor stages including a plurality of turbine blades. The shaft and the plurality of turbine blades define a wheelspace therein. The turbine assembly further includes a plurality of seals in series, at least one seal of the plurality of seals is coupled between a static support member and a respective rotor stage such that a plurality of turbine cavities in series are defined within the wheelspace. Each turbine cavity of the plurality of turbine cavities defined by the plurality of seals receives a pressurized fluid flow that applies an axially aft force to the respective rotor stage of the plurality of rotor stages that at least partially reduces net rotor thrust generated by the rotor assembly during operation, the pressurized fluid flow further provides turbine purge within the wheel space.


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