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. 19, 2016

Filed:

Jan. 21, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Xiaoqing Zheng, Niskayuna, NY (US);

Jason Winfred Jewett, Clifton Park, NY (US);

Richard James Miller, Jr., Round Lake, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/02 (2006.01); F01D 11/04 (2006.01); F01D 11/00 (2006.01); F01D 11/08 (2006.01);
U.S. Cl.
CPC ...
F01D 11/04 (2013.01); F01D 11/001 (2013.01); F01D 11/08 (2013.01); F05D 2240/11 (2013.01); F05D 2240/80 (2013.01);
Abstract

Various embodiments include a turbomachine including a swirl-inhibiting seal. In various particular embodiments, a turbomachine includes: a rotor section having sets of axially disposed blades; a diaphragm section at least partially surrounding the rotor section, the diaphragm section including a set of nozzles positioned between adjacent sets of axially disposed blades, wherein the set of nozzles includes at least one nozzle having: a base section coupled to the diaphragm section; a blade coupled to the base section; and a radial tip section coupled to a radial end of the blade, the radial tip section including an axially extending flange having a slot extending therethrough for controlling fluid flow within the turbomachine.


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