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:
Oct. 30, 2018

Filed:

Jan. 08, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Ory Moniz, Loveland, OH (US);

Joseph George Rose, Mason, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/08 (2006.01); F04D 29/42 (2006.01); F04D 17/02 (2006.01); F04D 27/02 (2006.01); F04D 29/16 (2006.01); F02C 9/16 (2006.01);
U.S. Cl.
CPC ...
F04D 29/4206 (2013.01); F02C 9/16 (2013.01); F04D 17/025 (2013.01); F04D 27/0246 (2013.01); F04D 29/162 (2013.01); F05B 2220/302 (2013.01); F05B 2230/60 (2013.01);
Abstract

A centrifugal compressor assembly for use in a turbine engine is provided. The assembly includes an impeller that includes a plurality of rotor blades. The assembly also includes a stationary assembly circumscribing the impeller such that a clearance is defined therebetween. The stationary assembly includes at least one articulating seal member positioned adjacent the plurality of rotor blades, and a biasing mechanism configured to cause the at least one articulating seal member to selectively translate relative to the plurality of rotor blades based on an operating condition of the turbine engine.


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