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:
Apr. 12, 2016

Filed:

Sep. 11, 2012
Applicants:

Sanji Ekanayake, Mableton, GA (US);

Alston Ilford Scipio, Mableton, GA (US);

Raymond Henry Goetze, Simpsonville, SC (US);

Peter Samuel King, Greenville, SC (US);

Douglas Corbin Warwick, Ball Ground, GA (US);

Inventors:

Sanji Ekanayake, Mableton, GA (US);

Alston Ilford Scipio, Mableton, GA (US);

Raymond Henry Goetze, Simpsonville, SC (US);

Peter Samuel King, Greenville, SC (US);

Douglas Corbin Warwick, Ball Ground, GA (US);

Assignee:

General Electric Company, Schenctady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 11/08 (2006.01); F01D 11/12 (2006.01); B23P 6/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); B23P 6/005 (2013.01); F01D 11/12 (2013.01); Y10T 29/49238 (2015.01);
Abstract

An assembly and method are provided for sealing a compressor in a gas turbine engine. The method comprises forming an annular groove in a compressor casing such that the groove extends circumferentially about a rotor that is housed within the casing. The compressor casing is then coupled to the rotor such that the compressor casing extends circumferentially about the rotor. A plurality of arcuate seal segments are then inserted into the annular groove without removing the rotor from the compressor casing such that the plurality of seal segments extend circumferentially about the rotor to facilitate sealing a gap that is defined between the rotor and the compressor casing.


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