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:
May. 18, 2010

Filed:

Sep. 29, 2006
Applicants:

Ryan Michael Urbassik, Cincinnati, OH (US);

Scott Anthony Estridge, Cincinnati, OH (US);

Rafael Ruiz, Liberty Township, OH (US);

Robert Proctor, West Chester, OH (US);

Robert J. Albers, Park Hills, KY (US);

Kevin Stephen Hansell, Okeana, OH (US);

Inventors:

Ryan Michael Urbassik, Cincinnati, OH (US);

Scott Anthony Estridge, Cincinnati, OH (US);

Rafael Ruiz, Liberty Township, OH (US);

Robert Proctor, West Chester, OH (US);

Robert J. Albers, Park Hills, KY (US);

Kevin Stephen Hansell, Okeana, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 31/00 (2006.01); F01D 11/24 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method for operating a gas turbine engine is provided. The gas turbine engine includes a fan, a high pressure turbine coupled downstream from the fan, and a low pressure turbine downstream from the high pressure turbine. The method includes channeling a portion of air discharged from the fan through a clearance control system including an inlet assembly that includes a plurality of louvers, and directing air from the inlet assembly into a first pipe and second pipe coupled to the inlet assembly such that pressure losses associated with the airflow are facilitated to be reduced.


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