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. 07, 2005

Filed:

Jul. 26, 2002
Applicants:

Henry Calvin Anderson, Jr., West Chester, OH (US);

Frederick J. Zegarski, Cincinnati, OH (US);

James Edward Thompson, Middletown, OH (US);

Tod Kenneth Bosel, Cincinnati, OH (US);

Kurt Thomas Hildebrand, Cincinnati, OH (US);

Inventors:

Henry Calvin Anderson, Jr., West Chester, OH (US);

Frederick J. Zegarski, Cincinnati, OH (US);

James Edward Thompson, Middletown, OH (US);

Tod Kenneth Bosel, Cincinnati, OH (US);

Kurt Thomas Hildebrand, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D005/14 ;
U.S. Cl.
CPC ...
Abstract

A low pressure turbine casing has a conical annular shell circumscribed about a centerline. A forward flange depends from a forward end of the annular shell and a forward hook extends aftwardly from the forward flange. First and second rails having first and second hooks, respectively, extend aftwardly from the annular shell. First and second cooling holes extend through the first and second rails, respectively. Cooling air feed holes extend through the forward flange. The first and second cooling holes may be radially disposed through the first and second rails, respectively, with respect to the centerline or disposed through the first and second rails at an oblique angle with respect to the centerline. A low pressure turbine casing and shroud assembly further includes a first annular cavity in fluid flow communication with the first cooling holes and the second cooling holes. A second annular cavity is in fluid flow communication with the first and second cooling holes.


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