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.

Patent No.:

US 7604456 B1

PDF
Full Text
Expired
Date of Patent:
Oct. 20, 2009

Filed:

Apr. 11, 2006
Applicants:

Anthony L. Schiavo, Jr., Oviedo, FL (US);

Bonnie D. Marini, Oviedo, FL (US);

Inventors:

Anthony L. Schiavo, Jr., Oviedo, FL (US);

Bonnie D. Marini, Oviedo, FL (US);

Assignee:

Siemens Energy, Inc., Orlando, FL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/40 (2006.01); F03B 11/02 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbine vane array () for a combustion assembly () in a combustion turbine engine. The vane array () includes a plurality of stationary vane assemblies (), each vane assembly () including at least one airfoil () and inner and outer shroud segments () attached to opposing ends of the airfoil (). The inner and outer shroud segments () each include an inner face () facing toward a gas path () extending through the vane array (). A removable cover structure may be provided on the inner faces () of the inner and outer shroud segments (). The cover structure may include removably attached insert elements () that are positioned on the inner faces () extending between upstream edges () and downstream edges () of the shroud segments () and extending between adjacent airfoils ().


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