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. 26, 2016

Filed:

Mar. 15, 2013
Applicants:

Richard C. Charron, West Palm Beach, FL (US);

William W. Pankey, Palm Beach Gardens, FL (US);

Inventors:

Richard C. Charron, West Palm Beach, FL (US);

William W. Pankey, Palm Beach Gardens, FL (US);

Assignee:

SIEMENS ENERGY, INC., Orlando, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); F01D 9/02 (2006.01); F23R 3/42 (2006.01);
U.S. Cl.
CPC ...
F02C 7/20 (2013.01); F01D 9/023 (2013.01); F23R 3/425 (2013.01); F05D 2250/25 (2013.01);
Abstract

An exit piece () with an inlet throat () that conducts a combustion gas flow (A) in a path () from a combustor () to an annular chamber () that feeds the first blade section () of a gas turbine (). The exit piece further includes an outlet portion () that forms a circumferential segment of the annular chamber. The outlet portion interconnects with adjacent outlet portions by hinges (A,B,A,B). Each hinge may have a hinge axis (A,B) parallel to a centerline () of the turbine. Respective gas flows (A) are configured by an assembly () of the exit pieces to converge on the feed chamber () into a uniform helical flow that drives the first blade section with minimal circumferential variations in force.


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