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:
Mar. 05, 2019

Filed:

May. 26, 2016
Applicant:

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

Inventors:

Yuntao Chen, Oviedo, FL (US);

Juan Enrique Portillo Bilbao, Oviedo, FL (US);

Andrew J. North, Orlando, FL (US);

Lucky Tran, Orlando, FL (US);

Joseph Meadows, Charlotte, NC (US);

Walter Ray Laster, Oviedo, FL (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/34 (2006.01); F23R 3/28 (2006.01); F23R 3/10 (2006.01); F23R 3/06 (2006.01); F23R 3/20 (2006.01); F23R 3/00 (2006.01); F23R 3/16 (2006.01); F23R 3/42 (2006.01); F02C 6/00 (2006.01); F02C 7/22 (2006.01); F23R 3/04 (2006.01); F23R 3/18 (2006.01); F23R 3/02 (2006.01);
U.S. Cl.
CPC ...
F23R 3/346 (2013.01); F02C 6/003 (2013.01); F02C 7/222 (2013.01); F23R 3/002 (2013.01); F23R 3/02 (2013.01); F23R 3/04 (2013.01); F23R 3/045 (2013.01); F23R 3/06 (2013.01); F23R 3/10 (2013.01); F23R 3/16 (2013.01); F23R 3/18 (2013.01); F23R 3/20 (2013.01); F23R 3/286 (2013.01); F23R 3/34 (2013.01); F23R 3/42 (2013.01); F05D 2240/35 (2013.01); F23R 2900/03341 (2013.01);
Abstract

A ducting arrangement () in a combustion stage downstream of a main combustion stage of a gas turbine engine is provided. A duct () is fluidly coupled to receive a cross-flow of combustion gases from the main combustion stage. Duct () includes a duct segment () with an expanding cross-sectional area () where one or more injector assemblies () are disposed. Injector assembly () includes one or more reactant-guiding structures () arranged to deliver a flow of reactants into the downstream combustion stage to be mixed with the cross-flow of combustion gases. Disclosed injector assemblies are arranged in expanding cross-sectional area () to reduce total pressure loss while providing an effective level of mixing of the injected reactants with the passing cross-flow. Respective duct components or the entire ducting arrangement may be formed as a unitized structure, such as a single piece using a rapid manufacturing technology, such as 3D Printing/Additive Manufacturing (AM) technologies.


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