Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine
Abstract
Method and computer-readable model for additively manufacturing a ducting arrangement (10) for a gas turbine engine are provided. Ducting arrangement (10) may include a duct (18) to be fluidly coupled to receive a cross-flow of combustion gases from a main combustion stage. Duct (18) includes a duct segment (23) with an expanding cross-sectional area (24) where one or more injector assemblies (26) are disposed. Injector assembly (26) includes one or more reactant-guiding structures (27) arranged to deliver a flow of reactants to be mixed with the cross-flow of combustion gases. The ducting arrangement is effective 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.
- Inventors:
- Issue Date:
- Research Org.:
- Siemens Energy, Inc., Orlando, FL (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1524998
- Patent Number(s):
- 10215038
- Application Number:
- 15/165,210
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- Patent Classifications (CPCs):
-
B - PERFORMING OPERATIONS B33 - ADDITIVE MANUFACTURING TECHNOLOGY B33Y - ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- DOE Contract Number:
- FE0023968
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2016-05-26
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Chen, Yuntao, Portillo Bilbao, Juan Enrique, North, Andrew J., Tran, Lucky, Meadows, Joseph, and Laster, Walter Ray. Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine. United States: N. p., 2019.
Web.
Chen, Yuntao, Portillo Bilbao, Juan Enrique, North, Andrew J., Tran, Lucky, Meadows, Joseph, & Laster, Walter Ray. Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine. United States.
Chen, Yuntao, Portillo Bilbao, Juan Enrique, North, Andrew J., Tran, Lucky, Meadows, Joseph, and Laster, Walter Ray. Tue .
"Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine". United States. https://www.osti.gov/servlets/purl/1524998.
@article{osti_1524998,
title = {Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine},
author = {Chen, Yuntao and Portillo Bilbao, Juan Enrique and North, Andrew J. and Tran, Lucky and Meadows, Joseph and Laster, Walter Ray},
abstractNote = {Method and computer-readable model for additively manufacturing a ducting arrangement (10) for a gas turbine engine are provided. Ducting arrangement (10) may include a duct (18) to be fluidly coupled to receive a cross-flow of combustion gases from a main combustion stage. Duct (18) includes a duct segment (23) with an expanding cross-sectional area (24) where one or more injector assemblies (26) are disposed. Injector assembly (26) includes one or more reactant-guiding structures (27) arranged to deliver a flow of reactants to be mixed with the cross-flow of combustion gases. The ducting arrangement is effective 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.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {2}
}
Save to My Library
You must Sign In or Create an Account in order to save documents to your library.
Works referenced in this record:
Small diameter gas turbine engine
patent, May 1993
- Rodgers, Colin; Shekleton, Jack R.; Jones, Anthony C.
- US Patent Document 5,207,054
Combustion transition duct providing stage 1 tangential turning for turbine engines
patent, May 2010
- Bancalari, Eduardo; Wilson, Jody W.; Little, David A.
- US Patent Document 7,721,547
Forming structures from CAD solid models
patent, November 2004
- Keicher, David M.; Love, James W.; Dullea, Kevin J.
- US Patent Document 6,811,744
Assembly for directing combustion gas
patent, October 2012
- Charron, Richard C.; Nordlund, Raymond S.; Morrison, Jay A.
- US Patent Document 8,276,389
Method and apparatus for total energy systems
patent, September 1986
- Cirrito, Anthony
- US Patent Document 4,609,328
Trapped Vortex Fuel Injector and Method for Manufacture
patent-application, October 2015
- Melton, Patrick Benedict
- US Patent Application 14/247,533; 2015/0285504 Al
Combustor assembly in a gas turbine engine
patent, February 2013
- Wiebe, David J.; Fox, Timothy A.
- US Patent Document 8,375,726
Air/fuel supply system for use in a gas turbine engine
patent, June 2014
- Fox, Timothy A.; Schilp, Reinhard; Gambacorta, Domenico
- US Patent Document 8,752,386
Gas turbine engine combustion chamber
patent, December 1995
- Oag, Keith; Willis, Jeffrey David; Knocker, Alan
- US Patent Document 5,475,979
Late lean injection with adjustable air splits
patent, February 2012
- Davis, Jr., Lewis Berkley; Venkataraman, Krishna Kumar; Ziminsky, Willy Steve
- US Patent Document 8,112,216
Fuel nozzle
patent, November 2015
- McMasters, Marie Ann; Lohmueller, Steven Joseph; Boehm, Randall Charles
- US Patent Document 9,188,341