Volume 1: Turbo Expo 2004 2004
DOI: 10.1115/gt2004-54011
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Integrated Process for CFD Modeling and Optimization of Gas Turbine Combustors

Abstract: Honeywell Engines, Systems & Services has developed the Advanced Combustion Tool (ACT) CFD process to rapidly analyze the performance of a combustor configuration from a given fuel injector, CAD geometry and engine cycle information. ACT integrates and streamlines the traditional steps of generating and specifying geometry, mesh, physical models, boundary conditions, initial conditions, convergence criteria and post-processing. Notably, ACT utilizes several key features to reduce cycle time and improve fid… Show more

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Cited by 9 publications
(5 citation statements)
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“…Additionally, some penalty-function constraints were assigned regarding the maximum values for the emissions of CO, CH 4 and NO (less than 10, 0.01 and 250 ppmvd @ 15% O 2 , respectively), plus a roof for the pressure losses (less than 7%). The limits have been chosen on the basis of indications given in [13].…”
Section: The Baseline Design Optimizationmentioning
confidence: 99%
See 1 more Smart Citation
“…Additionally, some penalty-function constraints were assigned regarding the maximum values for the emissions of CO, CH 4 and NO (less than 10, 0.01 and 250 ppmvd @ 15% O 2 , respectively), plus a roof for the pressure losses (less than 7%). The limits have been chosen on the basis of indications given in [13].…”
Section: The Baseline Design Optimizationmentioning
confidence: 99%
“…In [2] an algorithm is presented to produce the global layout of combustion chambers for aircraft application, based on generic relations between combustor overall performance and geometry. In [3,4] the general structure of the Honeywell analysis procedure named Advanced Combustion Tool (ACT) is presented. It is based on CAD, CFD and pre and post-processing tools and allows the integrated modeling and design refinement of gas turbine combustor.…”
Section: Introductionmentioning
confidence: 99%
“…For this purpose, several procedures have been developed for the sole combustion system. Honeywell Engines & Systems started implementing the Advanced Combustion Tool in 1998, an integrated process for rapidly analyzing and optimizing the combustor's aerodynamics from compressor deswirl to turbine stator inlet [1]. Rolls-Royce too supported the development of such methodologies.…”
Section: Introductionmentioning
confidence: 99%
“…Rudolph D. et al [8], developed the Advanced Combustion Tool (ACT) CFD process to rapidly analyze the performance of a gas turbine combustor from a given fuel injector, CAD geometry and engine cycle information.…”
Section: Introductionmentioning
confidence: 99%