کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1731301 1521452 2016 12 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Numerical investigation of syngas oxy-combustion inside a LSCF-6428 oxygen transport membrane reactor
موضوعات مرتبط
مهندسی و علوم پایه مهندسی انرژی انرژی (عمومی)
پیش نمایش صفحه اول مقاله
Numerical investigation of syngas oxy-combustion inside a LSCF-6428 oxygen transport membrane reactor
چکیده انگلیسی


• Oxy-combustion of syngas inside a tubular-shaped oxygen transport reactor.
• Validations of oxygen permeation and syngas oxy-combustion reaction kinetics models.
• UDFs written in C++ are compiled to the software for oxygen transport across the ITM.
• Simulations were performed considering non-reactive and reactive flow conditions.
• Effects of temperature, CO2 circulation, fuel composition and sweep flux are studied.

The present work provides an investigation of the oxy-fuel combustion of syngas (mixture of CO and H2) inside an OTR (oxygen transport reactor) of tubular shape and surrounded by air in an annulus. The syngas is generated from solar thermal reforming of methane. CFD (Computational fluid dynamics) calculations were performed using FLUENT 14.0 commercial code, where a series of UDFs (user defined functions) that enable the transfer of oxygen across the membrane were written in VC++, then compiled and hooked to FLUENT software. The models of oxygen permeation and reaction kinetics are validated against the available experimental data under similar oxy-combustion conditions. Simulations were performed considering non-reactive and reactive flow conditions. The results showed that the reactive flow results in increase in oxygen permeation flux of about four times the case of non-reactive flow. Oxy-combustion characteristics of synthetic gas in a medium of recirculated CO2 are investigated. Considering reactive flow conditions, the effects of inlet temperature, CO2 circulation, fuel composition and sweep gas flux on oxygen permeation and combustion temperature are studied. It was found that increase in inlet temperature, inlet fuel concentration, inlet hydrogen concentration and sweep flow rate result in high combustion temperature and improved oxygen permeation flux.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Energy - Volume 96, 1 February 2016, Pages 654–665
نویسندگان
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