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Design Procedure and Performance Analysis of a Microturbine Combustor Working on Biogas for Power Generation

机译:沼气发电微型燃气轮机的设计程序和性能分析

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Design of the combustor is of high priority in microturbine generators (MTG) due to the small and compact configuration of these type of generators and high range of the shaft revolution (normally over 100k rpm). Design process of the MTG components including the micro combustor and turbomachinery also require accurate description of the combustion phenomena, heat transfer, emission level and performance analysis of the system. Design of combustors for renewable fuels such as biogas has several complications including overcoming the lower heating value of the biogas (normally 1/3 of the natural gas), combustion instabilities and corrosion effects of burning these types of fuels. The main benefit of burning a carbon neutral fuel (e.g., biogas), however will be in reducing the carbon emission by avoiding fossil fuels and achieving the environmental targets (e.g., Paris Agreement). The tubular combustors are in the centre of attention in design and operations of the microturbines due to their low cost and the level of emission. This research work presents the design procedure and CFD modelling of a tubular combustor for a biogas burnt microturbine engine assembly. The biogas is generated from anaerobic digestions of agriculture waste and include a 57% and 43% mixture of methane and CO_2 respectively. All the combustor parts are designed with empirical and practical equations and dimensions are optimised by CFD simulations. Operation of the combustor is then analysed in terms of its gaseous emissions. Finally, the operation of the new combustor in a closed heat and power cycle was verified and compared with conventional combustor of the microturbine burning diesel fuel, and as a result all the benefits and considerations for the application of biogas in microturbine assembly are carefully remarked and discussed.
机译:在微型涡轮发电机(MTG)中,燃烧器的设计具有较高的优先级,这是因为这类发电机的结构紧凑小巧,并且轴旋转范围大(通常超过100k rpm)。 MTG组件(包括微型燃烧器和涡轮机械)的设计过程还需要准确描述燃烧现象,传热,排放水平和系统性能分析。用于诸如沼气的可再生燃料的燃烧器的设计具有若干复杂性,包括克服沼气的较低的热值(通常为天然气的1/3),燃烧不稳定性以及燃烧这些类型的燃料的腐蚀效果。但是,燃烧碳中性燃料(例如沼气)的主要好处是通过避免使用化石燃料并实现环境目标(例如《巴黎协定》)来减少碳排放。由于微型涡轮机的低成本和排放水平,管状燃烧器成为微型涡轮机设计和操作的重点。这项研究工作介绍了沼气燃烧微型涡轮发动机总成的管状燃烧器的设计程序和CFD建模。沼气是由农业废弃物的厌氧消化产生的,分别包含57%和43%的甲烷和CO_2混合物。所有燃烧室部件均设计有经验公式和实用公式,并且尺寸通过CFD仿真进行了优化。然后根据燃烧器的气体排放量对其进行分析。最后,验证了新燃烧器在封闭的热电循环中的运行情况,并将其与微型燃气轮机燃烧柴油的传统燃烧器进行了比较,结果,仔细地记述了沼气在微型燃气轮机组件中应用的所有好处和考虑因素,讨论过。

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