实现零碳排放:研究使用 H2/Air 和 NH3/Air 混合物的异型微型燃烧器的燃烧性能

IF 2.1 3区 工程技术 Q2 ENGINEERING, AEROSPACE Aerospace Pub Date : 2023-12-22 DOI:10.3390/aerospace11010012
Giacomo Cinieri, Zubair Ali Shah, Guido Marseglia, M. D. De Giorgi
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引用次数: 0

摘要

由于微机电和微型发电设备对高性能系统的需求,微燃烧器领域的研究工作最近有所增加。为了解决人们日益关注的化石源污染物问题,氢气(H2)和氨气(NH3)等零碳燃料已被视为微燃烧过程中的替代燃料。与传统燃烧系统相比,微型燃烧器的表面积与体积比要高得多,因此传热速度更快,燃烧反应更剧烈。然而,由于微燃烧器体积小,在微燃烧器中实现燃料和氧化剂的高效混合具有挑战性,特别是对于 H2 等高活性燃料。对于 NH3,微燃烧面临的挑战包括低活性、高点火温度(923 K,而 H2 为 793 K)和高浓度氮氧化物燃烧产物。因此,研究这些燃料在微型燃烧器中的性能对于开发清洁能源技术非常重要。本文对 Y 型微型燃烧器进行了 Ansys Fluent 数值研究,以探索 NH3/空气和 H2/空气在微型燃烧器中的非预混合燃烧特性。结果表明,对于使用 H2 的燃烧,即使在较低的当量比下也能实现静止火焰。此外,H2 在火焰中产生的污染物通常是 NH3 的两倍。在 NH3 条件下,微型燃烧器的整体效率是 H2 条件下的两倍。
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Toward Zero Carbon Emissions: Investigating the Combustion Performance of Shaped Microcombustors Using H2/Air and NH3/Air Mixtures
The research effort in the microcombustor field has recently increased due to the demand for high-performance systems in microelectromechanical and micro power generation devices. To address rising concerns about pollutants from fossil sources, zero-carbon fuels such as hydrogen (H2) and ammonia (NH3) have been considered as an alternative in microcombustion processes. In a microcombustor, the surface area-to-volume ratio is much higher compared to conventional combustion systems, resulting in faster heat transfer rates and more intense combustion reactions. However, achieving efficient mixing of fuel and an oxidizer in a microcombustor can be challenging due to its small size, particularly for highly reactive fuels like H2. For NH3, challenges in microcombustion involve a low reactive, high ignition temperature (923 K vs. 793 K of H2) and high concentration of NOx combustion products. Therefore, studying the performance of these fuels in microcombustors is important for developing clean energy technologies. In this paper, to explore features of non-premixed NH3/air and H2/air combustion in micro-scale combustors, an Ansys Fluent numerical investigation was conducted on a Y-shaped microcombustor. Results show that for combustion with H2, stationary flames can be achieved even at lower equivalence ratios. Additionally, the pollutants generated from H2 in the flame are generally twice those of NH3. The overall efficiency of the microcombustor is two times greater for NH3 conditions than for H2 conditions.
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来源期刊
Aerospace
Aerospace ENGINEERING, AEROSPACE-
CiteScore
3.40
自引率
23.10%
发文量
661
审稿时长
6 weeks
期刊介绍: Aerospace is a multidisciplinary science inviting submissions on, but not limited to, the following subject areas: aerodynamics computational fluid dynamics fluid-structure interaction flight mechanics plasmas research instrumentation test facilities environment material science structural analysis thermophysics and heat transfer thermal-structure interaction aeroacoustics optics electromagnetism and radar propulsion power generation and conversion fuels and propellants combustion multidisciplinary design optimization software engineering data analysis signal and image processing artificial intelligence aerospace vehicles'' operation, control and maintenance risk and reliability human factors human-automation interaction airline operations and management air traffic management airport design meteorology space exploration multi-physics interaction.
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