精益气体照明喷嘴技术减少泰国湾的排放量

C. Carpenter
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引用次数: 0

摘要

本文由 JPT 技术编辑 Chris Carpenter 撰写,包含 SPE 216098 号论文 "彻底改变可持续性:该论文未经同行评审,作者是 PTTEP 的 Nunthachai Amarutanon、Boonyakorn Assavanives 和 Kantkanit Watanakun 等人。 在这篇完整的论文中,作者介绍了一种旨在帮助石油和天然气行业实现净零排放目标的超低热值(ELBTU)火炬尖技术。运营商开展了一个联合研发项目,通过设计该技术来解决高热值要求的限制。事实证明,原型可成功燃烧较低热值的火炬气,大大优于现有技术。 联合研发项目于 2018 年开始工作。所述技术的开发始于对贫气燃烧理论的文献调查。该项目包括原型设计、模拟和测试的多次迭代,通过各种参数调整来优化性能,同时全面考虑各种燃烧标准。通过计算流体动力学模拟对设计进行了研究,并进行了测试以确定其工作包络线。一系列原型测试证明了最终设计的性能和机械完整性。 该技术必须达到的要求和一般功能(详见完整论文)包括以下内容:- 保持火焰稳定 - 尽量减少回烧 - 尽量减少火焰下坠 - 确保机械完整性 ELBTU 火炬喷嘴的设计如图 1 所示,包括喷嘴周边排出物周围的辅助火和穿透火炬气体排出物的辐条。辅助火被设计成一个辅助气体燃烧器,用于输送辅助气体和辅助空气。喷射泵用于向辅助气体燃烧器提供辅助空气,从而将辅助空气的管路尺寸降至最低。在这种设计下,辅助气体和辅助空气混合均匀,燃烧稳定,并为燃烧气体提供热量。顶帽的引入可减轻风的影响,延缓环境空气的混合,并延长火炬气在高温下的停留时间。这些优点使辅助气体得以燃烧,随后燃烧自由基与火炬气混合,而不受风的影响。辅助火环和辐条这两个主要部件借鉴了经过几十年运行证明可靠的现有喷嘴设计。 原型试验通过改变火炬气低热值(LHV)、火炬气出口速度、辅助空气流量和辅助气体流量(与热量释放有关)来研究火炬喷嘴的性能,包括使用和不使用风力发电机,以及使用和不使用顶帽。风力发电机是测试设施的升级版。风力发电机在顶端产生了超过 32 公里/小时的横风。性能包络线是根据火焰特性的两个性能方面(稳定性和质量)的可接受工作点生成的。经过数百次测试后发现,ELBTU 烟嘴能够燃烧 LHV 低至 110 BTU/scf 的排放气体,火焰稳定性和火焰质量均可接受。机械完整性是确保 ELBTU 烟嘴使用寿命的关键因素,为确保机械完整性,在测试前后对原型的内部和外部部件进行了彻底检查。得出的结论是,该设计具有可接受的机械完整性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Lean Gas-Flare-Tip Technology Reduces Emissions in the Gulf of Thailand
This article, written by JPT Technology Editor Chris Carpenter, contains highlights of paper SPE 216098, “Revolutionizing Sustainability: Achieving Net-Zero Emissions With Lean Gas-Flare-Tip Technology Breakthrough in the Gulf of Thailand,” by Nunthachai Amarutanon, Boonyakorn Assavanives, and Kantkanit Watanakun, PTTEP, et al. The paper has not been peer reviewed. In the complete paper, the authors describe an extremely low-BTU (ELBTU) flare-tip technology designed to help the oil and gas industry achieve net-zero targets. The operator embarked on a joint research and development project to address the limitations of high-heating-value requirements by designing the technology. The prototype was proved to successfully combust lower-heating-value flare gas, significantly outperforming existing technologies. The joint research and development project began work in 2018. The development of the described technology began with a literature survey on lean-gas-combustion theory. The project included multiple iterations of prototype design, simulation, and testing, with various parameter adjustments to optimize performance while considering a thorough range of combustion criteria. The design was studied through computational fluid dynamics simulation and tested to determine its operating envelope. Confidence in the performance and mechanical integrity of the final design has been proved by a series of prototype tests. Requirements and general functions that had to be achieved by the technology, all of which are detailed in the complete paper, included the following: - Maintain flame stability - Minimize burnback - Minimize flame pulldown - Ensure mechanical integrity The design of the ELBTU flare tip, shown in Fig. 1, includes an assist fire around the tip-perimeter discharge and spokes that penetrate the flare-gas discharge. The assist fire is designed as a supplementary gas burner where assist gas and assist air are delivered. Jet pumps are used to supply assist air to the assist gas burner, minimizing the line size for the assist air. With this design, assist gas and assist air are well-mixed, producing stable combustion and providing heat to the flare gas. A top hat was introduced to mitigate wind impact, retard the mixing of ambient air, and increase the time the flare gas remains at elevated temperatures. These benefits allow combustion of the assist gas and subsequent mixing of combustion radicals with the flare gas without the involvement of wind. Two of the major components, the assist fire ring and the spokes, were borrowed from existing tip designs that have proved reliable over decades of operation. The prototype test investigated flare-tip performance by varying vent-gas low heating value (LHV), vent-gas exit velocity, assist-air flow rate, and assist-gas flow rate (related to heat release) with and without a wind generator and with and without the top hat. The wind generator was an upgrade to the test facility. The wind generator created a crosswind across the tip of over 32 km/h. The performance envelope was generated based on the acceptable operating points regarding two performance aspects of the flame characteristics (stability and quality). After hundreds of tests, it was found that the ELBTU flare tip was able to combust a vent gas having an LHV as low as 110 BTU/scf with acceptable flame stability and flame quality. To ensure mechanical integrity, a crucial factor to ensure that the ELBTU flare tip will have an acceptable service life, internal and external parts of the prototype were thoroughly investigated before and after testing. It was concluded that the design has acceptable mechanical integrity for this application.
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