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Propagation and control of fire front in the combustion assisted gravity drainage using horizontal wells

机译:使用水平井的燃烧辅助重力排水中火锋的传播和控制

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The propagating characteristics of combustion fronts and coke zones in the combustion assisted gravity drainage process were studied using 3D physical simulation experiments. The main mechanisms and factors affecting stable propagation of the combustion fronts were discussed. The experimental results show that the propagation of combustion front can be divided into startup stage, radial expands stage and moving forward stage. The top oil layer is ignited first at the startup stage. Ignition temperature, ignition time and air injection rate are the key parameters for successful ignition. At the radial expanding stage the combustion front grows in size and expands radically and downwards like a funnel, and the air injection rate should match the area of combustion front. After the combustion front propagates beyond the “toe” position, the burning zone would advance along the horizontal well at a certain angle. The controlled gas override and gas seal of the coke in the horizontal well contributes significantly to the overall stability of the process. In field pilot testing, well pattern, ignition parameters and regime of injection and production should be optimized to ensure the stable propagation of the combustion front.
机译:使用3D物理模拟实验研究了燃烧辅助重力排水过程中燃烧前沿和焦炭区的传播特性。讨论了影响燃烧前沿稳定传播的主要机理和因素。实验结果表明,燃烧前沿的传播可分为启动阶段,径向扩展阶段和前进阶段。在启动阶段首先点燃顶部的油层。点火温度,点火时间和空气注入速率是成功点火的关键参数。在径向扩展阶段,燃烧前沿的大小会增大,并像漏斗一样从根本上向下扩展,并且空气喷射速率应与燃烧前沿的面积匹配。在燃烧前沿扩展到“脚趾”位置之后,燃烧区将沿水平井以一定角度前进。水平井中焦炭的受控气体超驰和气体密封对过程的整体稳定性有重要贡献。在现场先导测试中,应优化井型,点火参数以及注入和生产方式,以确保燃烧前沿的稳定传播。

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