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Imaging Fractures Using Temperature Transients From Perturbation Analysis-A Novel Surveillance Technique Applied to the Belridge Diatomite

机译:使用摄动分析的温度瞬变对骨折进行成像-一种应用于Belridge硅藻土的新型监视技术

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Results of a temperature transient analysis of data from Shell's diatomite steamdrive pilots are used to image hydraulic injection fracture lengths, angles, and heat injectivities into the low-permeability formation. The Phase I pilot is a limited-interval injection test. In Phase II, steam is injected into two 350-ft upper and lower zones through separate hydraulic fractures. Temperature response of both pilots is monitored with 16 logging-observation wells. A perturbation analysis of the nonlinear pressure diffusion and heat-transport equations indicates that at a permeability of approximately 0.1 md or less, heat transport in the diatomite tends to be dominated by thermal diffusivity, and pressure diffusion is dominated by the ratio of thermal expansion to fluid compressibility. Under these conditions, the temperature observed at a logging-observation well is governed by a dimensionless quantity that depends on the perpendicular distance between the observation well and the hydraulic fracture divided by the square root of time. Using this dependence, a novel method is developed for imaging hydraulic-fracture geometry and relative heat injectivity from the temperature history of the pilot. The azimuth of the Phase I hydraulic fracture is determined to be 14° ± 2 N-NE. The azimuth of the Phase II upper hydraulic fracture is determined to be 16° ± 2 N-NE in the northern half of the pilot, and estimated to increase to 21 ° ± 2 in the southern half of the pilot. The azimuth of the lower hydraulic fracture averages 19° ±4. The hydraulic fractures are found to be symmetric around both injectors, with an estimated length of 200 ft. Increased steam injection after the first year of pilot operations caused what is interpreted to be horizontal fractures toward the west in the G cycle and the east in the M cycle. These features are imaged to be at least 100 and 160 ft, respectively, along the hydraulic fracture azimuth. These conclusions are compared to tiltmeter data, microseis-mic data, and a simulation history match of pilot performance. Microseismic events recorded in the pilot are apparently not diagnostic of heat delivery to the formation.
机译:壳牌硅藻土蒸汽驱动器先导数据的温度瞬态分析结果用于对低渗透地层中水力压裂的裂缝长度,角度和热注入量进行成像。第一阶段的先导是有限间隔喷射测试。在第二阶段中,通过单独的水力压裂将蒸汽注入到两个350英尺的上部和下部区域。两个试点的温度响应通过16个测井观测井进行监控。对非线性压力扩散和热传递方程的扰动分析表明,在渗透率约为0.1 md或更小时,硅藻土中的热传递往往受热扩散率支配,而压力扩散受热膨胀比与热膨胀率的支配。流体可压缩性。在这些条件下,测井观测井的温度由无量纲的量控制,无量纲的量取决于观测井与水力压裂之间的垂直距离除以时间的平方根。利用这种依赖性,开发了一种新颖的方法,用于根据飞行员的温度历史记录水力压裂的几何形状和相对热注入率。一期水力压裂的方位角确定为14°±2 N-NE。在飞行员的北半部,确定第二阶段上水力裂缝的方位角为16°±2 N-NE,在飞行员的南半部,估计增加到21°±2。下部水力压裂的方位角平均为19°±4。发现两个注入器周围的水力压裂是对称的,估计长度为200 ft。在试运行的第一年后增加的注汽量导致在G循环中向西和向东向中的水平压裂。 M循环。这些特征沿水力压裂方位分别成像为至少100英尺和160英尺。将这些结论与测斜仪数据,微地震数据以及飞行员性能的模拟历史记录进行比较。飞行员中记录的微地震事件显然不能诊断出热量是否传递到地层。

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