基于非稳态反演的气枪阵列子波方向性反褶积(英文)
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  • 英文篇名:Nonstationary inversion-based directional deconvolution of airgun array signature
  • 作者:李皓 ; 李国发 ; 郭祥辉 ; 孙夕平 ; 王建富
  • 英文作者:Li Hao;Li Guo-Fa;Guo Xiang-Hui;Sun Xi-Ping;Wang Jian-Fu;CNPC Key Laboratory of Geophysical Prospecting, China University of Petroleum;State Key Laboratory of Petroleum Resources and Prospecting, China University of Petroleum;Research Institute of Petroleum Exploration and Development,Petrochina;Dagang Oil Field,Petrochina;
  • 关键词:气枪阵列 ; 气枪子波 ; 方向性 ; 非稳态反褶积
  • 英文关键词:Airgun array;;airgun signature;;directivity;;nonstationary deconvolution
  • 中文刊名:CAGJ
  • 英文刊名:应用地球物理(英文版)
  • 机构:中国石油大学(北京)CNPC物探重点实验室;中国石油大学(北京)油气资源与探测国家重点实验室;中国石油勘探开发研究院;中国石油天然气股份有限公司大港油田分公司;
  • 出版日期:2019-03-15
  • 出版单位:Applied Geophysics
  • 年:2019
  • 期:v.16
  • 基金:financially supported by the National Natural Science Foundation of China(No.41474109);; the China National Petroleum Corporation under grant number 2016A-33
  • 语种:英文;
  • 页:CAGJ201901011
  • 页数:10
  • CN:01
  • ISSN:11-5212/O
  • 分类号:120-128+144
摘要
由于气枪阵列所激发的子波具有能量强,气泡比高等优点,因此,海上地震勘探大多采用气枪阵列进行激发。但是气枪阵列具有一定的长度和宽度,加之海水虚反射的影响;致使气枪阵列子波具有明显的方向性效应,破坏了地震子波一致性,改变了反射振幅随入射角和方位角的函数关系。针对这一问题,本文提出了一种基于非稳态反演的方向性反褶积方法。该方法首先根据气枪阵列的空间配置和近场子波计算与方位角和出射角有关的远场子波。然后,基于速度模型计算不同时间地震反射在震源位置的出射角,构建方向性滤波算子。最后,采用非稳态反演方法将不同方向的地震子波整形为阵列正下方的远场子波,实现气枪阵列子波方向性反褶积处理。
        Airgun arrays are widely used in marine seismic exploration because signatures excited by airgun arrays have high energy and high-peak bubble ratio, whereas the considerable length and width of the array and ghost reflections make the airgun array signature directional. As a result, the relation of the reflection amplitude with the incident and azimuth angles is variable. This means that the directivity of the airgun array results in a nonstationary wavelet and distorts the relation of the amplitude variation with the incident and azimuth angles. To remove the directivity effect, we propose a nonstationary inversion-based directional deconvolution. At first, the signature as a function of take-off angle and azimuth angle is calculated using the spatial configuration of the airgun array and the near-field signatures. Then, based on the velocity model, the time-variant take-off angles are estimated and directional filters are designed using the take-off angles. Finally, the directivity-dependent signatures are shaped to the signature right below the airgun array using nonstationary inversion in the directional deconvolution.
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