# Patent application title: Method for Determination of Diffractor Locations at Sea Bottom for the Purpose of Attenuating Such Energy

##
Inventors:
Necati Gulunay (Missouri City, TX, US)

IPC8 Class: AG01V130FI

USPC Class:
702 16

Class name: Earth science seismology specific display system (e.g., mapping, profiling)

Publication date: 2010-09-02

Patent application number: 20100223012

Sign up to receive free email alerts when patent applications with chosen keywords are published SIGN UP

## Abstract:

Coherency analysis, such as semblance scan or stacking amplitude, is used
to locate diffractors. Once the diffractors are located, noise energy
originating from the diffractors is minimized. Locations of each
diffractor are determined by comparing the lateral coherency of the
received amplitudes that each assumed diffractor position generates.## Claims:

**1.**A method of determination of seabottom diffractor location utilizing traces of a recorded 3-D marine seismic survey with one or more cables, comprising the steps of:Selecting coordinate boundary;Calculating lateral coherency values, wherein the coherency value is calculated using amplitudes of traces at calculated travel times; andDetermining seabottom diffractor location in the coordinate boundary area using the coherency values.

**2.**A method of determination of diffractor location utilizing traces of a recorded 3-D marine survey with one or more cables, comprising the steps of:Selecting coordinate boundary;Calculating lateral coherency values, wherein the coherency value is calculated using amplitudes of traces at calculated travel times;Determining diffractor location in the coordinate boundary area using the coherency values; and wherein said Steps B and C include the steps of:Selecting scan increments; andSearching local maxima in the scan increment identified from said coherency value calculation to determine the locations of the diffractors.

**3.**The method of claim 2 wherein Step B includes smoothing in coherency calculations using multiple time samples and there is included the step of:Rejecting the diffracted energy for each selected diffractor location.

**4.**The method of claim 3 wherein Step B has included the step of accomplishing the smoothness of the coherency values by the use of multiple time samples.

**5.**The method of claim 4 wherein more than one time sample is used and a matrix of numbers is created for use in coherency calculations.

**6.**The method of claim 4 wherein the number of time samples chosen is arbitrary.

**7.**The method of claim 4 wherein Step A includes the step of constituting a test grid and semblance is used for the coherency calculations for all points on the grid and there is included the step of calculating semblance using one or many time samples on each trace.

**8.**The method of claim 7 wherein the fold value at each location is used to accomplish normalizing.

**9.**The method of claim 8 wherein the maximum fold value can be used for normalizing.

**10.**The method of claim 2 wherein the scan increments are chosen from any random distance value.

**11.**The method of claim 10 wherein the scan increments are 25 m in both x and y directions.

**12.**The method of claim 10 wherein the scan increments are as low as 5 m and as high as 100 m.

**13.**The method of claim I wherein in Step B at least one of the traces that a diffractor has contaminated is used in the coherency calculations.

**14.**

**15.**The method of claim 1 wherein there are boundary values of the boundary area and the chosen boundary values, X

_{min}, X

_{max}, Y

_{min}, Y

_{max}, are extended by the amount that a seismic wave can travel in the recording time.

**16.**The method of claim 1 wherein the calculated travel times are in the recorded range of said survey.

**17.**The method of claim 1 wherein the one or more cables per shot and one or more shots are used in the coherency value calculations.

**18.**The method of claim 1 wherein if the calculated travel time falls between two samples having a coarse increment between them of the recorded trace, the value of the amplitude is interpolated.

**19.**The method of claim 1 wherein semblance is used for the coherency calculations.

**20.**The method of claim 2 wherein semblance is used for the coherency calculations.

**21.**The method of claim 1 wherein the size of the surveyed area to be searched for diffractors is selected as necessary from the 3-D marine survey parameters.

**22.**The method of claim 1 wherein there is included the step of creating a plot of the coherency values with relation to their physical location in the survey.

**23.**A method of determination of diffractor location utilizing traces of a recorded 3-D marine survey with one or more cables, comprising the steps of:Selecting coordinate boundary;Calculating lateral coherency values, wherein the coherency value is calculated using amplitudes of traces at calculated travel times; andDetermining diffractor location in the coordinate boundary area using the coherency values;wherein the determining of the actual locations of the diffractors is determined by requiring that a local maxima point on a coherency plot be the largest amplitude in a space (x, y) window.

**24.**The method of claim 23 wherein the window size is 100 m by 100 m.

**25.**

**26.**The method of claim 23 wherein the window size is calculated by inputting a window size in distance, which is then converted into a window size in grid points.

**27.**The method of claim 23 wherein there is included the step of comparing the coherency value inside the window to determine the largest amplitude in the neighborhood.

**28.**The method of claim 27 wherein a point of coherency value is chosen as local maxima if it is greater than its neighbors.

**29.**The method of claim 23 wherein said window is then moved by a single point in either the x or y direction until every point on the grid has been compared to its neighbors.

**30.**

**31.**The method of claim 1 wherein there is included the step of using flattening techniques once the diffractors are located.

**32.**The method of claim 31 wherein noise rejection is included in the steps of claim 31 and is accomplished through the use of a tool for removing events that contaminate data.

**33.**The method of claim 32 wherein noise rejection is accomplished through FK filter.

**34.**The method of claim 32 wherein noise rejection is accomplished through regular and high-resolution radon filter.

**35.**The method of claim 32 wherein noise rejection is accomplished through eigenimage filter.

**36.**The method of claim 1 wherein there is included the steps of flattening and event suppressing for the found diffractor locations.

**37.**The method of claim 1 wherein the coherency values are calculated by stacking amplitude.

**38.**The method of claim 1 wherein in Step A the coordinate boundary area is the area necessary for evaluating one shot.

**39.**The method of claim 1 wherein in Step A is the step of selecting coordinate boundary area of surveyed data of a recorded range.

**40.**The method of claim 39 wherein the data of the whole survey area is used.

**41.**A method of determination of diffractor location utilizing a recorded 3D marine survey with one or more cables, comprising the steps of:Selecting coordinate boundary area;Selecting scan increments;Calculating semblance values; andSearching local maxima in the scan increment identified from said semblance value calculation to determine the locations of the diffractors.

**42.**A method of determination of diffractor location utilizing a recorded 3D marine survey with one or more cables, comprising the steps of:Selecting coordinate boundary area;Selecting scan increments;Calculating stacking amplitudes values; andSearching local maxima in the scan increment identified from said stacking amplitudes value calculation to determine the locations of the diffractors.

**43.**A method of determination of a diffractor location utilizing a recorded 3-D marine survey with one or more cables, comprising the steps of:Selecting boundary area;Calculating coherency values;Determining diffractor location in the boundary area using the coherency values.

**44.**A method of determination of diffractor location utilizing traces of a recorded 3-D marine survey with one or more cables, comprising the steps of:Selecting coordinate boundary area;Selecting scan increments;Calculating coherency values, wherein the coherency value is calculated using amplitudes of traces at calculated travel times; andSearching local maxima in the scan increment identified from said coherency value calculation to determine the locations of the diffractors.

**45.**The method of claim 44 wherein there is included the step of:Rejecting the diffracted energy for each selected diffractor location.

**46.**The method of claim 44 wherein there is included the step of smoothing in coherency calculations.

**47.**A method of determination of sea bottom diffractor location utilizing traces of a recorded 3-D marine survey with one or more cables, comprising the steps of:Selecting coordinate boundary in the sea bottom;Calculating coherency values, wherein the coherency value is calculated using amplitudes of traces at calculated travel times; andDetermining diffractor location in the coordinate boundary area using the coherency values.

## Description:

**FIELD OF THE INVENTION**

**[0001]**The present invention relates to geophysical prospecting using seismic signals, and in particular an automatic method for determining the locations of the shallow inhomogeneities or obstacles (to be called diffractors or scatterers) that scatter back energy radiated from source to the recorded sections in 3-D marine surveys.

**BACKGROUND OF THE INVENTION**

**[0002]**In the field of geophysical prospecting, seismic signals are used to do 3-D seismic surveys of a predetermined area. However, problems arise in the collection of data due to the backscattering of energy from the shallow inhomogeneities or obstacles.

**[0003]**1. Prior Art at Compagnie Generale De Geophysique

**[0004]**Compagnie Generale de Geophysique utilizes a process called Deterministic Diffractor Noise Reduction (DDNR) to remove the contribution of diffractor energy from the survey. DDNR involves identifying and picking travel times for each diffractor located at sea bottom. Once travel times are known for a diffractor, then its location can be calculated by assuming a speed of propagation, like 1500 m/s, for the medium. Data can then be flattened using travel times calculated for the diffractor and the flat component of energy (diffraction) can be attenuated using FK filter or Radon transform filter, as it is known in the art.

**[0005]**2. Prior Art in the Industry

**[0006]**Fookes et al. ("Practical interference noise elimination in modern marine data processing," Expanded Abstracts, 2003 SEG Annual Meeting) follow a method similar to Compagnie Generale de Geophysique DDNR method mentioned above: pick travel times and find the diffractor location that minimizes the error between calculated travel times and measured travel times. Upon determination of diffractor location, the data is flattened and flat events suppressed.

**[0007]**A use of coherency measurement is using semblance in stacking velocity analysis of seismic data and is done by Taner and Koehler (1969, "Velocity spectra--digital computer derivation and applications of velocity functions," Geophysics, 34, 859-881). The use of other coherency measures than semblance for lateral coherency of events is also possible: energy normalized cross correlation sum, stacking power, or stacking amplitude are other possibilities. Key and Smithson (1990, "New approach to seismic-reflection event detection and velocity determination": GEOPHYSICS, Soc. of Expl. Geophys., 55, 1057-1069.) derived their coherency measure from the eigenvalues of the problem at hand. Gulunay (1991, "High resolution CVS: Generalized covariance measure", 61st Ann. Internat. Mtg: Soc. of Expl. Geophys., 1264-1267) studied the relationship of such coherency measures including the ones derived from semblance. Gonzalez-Serrano and Chon ("Migration velocity analysis in 3-D," Expanded Abstracts, 1984 SEG Annual Meeting), Sicking ("Diffraction semblance for velocity and structure analysis," Expanded Abstracts, 1987 SEG Annual Meeting), and VarWest et al. ("Relation between velocity fields and imaging in the presence of lateral velocity variations," Expanded Abstracts, 1985 SEG Annual Meeting) use semblance analysis for prestack migration velocity determination. Landa et al. ("A method for detection of diffracted waves on common offset sections," Geophysical Prospecting, 35, 359-373, 1987) use semblance analysis to find buried edges in x-z plane that cause diffraction under a 2-D seismic line (shooting and receiving along x direction, shots and receivers at the surface, z=0) using common offset data (x-t). Landa and Keydar ("Seismic monitoring of diffraction images for detection of local heterogeneities," Geophysics, 63, 3, 1093-1100, May 1998) use semblance analysis to detect local heterogeneities (diffractors) buried under a 2-D section (x-z plane) using a source receiver configuration similar to the ones used in 2-D seismic recordings (shooting and receiving along x-z direction, shots and receivers at the surface, z=0). The paper discusses a "D-section" which is similar in concept to semblance scanning; however, D-section is done for diffractor buried in a vertical plane of a complex earth. U.S. Pat. Nos. 6,687,618 and 6,546,339 also address the use of semblance scan in geophysical processing using seismic signals.

**[0008]**Two papers by Blonk et al (1994, "Inverse scattering of surface waves: A new look at surface consistency", Geophysics, 59, 6, 963-972 and 1995, "An elastodynamic inverse scattering method for removing scattered surface waves from field data", Geophysics, 60, 6, 1897-1903.) address the issue of finding and removing such diffractors for land data but their method is based on "linearized elastodynamic inverse scattering theory" and involves consideration of temporal frequency, solution of linear systems with tools like conjugate gradient algorithm and is completely different from the time domain amplitude coherency approach of the arrival energy used in this invention.

**[0009]**It is an object of this invention to remove the energy from the survey that is contributed by the diffractor.

**[0010]**It is a further object of the present invention to eliminate the task or necessity of picking of arrival or travel-times or going into complex theoretical calculations as in Blonk et al (1994, 1995) papers for determination of diffractor locations.

**SUMMARY OF THE INVENTION**

**[0011]**Diffraction is a wave phenomenon where a source radiates energy to a medium and an obstacle in the medium scatters that energy back to an array of receivers placed in the same medium. Seismic energy radiated by air guns in a 3-D marine survey travels in water or shallow part of the seismic section and gets scattered by diffractors at the water bottom, contaminating the seismic sections. Materials left at the sea bottom, such as wellheads, shipwrecks, even outcropping geology, may act like diffractors.

**[0012]**The present invention eliminates the task of picking arrival times by judging the likelihood of a tested location to be a diffractor point by calculating coherency of arrivals from that point. The present invention preferably utilizes semblance scan as a coherency analysis tool to minimize the energy contributed to the survey by diffractors. Any of the aforementioned measures could be used for coherency calculation; however, semblance derived measures are the most advantageous. First, they are the most economical to use. For this reason, the present invention uses semblance as the coherency measure. Second, semblance is sensitive to the coherency of the event but not to its actual strength. For example, stack amplitude for a five-sample event with amplitudes (1,1,1,2,1) is 6/5=1.2 and its semblance is 0.9. Stack amplitude for (10,10,10,20,10) is 60/5=12 but its semblance is still the same and is 0.9. An event could be weak but it could be coherent while an event could be strong but it may not be coherent.

**[0013]**In the present invention, locations of each diffractor are determined by comparing the lateral coherency of the received amplitudes that each assumed diffractor position generates. That is, these are the locations that are in agreement with the travel paths observed on the seismic traces recorded. The amplitudes of the diffractions are picked from received traces at the travel times (or around the travel times) it takes the emitted energy by a source to travel from it to a diffractor and from a diffractor to a receiver. Many measures may be used for lateral (receiver to receiver) coherency, including semblance. Areas of the x-y plane that radiate back scattered energy from sources to receivers in a 3-D marine recording can be put into semblance scan to find out which of these locations are likely to be the diffractor locations (by attaching a semblance value to each point). For a given diffractor, the amplitudes picked to be put into the semblance calculation can come from the traces (source-receiver pairs) of one or many sources and one or many array of receivers (called cables or streamers). This allows points with large semblance to be picked, thereby eliminating the need for picking travel times for each diffractor. Once a diffractor location is known, then data can be flattened using sum of the travel times from source to diffractor and from diffractor to receiver and then applying one of the methods of prior art, such as FK filtering, Radon filtering, etc. to remove such energy contributed by this diffractor.

**DESCRIPTION OF THE DRAWINGS**

**[0014]**For further understanding of the nature and objects of the present invention, reference should be had to the following figures in which like parts are given like reference numerals and wherein:

**[0015]**FIG. 1 shows boat sail-line patterns on a typical 3-D marine survey;

**[0016]**FIG. 2 shows source-diffractor-receiver travel path;

**[0017]**FIG. 3 shows arrival times of diffractions that are received from a diffractor by a boat carrying five cables;

**[0018]**FIG. 4 shows scan range for a given cable;

**[0019]**FIG. 5 shows a semblance plot generated from 20 shots each with 8 cables, each cable with 120 traces;

**[0020]**FIG. 6 shows local maxima picker; and

**[0021]**FIG. 7 shows flattening a diffractor.

**DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS**

**[0022]**In seismic prospecting for oil and gas, a boat 10 pulls a set of receivers 15 ((x

_{r,y}

_{r}) positions) placed on structures referred as "streamers" or "cables". The boat 10 has airguns (not shown but well known in the art) placed near it and these guns fire at certain intervals ((x

_{s,y}

_{s}) positions) creating a seismic disturbance that travels into layers of earth and is reflected from each layer and received by these receivers. Reflections generally come from vertical slices of earth, which are called "subsurface lines" or "common midpoint lines," formed by the geometry of the recording. There are as many subsurface lines as there are cables. The boat 10 generally travels on a straight line to cover an area of interest and then turns back and places itself on the same course but with some lateral shift to produce more subsurface lines as shown in FIG. 1. Surface lines may overlap. It is imperative that what is recorded represents reflections from strata, but there are many noise types recorded. Among them is the scattered energy from inhomogeneities at sea bottom or materials that are at the sea bottom as wells, wellheads, sunken ships, etc. The scattered energy from the inhomogeneities are what the present invention seeks to eliminate.

**[0023]**A 3-D marine survey is generally recorded with patterns depicted in FIG. 1. A boat 10 pulling a number of streamers 15 starts from a point, like point 1, and travels to point 2. Direction from Point 1 to Point 2 could be any azimuth, i.e. not necessarily a south to north line. The boat turns at point 2 and travels until point 3 and makes another turn at point 3. It then travels to point 4 and makes another turn. It travels to point 5 and then makes another turn, and so on. Therefore, slightly shifting rectangles defined by points (1,2,3,4), (5,6,7,8), and so forth, are formed.

**[0024]**In the present invention, the initial step in locating the diffractors is to determine the minimum x value, maximum x value, minimum y value, and maximum y value of the receiver coordinates for the whole survey, as shown in FIG. 1. This is done by looking at the trace headers on the data. (A source receiver pair is called a trace.) These values are called: X'

_{min}, X'

_{max}, Y'

_{min}, Y'

_{max}, respectively. These values are then extended by an amount that a seismic wave can travel at the water velocity in the recording time. These new minimum and maximum values are called: X

_{min}, X

_{max}, Y

_{min}, and Y

_{max}, respectively. Then,

**X**

_{min}=X'

_{min}-VT

**X**

_{max}=X'

_{max}+VT

**Y**

_{min}=Y'

_{min}-VT

**Y**

_{max}=Y'

_{max}+VT

**where V is the medium**(water) velocity and T is the recording time.

**[0025]**X and Y grid sizes, dx and dy respectively, are chosen to scan this area. Grid size (scan increment) used is typically 25 m both in x and y. Practice shows that any scan increments lower than 25 m and scan increments as high as 100 m can be used. However, the finer the scan increment, the more accurate the location determination for the diffractors. Of course, the run time is the more expensive. Sampling coarser than 100 m is not expected to yield accurate travel times for flattening the data for purpose of noise attenuation.

**[0026]**Then, for each point (x

_{d,y}

_{d}) on the grid defined by:

**x**

_{d}=x

_{min}+(i-1)*dx (i=1, 2, . . . , i

_{max})

**y**

_{d}=y

_{min}+(j-1)*dy (j=1, 2, . . . , j

_{max})

**where**

**i**

_{max}=1+(X

_{max}-X

_{min})/dx

**j**

_{max}=1+(Y

_{max}-Y

_{min})/dy

**a coherency value is calculated using amplitudes**, a

_{n}, picked at the travel time (using Eq. 2) from some (or all) of the source-receiver pairs ((x

_{s,y}

_{s}) and (x

_{r,y}

_{r}) pairs) for which travel times are in the recorded range (i.e. scattered energy from diffractors far away will not reach a given receiver if its arrival time is greater than recording time.)

**[0027]**There are many coherency measures available in the prior art. As discussed in the background and summary of the invention, it is possible to use stack amplitudes, stack power, energy normalized cross-correlation sum, or semblance. This invention uses the conventional semblance defined by

**s**= ( n = 1 N a n ) 2 N n = 1 N a n 2 EQ . 1 ##EQU00001##

**[0028]**Semblance Calculation from a Single Time Sample Per Trace

**[0029]**If selectivity is desired, one can use functions of semblance as discussed by Gulunay, (1991). Some of the useful functions are:

**s n n**> 1 ##EQU00002## s 1 - s ##EQU00002.2## log ( 1 1 - s ) ##EQU00002.3##

**[0030]**This invention preferably uses semblance (Eq. 1 or its smoothed version to be given in Eq. 4). Once such a semblance distribution is obtained,

**S**(i,j) (i=1, 2, . . . , i

_{max}, j=1, 2, . . . , i

_{max})

**then local maxima in this function can be found by requiring a point to be**larger than all of the points in its neighborhood, (e.g. in a 100 m by 100 m part of the grid). Among all such points, the ones with significant values can be selected as valid diffractors.

**[0031]**FIG. 2 depicts a source (point S) pulling some streamers 15 (cables) with typically hundreds (even thousands) of receivers (point R) placed on them. As source radiates energy travels to diffractor point D and is scattered back. Scattered energy radiates backs and sweeps all of the receivers (points like R) on the streamers 15.

**[0032]**Arrival time of diffracted energy is the sum of two terms: source term, T

_{1}, and receiver term T

_{2}, as shown in FIG. 2. As source (x

_{s,y}

_{s}) and receiver (x

_{r,y}

_{r}) coordinates are known, the value of arrival time from an assumed diffractor location (x

_{d,y}

_{d}) can be calculated using a medium velocity, V, like 1500 m/s. The equation for this calculation is given in Eq. 2.

**T**= T 1 + T 2 = 1 V ( ( x s - x d ) 2 + ( y s - y d ) 2 + z d 2 + ( x r - x d ) 2 + ( y r - y d ) 2 + z d 2 ) EQ . 2 ##EQU00003##

**[0033]**Travel Time Equation for Source-Diffractor-Receiver Travel Path.

**[0034]**Here z

_{d}represents the relative (with respect to the source and receivers) depth of the diffractor which is assumed to be zero in general but one can scan for a range of depths as well, if desired.

**[0035]**Indeed, if stacking amplitude

**s**= n = 1 N a n EQ . 3 ##EQU00004##

**[0036]**Stack Amplitude as an Attribute.

**rather than semblance values**(defined in Eq. 1) are calculated, this invention will produce pre-stack migration, done for a small range of depths, and with velocity, V (medium velocity). Therefore, using such stack amplitudes for picking the location of diffractors in half space (x

_{d,y}

_{d},z

_{d}) is also a new approach.

**[0037]**To illustrate the method, note that arrival times form hyperbolic looking events 25 as depicted in FIG. 3 (for a small set of (five) cables). Each vertical line 20 in FIG. 3 depicts a trace (source-receiver pair) recorded by receiver on a cable during a particular 3-D shot. The wavelets on the traces depict the diffracted energy. The amplitude value, a

_{n}, (n=1, 2, . . . , N where N is the number of traces that diffractor contaminated) at the arrival time calculated by Eq. 2 for each source-receiver pair that can record energy from this diffractor with the recording time available on the seismic traces can be picked and put into semblance calculation given by Eq. 1.

**[0038]**When the travel time falls between the two time samples of the digitally recorded seismic trace then the value of sample, a

_{n}is interpolated from the nearby samples with known techniques of the prior art.

**[0039]**To increase the reliability (smoothness) of semblance values, as it is known in prior art, it is possible to use more than one time sample (centered at the arrival time) for a trace to improve the reliability of the semblance calculation. If M time samples, instead of a single one, are picked, then there is a matrix of numbers (A

_{m,n}) to use in the semblance

**( a 1 , 1 , a 1 , 2 , , a 1 , N a 2 , 1 , a 2 , 2 , , a 2 , N a M , 1 , a M , 2 , , a M , N ) ##EQU00005##**

**where rows**, m=1, 2, . . . , M, represent time and columns, n=1, 2, . . . , N, represent space (traces).

**[0040]**Semblance calculations, as it is known in prior art, are made using Eq. 4:

**s**= m = 1 M ( n = 1 N a m , n ) 2 N m = 1 M n = 1 N a m , n 2 EQ . 4 ##EQU00006##

**[0041]**Semblance Calculation from M Samples Per Trace (Samples Centered at the Arrival Time).

**[0042]**The value of M can be arbitrary. However, practice shows that large values of M are not helpful. Lower values of M are preferable to increase both peak semblance values and resolution in time, which is equivalent in resolution in location (resolution in source to diffractor, diffractor to receiver distance means resolution in diffractor distance). A value of M about the size of the main peak of the diffracted arrival wavelet is best.

**[0043]**It is mentioned above that N in Eq. 1 is the number of traces that a diffractor has contaminated. There could be many such traces, coming from many sources and many streamers. There is not an increased benefit in using all these of contributions in one semblance calculation, as there are issues in mixing amplitudes from different shots and cables. For example, noise content differences would be one such obstacle. It was found that using only traces from one shot and one cable at a time tends to work the best. As there are many cables (c=1, 2, . . . , N

_{c}) and many shots (p=1, 2, . . . , N

_{p}), the results of multiple scans at one point (i,j) need to be accumulated

**s**( i , j ) = p = 1 Np c = 1 Nc s p , c ( i , j ) EQ . 5 ##EQU00007##

**[0044]**Semblance Accumulation from Many Cables and Shots.

**[0045]**One needs to keep track of the number of values summed for each position (i,j), known sometimes as "fold," so that the results could be divided by its maximum to achieve physically meaningful semblance values (between 0 and 1). This is known as "normalization". It is also possible to use the fold value at each location to do the normalization (i.e. division by Np*Nc), but that might enhance the value of a low fold semblance and hence cause an unreliable semblance value to be considered as a diffractor location. It was found that the maximum fold is a better value to use for the normalization.

**[0046]**For determination of the diffractor azimuth and individual scan values,

**[0047]**1) For cables that are not far from the shot, as in current 3-D marine recordings, one cable alone cannot tell the azimuth of the diffractor. That is, a diffractor shows itself at two points that are symmetrically oriented with respect to the line formed by the cable, one being the correct image, the other one incorrect. Adding the results of the scans from multiple cables suppresses the incorrect image and enhances the correct one.

**[0048]**2) When calculating individual scan values S

_{pc}(i,j), it saves computer time if one does not attempt to calculate this value for all grid points. That is, only those points that are within VT neighborhood of the receivers on the cable (see FIG. 4) need to be considered. If a' and b' are minimum and maximum found on the receiver x coordinates then considering diffractors with x coordinates that are in the range [a,b] where a=a'-VT and b=b'+VT is sufficient. Similarly, if c' and d' are minimum and maximum found on the receiver y coordinates, then considering diffractors with y coordinates that are in range [c,d] where c=c'-VT and d=d'+VT is sufficient. Here V represents medium velocity and T represents the recording time as before.

**[0049]**FIG. 5 shows the results of semblance scan obtained from 20 shots (N

_{p}=20) each pulling 8 cables (N

_{c}=8). Horizontal axis 30 is the x-coordinate and vertical axis 35 is the y-coordinate. The x-coordinate 30 increases towards the right, facing the figures and y-coordinate increases towards the top of the FIG. 5. The scan increment used here is preferably 10 m in both x and y directions. Practice shows that scan increments as low as 5 m and as high as 100 m can be used. The finer the scan increment, more accurate the location of the local maxima. Sampling coarser than 100 m is not preferred and is not expected to yield accurate travel times for flattening the data for purpose of noise attenuation. The color code 40 is shown at the lower right corner of FIG. 5. Semblance values vary between zero and one. Peak semblance value for this run was 0.239. Semblance values above 0.100 are clipped in the Figure.

**[0050]**FIG. 5 provides a visual display of the diffractor locations. It covers an area of roughly 40 km

^{2}. Actual locations are machine picked by requiring that a local maxima point needs to be the biggest amplitude in a space (x,y) window, typically and preferably specified as 100 m by 100 m. More explicitly, a user given window size in distance units (like meters) for local maxima determination is first converted to a window size in grid points, each side being an odd number (1, 3, 5, . . . ). If window size is 2m+1 by 2n+1 (where m and n are positive integers), then each point, (i,j) on the grid is checked to determine if it is the largest amplitude in 2m+1 and 2n+1 neighborhood:

**a**

_{i,j}≧a

_{i}-u,j-v for -m≦u≦+m and -n≦v≦+n EQ.6

**[0051]**Local Maxima Checker Definition

**where u and v are integers except u**=v=o. All i and j locations, except the edges, i.e. all the points satisfying

**m**+1≦i≦i

_{max}-m and n+1≦j≦j

_{max}-n

**are checked and**(i,j) points satisfying Eq. 6 are taken as possible diffractor locations. Order in which one varies i and j depends on how the values are stored in the computer; preferably one first scans row indices on column 1 (i=1,i

_{max}), then column 2, then column 3, etc.

**[0052]**FIG. 6 illustrates local maxima search window 50 for a 3-by-3 window for simplicity. For a center point 55 to be chosen as a local maxima, it must be greater than its eight neighbors 55 in FIG. 6. For a 5-by-5 window the middle point must be greater than its 24 neighbors. For a (2m+1)-by-(2n+1) window the amplitude of the middle point must be greater than the amplitudes of its (2m+1)(2n+1)-1 neighbors.

**[0053]**Once a set of such diffractor locations are found, one can use methods known in prior art to flatten and reject diffracted energy for each location. Flattening is a process (depicted in FIG. 7) where diffracted event's travel times 60 are subtracted 65 from the trace. This is known in prior art as "static shift". During this static shift, care must be taken not to lose data by extending (doubling) trace length and putting data at the bottom before static shifting upwards (otherwise data above diffraction will be lost).

**[0054]**There are numerous tools in geophysical industry to remove events contaminating the data. Among them are FK filter, regular and high-resolution radon filter, eigenimage filter, etc. Any of these could be used to suppress such diffracted energy. Flattening and flat event suppression is done for every diffractor found in the survey.

**[0055]**Because many varying and different embodiments may be made within the scope of the invention concept taught herein which may involve many modifications in the embodiments herein detailed in accordance with the descriptive requirements of the law, it is to be understood that the details herein are to be interpreted as illustrative and not in a limiting sense.

User Contributions:

Comment about this patent or add new information about this topic:

People who visited this patent also read: | |

Patent application number | Title |
---|---|

20110208175 | Methods for Treating Sleep Apnea Via Renal Denervation |

20110208174 | CRYOCLAMP AND METHOD OF USE |

20110208173 | Methods for Treating sleep apnea via renal Denervation |

20110208172 | Eye measurement and modeling techniques |

20110208171 | METHOD AND DEVICE FOR FORMING CUT SURFACES IN A TRANSPARENT MATERIAL |