Senin, 04 April 2016

3-D SEISMIC DESIGN FOR LAND SURVEY

Tri Satyo S.P
Independent Seismic Consultant
For Designing Land 3D Seismic Survey


BASIC CONCEPT
 

There are some new aspects to the survey design in three dimensions relative to 2-D surveys. The 2-D surveys are as linear as the terrain allows. Source and receiver are normally in-line with each other. Arrays may be multidimensional but most often are also in the line of survey. For 3-D surveys this is seldom the case.

The 3-D survey also includes multiple source lines as well as multiple receiver lines, and it is possible to record two source lines. The arrays also may respond in less predictable manner as they are not necessarily in line with either the source or receiver locations. If the survey is planned to acquire a good directional range of offsets, the arrays will see oncoming wavefront from a number of angles. This will require a more sophisticated analysis of the array effect. Use of the patterns and other multi-azimuth array patterns is sometimes practiced.

The accent of 2-D lines is on the fold coverage and offset range. For 3-D survey, the fold may be less but the azimuth range is added to the offset range as a parameter. If structure is complex, the good azimuthal range become important. In fig-1. There are some arbitrary number of seismic traces in a bin. For velocity analysis the bin needs to contain a range of offsets. The range of azimuth in a bin is also a consideration. The concept of azimuths also is a new factor in 3-D survey.  

The azimuthal property is not significant when the geology features only gentle dips and lateral consistency. The effect of dip is to increase apparent velocity. Thus the velocity analysis must have an azimuthal property. The imaging of complex structure is also improved by surveys with a good range of azimuths.


                                 Fig-1. Bin in 3-D survey, contains of offsets and azimuths
                                         
The Fresnel zone takes on some new characteristics in 3-D. Generally, even in 2-D, this important concept is given a small amount of attention. As the target sizes historically decrease in the size the zone become more important.

Essentially, the theoretical point source expands as it propagates in depth, “illuminating” a circular area at vertical incidence. In the seismic context this is the reflecting surface constructively contributing to the reflection. A good approximation to the radius of the zone is :


                                                   RF    = ( V-avg/2) * (T/F)1/2 


which show that the zone increases in radius with depth but decrease with higher frequency wavefronts. Migration serves to reduce the zone to some minimal size when accurately done and the data fits the assumption.


                                                         
                                             
                 
PRELIMINARY BASIC PARAMETERS

There are some parameters that need to be estimated as an input to designing 3D survey. The physics and concepts are somewhat independent of whether the survey is to have two or three dimensions or just involve some modification to their calculation.

1.   Offset
The imaging of shallow, target, and deep horizons still requires certain offsets of source and receiver. The calculation and direction may be different but the rule is :

                                                Offset  =  depth of target horizon

2.   Fold
The fold required for noise compression is a function of the local S/N conditions. This translates in 3D to the number of trace in bin. Because of the extra focusing by migration and the flexibility of binning, fold can be less than required 2-D survey.

3.   Frequency     
The temporal frequency required Is not much different from that for 2-D survey. The rule for the resolution of layer of given thicknesses are best determined by modeling. The general rule is that the resolution of thin bed requires it to be sampled twice with a quarter wavelength of the highest frequency.

4.   Migration
     
At this point it is relevant to remember that when dipping beds are in the preliminary model of the survey the extent of the survey must be increased. The tangent of the angle of maximum dip modifies the areal extent of the survey.


A  3D DESIGN SEQUENCES

There are so many ways to begin and complete a survey design. The specific sequence of steps that follow are general guidelines.  The information gathering, modeling, and dimensionally independent parameters, such as offset range, are presumed to have been computed as previously describe. We must determine the offset ranges, temporal frequency, required fold, bin size, and available field equipment capacity. Less direct variables such as survey size adjustment for migration and any azimuthal requirements are also presumed to be ready. Another assumption is that the 3D software can cope with the template you have in mind.  A summary of the proposed sequence for developing in design script is :

Step-1
Determine the subsurface bin size. Twice the chosen bin size is source and receiver station spacing.

Step-2
Compute the number of source stations per square kilometer required to achieve fold with the available equipment. The number of stations per square kilometer allow computation of source line spacing.

Step-3   
Compute a receiver line spacing.

Step-4
Find the number of receiver lines allow by field equipment constrained by the required offset ranges. The result is the template.

Step-5
Decide on the x and y roll along.

Step-6
Allow for obstacles and run analyses of the script for offset distribution in the bins, ranges of offset in the bins, and azimuthal properties of the bin.

Step-7
Estimate time and costs of the script and iterate until attributes, costs and time are satisfied. Write the shooting script. Prepare to make more adjustments when the survey is begun. Often conditions found in the field requires changes in the shooting script.



                                                   Fig-2. A Schematic of 3D Design 

Group and Source Interval
The CDP bin size is the spacing between the stacked traces in the seismic cube and represents the limit of spatial resolution.  Therefore, all factors that limit resolution must be larger than the CDP size.

Group Interval
The group interval is the basic sampling of the earth by the survey. The custom is to compute this interval so that the recording data is clear from aliasing effect.  The formula for finding the largest spatial sampling will prevent aliasing is  :

                                              G = 0.5*(Va/Fmax) / sin θx    
Or inline bin size,               ΔX  = 0.25*(Va/Fmax) / sin θx    

Where G is group interval, Vis average velocity, Fmax is maximum frequency of the objective horizon and θx is dip of the horizon inline direction. Example : a 65 Hz wave travelling in a medium with dip 30 degree which has propagation velocity of 2150 m/s has a Group Interval approximately 34m. This represents  the expected limit of spatial resolution and the CDP bin size should not be larger than 17m.

Source Interval
The limit lateral resolution will be half the dominant wavelength. The dominant frequency can be measured directly from the seismic section, thus simple guideline equation for Source Interval is  :

                                          S  = Vi / Fdom

Or crossline bin size,      ΔY  = Vi / (2*Fdom)

Where S = Source interval, Vi is interval velocity and Fdom is frequency dominant.  Example : interval velocity 2150 m/s and Fdom 40 Hz, then we have the source interval is 54m.  This represents  the expected limit of spatial resolution in the crossline direction and the CDP bin size should not be larger than 27m.

Bin size recommendation
The factor which controls bin size in this case is the lateral resolution of the data since structural dips are relatively benign. 
Analysis of the geophysical data available indicates that the maximum achievable lateral resolution will be in the order of 17mx27m  The CDP bin size should therefore not be larger than this. 

Offset distributions and fold requirements

Fold considerations

If the legacy 2D data is 60 fold and is of variable quality.  Generally it ranges from fair to good but it is adequate for structural interpretation of major faults and structures.  Data of similar quality would be inadequate for detailed structural and stratigraphic interpretation. Therefore higher fold is required to stand a fair chance of gaining adequate signal to noise ratios for detailed reservoir mapping and modelling.  The design should therefore allow fold to be as high at the top of the target as the legacy 2D data and to continue to build up through to the base of the target zone. 

Common practices calculation the required 3D fold is show below :

3D Fold = 50% - 65% of 2D Fold. 


Offset

Minimum Offset

The minimum offset requirement is often calculated from the shallowest objective.  The specified shallowest objective,.  The most efficient survey design should be with source and receiver lines that capture the shallowest objective or less. This implies would provide high density shots and receivers.  Since it will cost so much, we have to make sure the shallowest offset include in the design with sufficient fold number. 
Very wide spaced receiver and source lines would also increase the footprint in the data.  Therefore the shallowest objective does not form a vital parameter in this case as the candidate designs comfortably satisfy this requirement.

Maximum Offset

The possibility that AVO effects may be present in the deeper target implies that data must be acquired at offsets long enough to give near critical angle reflections as allowed by CDP and stretch muting at the deepest objective.  There must also be regularly spaced near offset data so that AVO effects can be estimated robustly if they are present.
Therefore, fold acquired by the top of target must be sufficient to be able to image the stratigraphy and structures and fold must continue to build up until the base of the target zone so that AVO effects at the base of target can be investigated. 

The far offset required for AVO analysis can be calculated as  :

                                      Far offset   =  2 * Z * tan(i)

Where, Z is depth of deepest target and i is the incident angle close to critical angle for the deepest target.
Beside AVO consideration, the largest maximum offset is controlled by NMO Stretch.  The maximum offset demonstrated by Andreas Stark, 2008, as a simple derivation as shown below  :
                                       ΔT NMO  =  Tx – To = [(X2/V2) + To]1/2 – To 
                         
A stretch of more than Stretching factor, S,   would distort the signal after stacking and need to be mute out. This computation allow us to set the maximum spread length. If we only allow 50% stretch at the far offset, we can compute the far offset as follows  :
                                          ΔT / To   =  S
S is stretching factor (%), then  :
                              S. To  = ΔT
                             S.  To  = [(X2/V2) + To]1/2 - To  
                      (S + 1). To  = [(X2/V2) + To] 1/2     
                    (S + 1)2. To=  (X2/V2) + To2 
         [(S + 1)2 ) – 1 ]. To=  (X2/V2)
                                  X2 =   To2 V. [(S + 1)2 ) – 1 ]
                                           X   =  To.V [(S + 1)2 ) – 1 ] 1/2                                                    
                                           X   =  To.V [(S2 + 2S)] 1/2                                                     
                                 X   =  Z.  [(S2 + 2S)] 1/2    
  
Example, the deep target depth is 2,200 m we can find mute offset of 50% is 2,460m. It means, all traces with far offset more than 2,460m will be cut out under stretch mute 50%.

Azimuth Distribution
A     Wide azimuth surveys are desirable for future anisotropy and azimuth dependent processing.  However, wide azimuth surveys also tend to have a bias towards longer offset data and generally have more footprint problems than narrow azimuth surveys as they are typically recorded with larger receiver and source line intervals.  The footprint is derived from differences in data offset and azimuth properties of the traces from CDP bin to CDP bin and is more acute in low fold, wide azimuth land surveys.  CDP stretch and variations in fold at time slice and horizon times, as well as offset properties of the CDP contribute to this effect.   

Additionally, surveys which are rich in both azimuths and offsets are costly. Some compromise between the desire to record near offset data and to record all azimuths cheaply needs to be reached in order for the survey acquisition costs to be controlled.   The design proposed in this report attempt to combine optimum fold and offset distributions.

Migration Aperture
Migration process is to place dipping horizons and faults into their proper perspective dipping horizons and also the distance required to capture diffraction energy up to take off particular angle from the edge.

Lateral Migration
 The distance that a dipping reflector moves during the migration process is give by the equation

                            d = Z tan(θ),

where d is the distance moved or migration aperture, Z is the depth of the reflector and θ is the angle of dip. 
The steepest dipping event expected in the survey area is approximately 30 degrees; however, the migration aperture must be large enough to migrate diffractions, which will arise at discontinuities, bed truncations and faults
The area covered by survey must be extended to account for the aperture and can add significant cost to a survey.  This can be more efficiently handled with the use of tail spreads since it is the deeper data that has the larger aperture.  Tail spreads provide a migration friendly taper at the edge of the survey and helps to reduce the shot hole drilling effort.

Resolution

Resolution in seismic data is the ability to distinguish between objects, that is, to see a second object in the presence of another.

Vertical Resolution
Vertical resolution relates to how far apart two interfaces must be to distinguish separate reflections from them or how thick a bed must be to allow distinguishable reflections from the bed's top and bottom. The length (in time) of seismic wavelets produces confusion because successive reflections overlap, so it is desirable that the source wavelet be short. The wavelet should have a distinctive, sharp peak to be timed. Side lobes are undesirable because they can be mistaken for true reflections. They add to confusion because of interference. Constructive interference produces an amplitude buildup known as the tuning effect. The tuning thickness is usually taken as the limit of resolution or limit of separability. The vertical resolution equal with one-fourth wavelength  :
                                          Limit of  Vertical Resolution  =  Wavelength/4                 or,      
                                         Limit of  Vertical Resolution  =  V-average/(4*Fdom)                 
Example, using the equation above we can calculate the vertical resolution for both shallow and deep target as follows :

Shallow target
V-average    = 2150 m/s
F dom  =  40 Hz
Resolution  =  13 m

Deep Target
V-average    = 2900 m/s
F dom  =  20 Hz
Resolution  =  36 m
The calculation above recommend that the limit of layer thickness which can be observed for shallow target is minimum of 13m and for deep target is 36m.


                                              Fig-3. Schematic of Fresnel Zone


Lateral Resolution
The waves giving rise to a reflection event are reflected from a fairly large, roughly circular area of the reflecting interface known as the first Fresnel zone. Reflections from this zone arrive at a geophone so as to constructively interfere. The radius of this zone is often taken as the horizontal resolution for unmigrated seismic data and to be formulated as follows   :

                                                    RF    = ( V-avg/2) * (T/F)1/2          or
                                                    DF   =  V-avg * (T/F)1/2
Where RF is radius of Fresnel Zone and DF is diameter of Fresnel Zone.
Migration effectively collapses the in-line aspect of the Fresnel zone, so this measure of resolution is not appropriate with the migrated seismic data that are usually used for interpretation. In principle, after migration, lateral resolution is reduced to trace spacing.

Example, using the equation above, then we can calculate the Diameter of Fresnel Zone (DF) before migration on every target horizon as   :


Shallow target

V-average    = 2150 m/s
F dom  =  40 Hz
T  = 650 ms
D =  274 m

Deep Target

V-average    = 2900 m/s
F dom  =  20 Hz
T  =  2100 ms
DF  =  940 m
The calculation above recommend that the limit of horizontal resolution referred to the shallow target is 274m.
In order to collapse the diffraction hyperbolic up to 70% of migrated energy (or 15o point of diffraction curve), the edge of the survey boundary must be extent with half of deep Fresnel zone diameter, then, 940 : 2 = 470m for unmigrated data, or equal with deep radius of Fresnel Zone. 

                                            Fig-4.  Anatomy of diffraction curve





Edge Management

Edge management refers to the aspect of 3-D design that specifies the width of the migration apron and the fold taper. The fold taper is the area at the edge the survey where full-fold (or nearly full-fold) at depth has not been reached before migration. Often a small relaxation in the definition of sufficient fold near the edges can significantly reduce the total size of the survey.

The fold taper can easily add 30% to the total 3-D area, even on large surveys. On small surveys, this percentage increases disproportionately and makes small 3-D surveys, which might be intended to cover as little as 2.5 km2, extremely expensive on a cost-per-area basis. The design of the patch (and there-fore fold taper) is often different in the receiver line direction than in the source line direction because dips may change depending on the azimuth, and then the migration apron changes with dip azimuth.

Generally, fold builds up faster in the cross-line direction than in the in-line direction. This is especially true for narrow azimuth designs because the fold taper in the cross-line direction is directly proportional to the cross-line fold. Careful distribution of receivers can build up fold faster for certain geometries. The orientation of the patch with respect to the survey outline can affect the cost of a survey significantly.

Any 3-D survey should be considered as consisting of three zones. The first (innermost) zone is the domain of the interpreter. All traces lying in this zone should be considered full-fold and fully mi-grated. This is the image area the interpreter should limit his examinations to and use as the basis for geological interpretation. The second (middle) zone is a corridor around the innermost (image) zone.



                                Fig- 5.  Three zone acquisition model (theoretical)


Theoretically, the width of this corridor is equal to the migration apron. In this corridor, the seismic processor assembles full-fold stacked traces. Migration moves most of the energy of these traces into the edge of the innermost (image) zone. The third (outermost) zone is a corridor around the middle zone. The width of this zone is the fold taper. In this corridor, the acquisition planner places sources and receivers to ensure full-fold at the start of the middle (full-fold) zone. The term edge management implies the proper design of these three zones. Compromises can and almost always will be made.



                                 
                                       Fig-6. Practical edge management


It is not necessary that traces in the middle zone have near offsets. Farther traces contain deep data be-cause of NMO muting, but deep data migrate farther laterally. If the bins near the outside of the second zone contain only far traces, and bins closest to the innermost zone contain more near traces (hence shallow data), a good migrated result on the edge of the innermost (image) zone should result at all depths.

It may also be possible to relax the 30° requirement for very deep data. This concession reduces the size of the migration apron. Traces that are not quite full-fold may be acceptable for bins near the out-side edge of the middle zone

Rule of Thumb: Migration apron is normally chosen as the larger of:

     a)  The lateral migration movement of each dip in the expected geology, or


     b)  The distance required to capture diffraction energy coming upwards at a 
          scattering angle of 30°, or


     c)  The radius of the first Fresnel zone.




Calculation of Templates

Below is the example of final template 3-D design for orthogonal and brick patterns. The very detail recommendation  including the cost estimation are shown below.



                      Fig-7.  Table shows the final recommendation of 3D parameters






FINAL DELIVERY

At the end of the 3-D design, we will provide our client with a complete report and CD, this final delivery will include   :

1.   Final Report

This document reports the recommendation of some acquisition parameters with a flexibility for client to choose some options of template.  Some consideration and data analysis are also included in this report. 

2.   SPS Files

Beside the final report, we also provide our client a CD containing : RPS (Receiver), SPS (Shot Point) and XPS (Recording geometry) such that it will make easier for client to "replay" in Mesa software or directly uploaded to surveying software and recording instrument.  If the RPS and SPS are included with real co-ordinate, we can create 3-D seismic lines overlay to topographic map.

We are very grateful to assist you acquiring the best 3-D seismic data acquisition with high precision, high resolution  in acceptable cost.



The Author  :  Tri Satyo - Sr. Geophysicist



NARROW VS WIDE AZIMUTH ON 3D SEISMIC SURVEY

Tri Satyo S.P
Independent Seismic Consultant
For Designing Land 3D Seismic Survey



NARROW VERSUS WIDE AZIMUTH


The distinction between narrow and wide azimuth surveys is made on the basis of the aspect ratio of the recording patch. The aspect ratio is defined as the cross-line dimension of the patch divided by the in-line dimension. Recording patches with an aspect ratio less than 0.5 are considered narrow azimuth, while recording patches with an aspect ratio greater than 0.5 are wide azimuth.


Small-aspect-ratio patches (so-called narrow azimuth) lead to a more even distribution of offsets. However, these patches have, as the name indicates, a limited range of azimuths. Schematically, narrow azimuth surveys have a linear offset distribution with respect to offset similar to 2-D data (Figure-1a); however, when plotted against offset squared, the offset distribution shows bunching at the near offsets (Figure-1b). Narrow azimuth patches are better for AVO and DMO purposes and when significant lateral velocity variations are present (Lansley, 1994).



Fig. 1. Narrow- versus wide-azimuth templates and offset distributions. X offset distance.


Wide-azimuth surveys (i.e., patches that are closer to a square) have a nonlinear offset distribution with respect to x, with a heavy weighting of the far offsets (Figure-1c). However, when plotted against offset squared, the distribution is nearly linear (Figure-1d). Wide-azimuth surveys are better for velocity analysis, multiple attenuation, static solutions, and a more uniform directional sampling of the subsurface. These di-agrams are schematic, and variations in offset distributions may occur in real data.

Comparisons have been made to illustrate differences between narrow and wide azimuth acquisition. Figures-2, 3, and 4 compare a wide-azimuth acquisition consisting of a patch of 12 lines with 60 stations per line in the left column (a, c, e) to a narrow-azimuth acquisition comprised of a patch of 6 lines with 120 stations per line in the right column (b, d, f). The respective aspect ratios are 0.80 and 0.20 based on station spacing of 60 m and receiver line spacing of 240 m.

Since neither the source point density nor the number of receivers in the patch have been changed, the nominal fold for both acquisition strategies (Figures-2a, 2b) is 30 (Figures-2c, 2d). What does change, however, is the configuration of the fold taper, which is much less in the cross-line direction for the narrow azimuth patch (Figure-2d). The fold at an offset limit of 1500 m is significantly lower for the narrow azimuth patch (the fold scale is constant in Figures-2e, 2f)

The comparison of the offset distribution shows that the wide-azimuth patch has traces closer to the source points than the narrow-azimuth patch (Figures-3a, 3b), assuming that the same number of receivers are utilized in the patch. An average trace count of the narrow patch was copied onto the wide-patch display (Figure-3a) with the corrected scaling. The stick diagrams (Figures-3c, 3d) and the offset variation within a box (Figures-3e, 3f) indicate that the offset distribution is better for the wide patch be-cause of the nonlinearity in the source receiver spacing that results from the azimuthal distribution of the receivers. 


An azimuth-dependent trace count shows that there is a more even distribution of source–receiver pairs for the wide patch (Figures-4a, 4b). The azimuth distribution is far more varied for the wide patch than for the narrow patch (Figures-4c, 4d). The rose diagram in Figures-4e and 4f uses color to indicate the multiplicity of the occurrence of a particular source–receiver pair in offset and azimuth distribution (for the entire survey) and shows the focused nature of the narrow-azimuth patch.




Fig. 2. Wide versus narrow patch — template and fold; a. wide-azimuth template, b. narrow-azimuth template, c. wide-azimuth fold distribution at full offsets, d. narrow-azimuth fold distribution at full offsets, e. wide-azimuth fold distribution at 1500 m offsets, and f. narrow-azimuth fold distribution at 1500 m offsets.





















Fig. 3. Wide versus narrow patch — offset distribution; a. wide-azimuth offset distribution — trace count, b. narrow-azimuth offset distribution — trace count, c. wide-azimuth offset distribution — stick diagram, d. narrow-azimuth offset distribution — stick diagram, e. wide-azimuth offset distribution — offset variation within a box, and f. narrow-azimuth offset distribution — offset variation within a box.




Fig. 4. Wide versus narrow patch — azimuth distribution; a. wide-azimuth azimuth distribution — trace count, b. nar-row-azimuth azimuth distribution — trace count, c. wide-azimuth azimuth distribution — spider diagram,d. narrow-az-imuth azimuth distribution — spider diagram, e. wide-azimuth azimuth distribution — rose diagram, and f. narrow-az-imuth azimuth distribution — rose diagram.



85% RULE - ASPECT RATIO

Tri Satyo S.P.
Independent Seismic Consultant
For Designing Land 3D Seismic Survey



85% RULE

Three-dimensional crews often record with more channels on the ground than are necessary. This practice extends the recorded Xmax beyond the required Xmute. Equipment availability should be taken into consideration when the patch size is determined.

If a wide-azimuth survey is desired, one must de-cide on the best aspect ratio for the patch. For the moment, this discussion is restricted to square patches with an aspect ratio of 1.0, meaning that the in-line di-mension equals the cross-line dimension. Consider a circle of unit area (i.e., 1.0) with a radius of Xmute representing the mute zone (large red circle in Figure-1). If the patch lies entirely outside this circle, then 27% of the channels in the patch are being used to record data that will most likely be muted out. While these channels may have some value for longer wave-length refraction analysis, using that many extra channels may be expensive. The recorded Xmax is a factor of 2 larger than the required Xmute.

On the other hand, one can reduce the patch to lie entirely within the mute zone, as shown by the small blue square. Xmax is now measured along the diagonal of the patch, but this patch covers only 64% of the area of the design objective, i.e., the large red circle. This is the other extreme of inefficiency; there are only a few traces that lie at offsets close to the ideal mute distance. The recorded Xmax equals the required Xmute in this case. Some companies select a patch size that equals the large red square in order to record offsets of Xmute in all directions. However, the large red square is twice the area of the small blue square, and there is a significant difference in cost and effort be-tween the two patches.


The 85% Rule is a compromise and determines the aspect ratio of the patch relative to the desired Xmute. The 85% Rule is a simple way to optimize the area of usable traces recorded and the number of channels needed. The rule works as follows (Figure-2):


1.    Determine the desirable Xmute.
2.    Choose the in-line offset Xr to be 0.85 x  Xmute.
3.    Choose the cross-line offset Xs to be 0.85 x Xr = 0.72 x Xmute.

For a real example with Xmute  =    2000 m,

Half in-line dimension
           X = 85% x Xmute  = 1700 m    
Half cross-line dimension
          X  =  85%  x  Xr     =  1445 m
Aspect Ratio
          Xs   /   Xr    =  85%
                                              Fig-1.   Patch dimension Vs  Xmute
The usable area of the patch relative to the circle of Xmute increases from 64% to 78%. 
Only a small part of the patch is outside the theoretical maximum offset Xmute (e.g., for 
a 6-line patch the traces at offsets greater than Xmute are less than 2.5%).     Additional
 receiver lines farther out than indicated by  this  patch  are  mostly  out-side the usable
 offset Xmute. Therefore, the longer  dimension  of  the  patch  is  preferred  to be in the
 in-line  direction.               The  dimensions  may  need  some  slight  adjustment  to  be 
suitable  for  other  considerations  in  the  design  of  the  3-D.       The  recorded  Xmax 
is 1.13 times   the required  Xmute;   most likely the mute affects only t the far extremes 
of the two farthest receiver lines.


                                               Fig-2.  Ideal patch using 85% rule

Referring back to Figure-1, the relationships between the different areas are shown
graphically in Figure-3.  The  red  circle  of  radius  Xmute  has  unit  area  (100% at 
100% Xmute)  and  is  shown as the solid line. The inner blue circle with a radius of
0.71 Xmute  contains  50%  of  the  area  of  the larger circle. If the patch is entirely
within Xmute  (inner  blue  square  in  Figure-1),  then  the  curve describing its area 
deviates from the  y = x2 form at 0.71 Xmute. The area of this smaller blue patch is 
64% of the unit area (red circle).




                               


















      

            Fig-3. Percentage of area covered for various choices of Xmute

On the other hand, if the patch is entirely outside the red circle of Xmute (larger red 
squarein Figure-1), then the curve describing its area deviates from the y = x2 trend 
at 100% Xmute.   The area of  this  larger  patch  is  127%  of the unit area, which is 
twice  the  area  of  the  smaller patch, with its maximum offsets being 141% of the 
mute offset.   Therefore  if  one  lays  out receivers in a square patch that has Xmax 
measured  in  the  in-line  direction, then twice the number of receivers are needed
in comparison to a patch that has Xmax measured along the diagonal.

The patch using the 85% rule covers 78% of the unit area described by the red circle
 of Xmute.  The  green  patch covers an area that is 22% larger than the smaller blue 
square (compare Figure-2). The patch using the 85% rule is an excellent compromise
for the patch  design with the recorded maximum offsets being 113% of the required 
mute zone.   The design provides a sufficient number of large offsets, and only a few 
traces may have to be deleted in the stack.



The author  : Tri Satyo S.P  - Sr. Geophysicist