1. Field of the Invention
The present invention relates to telemetry equipment and methods, and particularly to sonic telemetry apparatus and methods used in the oil and gas industry associated with oil and gas exploration drilling, and in particular with the placement of the borehole in the earth in relatively precise alignment with a reference well or other reference locations.
2. Description of the Related Art
Ranging is the description of a general method whereby a specific measurement technique is used to determine the position of a borehole being drilled relative to a reference such as a surface reference or references or another borehole or set of boreholes. The position of the borehole being ranged specifically relates to the orientation, spacing or separation along all or part of the borehole relative to the reference.
In some drilling circumstances it may be important to determine the relative position of one or more boreholes in order to attain a certain separation and orientation (e.g. river crossing or steam-assisted gravity drainage (SAGD) well pair) or to either seek (e.g. relief well) or avoid (e.g. anti-collision) intersection between boreholes.
Avoiding intersection between boreholes that have been drilled when drilling a new borehole may be required on platforms or in areas that are congested with many previously drilled boreholes.
Achieving intersection between a borehole that has been drilled when drilling a new borehole may be required when a drilling a relief borehole or when linking a new borehole with an existing borehole.
Determining the relative position of a borehole relative to a surface reference in order to attain a certain separation and orientation is important when drilling underground passages such as those for cables or pipelines. These passages may be required to go under mountains, cities, roads, railroads or rivers or similar obstructions.
Determining the relative positions of two or more boreholes in order to attain a certain separation and orientation is important when a steam assisted gravity drainage production technique (SAGD) or similar techniques are used. The SAGD production technique for heavy oil, for example, involves the drilling of an upper and lower borehole pair with boreholes oriented in the same vertical plane and parallel to each other along the entire length of their horizontal sections. Steam that is injected into the upper borehole reduces the viscosity of the heavy hydrocarbons that are contained in the formations surrounding the upper borehole, thereby enabling these hydrocarbons to flow toward the lower borehole as a result of gravity. These hydrocarbons are then produced from the lower borehole using conventional production techniques. In order for the SAGD production technique to be successful, precise directional control must be maintained during the drilling of the borehole pair. Both the orientation and the distance between the boreholes must be precisely achieved. Typical separation distances between upper and lower boreholes are 15 m, with vertical and lateral relative displacements being held preferentially to within 1 m. This relatively precise directional control can be achieved using ranging techniques.
At present the ranging associated with SAGD wells is accomplished with certain magnetic techniques. The various shortcomings of commercial magnetic ranging techniques are discussed below.
The most recent, but so far commercially unproven, magnetic ranging technique requires that the casing in the target well be magnetised at various locations along the wellbore. A magnetic receiver system is installed in the well being ranged and ranging data are transmitted to surface using conventional MWD telemetry.
Existing commercial magnetic ranging techniques typically require the use of a wireline logging system to be deployed in the target well which can either be the injection or producing well. A tractor system is also required to convey the wireline magnetic receiver tool along the horizontal section of this wellbore. Alternatively, a coiled tubing system or a conventional jointed pipe rig can be used to convey the wireline magnetic receiver tool along the high angle sections of wellbore. In all cases the receiver tool must advance along the target wellbore in unison with the progress of the magnetic source in the well being drilled. Depth control must be achieved in both wells. Typical stated accuracy using magnetic ranging is about 100 cm. The present systems for drilling SAGD wells are particularly complex and would benefit in terms of reliability and cost with a simpler system.
The costs associated with the use of existing commercial magnetic ranging techniques include:
The use of such equipment typically costs the producer several million dollars per well, thus showing that cost reduction would be a distinct benefit. Our invention uses a sonic ranging technique that is simpler and less expensive than magnetic ranging techniques, albeit with lesser ranging accuracy. We describe some of its benefits below. Our sonic ranging technique provides a simpler ranging solution in comparison to existing magnetic ranging systems due to the replacement of a tractor, rig or coil tube drilling (CTD) deployed wireline magnetic receiver with a surface deployed sonic transmitter. The sonic receiver is deployed in the bottom hole assembly (BHA) of the well being ranged and ranging data is either sent uphole via a measurement while drilling (MWD) system (also required for measurement of toolface orientation) or processed by a closed loop rotary steering tool (RST) system downhole.
Pertinent ranging techniques can be readily understood by reference to “Understanding GPS: Principles and Applications”, Artech House, 1996, edited by E. D. Kaplan, section 2.1.
The costs associated with the use of the sonic ranging technique include surface source(s) and a sonic downhole receiver and either a surface ranging processing system for ranging data sent uphole via MWD telemetry and a downhole “short hop” or “direct wire” interface between the sonic receiver and the MWD system (if not already in place with standard equipment), or a downhole RST and downhole “short hop” or “direct wire” interface between the sonic receiver and the RST system (if not already in place with standard equipment), thereby leading to a dramatic reduction in equipment cost.
Furthermore the use of a sonic ranging system and a RST allows full closed loop control to be executed downhole without the need for surface processing or control using a directional driller. The accuracy and precision of the sonic ranging system is approximately an order of magnitude less than the magnetic ranging system (which may be accurate to 100 cm). However, this level of accuracy and precision is still acceptable for useable placement of wells such as SAGD well pairs or similar at a significantly lower cost because wellbore placement accurate to ˜1 m is adequate in most instances. Indeed, this accuracy is also acceptable for the placement of single generally horizontal wells such as river crossing or road crossing etc. wells.
It is an object of the present invention to overcome the problems associated with the present state of the art in drilling boreholes that must follow an accurate trajectory as defined by the position from the surface, as presently implemented by a magnetic ranging device. It is a further object of the invention to overcome problems associated with enabling a second borehole to follow an accurate trajectory as defined by the first, again as defined by the position from the surface, and also as presently implemented by a magnetic ranging device.
In order to clarify the method and means we present to outline of some of the invention's applications and then go on to describe the specific means by which the invention can be implemented.
According to one aspect of the invention, a set of sonic transmitters deployed at the surface substantially above and along the intended path of first well of a borehole is used to provide a ranging means to a sonic receiver disposed in the bottom hole assembly of drilling equipment, the receiver being preferentially placed close to the drill bit. The sonic energy received from the surface is processed and ranging data is subsequently sent back to the drilling rig by conventional methods where it is decoded and further processed in order to provide the driller a profile of the wellbore being drilled. In one embodiment this profile is in effect replicated and then modified to provide information on the offset profile to be ideally taken for a second borehole to be drilled, the application being a second well of use in SAGD applications or similar. In this embodiment drilling the second well proceeds by the process as briefly described above being repeated with the received telemetry data being compared to the idealized profile using a processor or other devices capable of making comparisons of received data. Discrepancies between the ideal and the actual profile are used by the directional driller in order to correct the second borehole well and steer it substantially along the intended path.
In one aspect of the invention the sonic transmitters are deployed in regular repeating patterns, such as contiguous squares or rectangles, with their positions being accurately known via means such as surveying or deduced by the global positioning system. The individual transmitters in each square or similar configuration are firmly anchored using such means as rig anchors or screw piles into the consolidated formation below, thus enabling sonic energy to be produced locally in the well's environment. Each grouping of sonic transmitters is individually or severally activated to produce a modulated energy carrier such that the downhole receiver is able to deduce the relative time of flight existing between each transmitter. In one embodiment this information is telemetered back to the surface where it is processed with the additional location information of the appropriate transmitters, thus forming a set of simultaneous equations that can be solved to produce the most likely three-dimensional position of the receiver. This calculation is not unlike that by which simple global positioning system (GPS) location finding is achieved. In our case we initially assume the sonic time of flight is governed not only by distance but a generally isotropic speed of sound within the formation between surface and the subsurface borehole. Typical speeds range from 2500 to 3000 msec. To carry the analogy further, our sets of spaced sonic transmitters are equivalent to the constellation of GPS satellites, and the sonic receiver is equivalent to a passive GPS receiver.
To a first approximation the sonic transmitters act like point energy sources transmitting isotropically into the ground. This assumption is modified in yet another aspect of the invention by incorporating into each transmitter a beam-steering capability in order to efficiently send as much sonic energy as possible to the estimated location of the downhole receiver. As drilling proceeds the transmitters are included in a near real time closed loop system that keeps their sonic beams actively pacing the downhole drill receiver, thus enhancing the receiver's signal to noise ratio (SNR).
In a another embodiment whereby the second borehole is substantially steered by an RST or similar, the RST is equipped with appropriate sensing, decoding and processing device, such as a processor, to detect the sonic transmissions from the surface. This capability is particularly useful in that the RST can be configured to drill the second borehole offset from the first and thus has the information necessary to provide automatic course corrections without the need for a directional driller to implement course changes that would otherwise be required.
In yet another embodiment the surface sonic transmitters are replaced by surface sonic receivers (such as geophones arranged in a grid pattern) and with the downhole sonic receiver being replaced by a sonic transmitter deployed in the BHA, preferably in a manner that transfers sonic energy to the drill bit and hence into the formation. Alternatively the sonic transmitter may also transfer sonic energy into the formation by means such as the axial stabilizers that are often used to steer an RST.
The following drawings illustrate the principles of the present invention and an exemplary embodiment thereof:
The present embodiment(s) seeks to overcome non-optimal design constraints in the complexity and cost of magnetic ranging techniques in use today that are used to place single or pairs of boreholes. Our sonic ranging invention utilizes time of flight (TOF) ranging techniques that are presently unknown in the drilling industry.
It is well understood that the time of arrival (TOA) of a signal traveling from a source at a known location to a receiver can be used to calculate time of flight and hence the distance traveled by the signal through a known medium. When more than one source is used, an estimate of the location of the receiver can be made based on the TOF for each of the sources and the geometry of the sources, in effect utilizing a differential TOF (DTOF). Although the practical implementation of DTOF will be obvious to one skilled in the art we provide here a simplified analysis that uses a more commonly understood term—time differential of arrival (TDOA) as it pertains to multilateration, or a ranging technique that depends on the detection of several signals in order to ascertain position. For ease of understanding and clarity we use an example that is commonly used in civil and military surveillance applications to accurately locate aircraft, vehicles or stationary emitters by measuring the time difference of arrival of a signal from an emitter at three or more receiver sites, although it is to be understood that in our embodiments we use the reciprocal case.
Consider a single emitter and two receivers; if a sonic wave is emitted from a surface position it will arrive at slightly different times at two spatially separated subsurface receiver sites, the TDOA being due to the different distances of each receiver from the emitter. For a given location of each of the two receivers a multiplicity of emitter locations would give the same measurement of TDOA. Given two receiver locations and a known TDOA the locus of possible emitter locations is a one half of a two-sheeted hyperboloid i.e. a three-dimensional hyperbola. Note that the receivers do not need require the absolute time at which the wave was transmitted to solve the location equations—only the time difference is needed.
Consider now a third receiver at a third subsurface location. This would provide a second TDOA measurement and hence locate the emitter on a second hyperboloid. The intersection of these two hyperboloids describes a curve on which the emitter is expected to lie. If a fourth receiver is introduced a third TDOA measurement is available and the intersection of the resulting third hyperboloid with the curve already found with the other three receivers defines a unique point in space. The emitter's location is therefore fully determined in three dimensions.
Errors in the measurement of the time of arrival of pulses mean that enhanced accuracy can be obtained with more than four receivers. In general N receivers provide N−1 hyperboloids. Assuming a perfect model and measurements with N>4 receivers the N−1 hyperboloids would intersect at a single point. In reality the surfaces rarely intersect because of errors due to the non-homogeneity of the formation through which the waves travel. Furthermore the stratification of typical formations and differing transit paths that are utilized by the sonic waves can lead to variations in TDOA measurements, thereby increasing positional error. Of course there are many causes of error that would have to be accounted for arriving at a position estimation, as would be known to one reasonably skilled in the art. In our environment the location solution could be thought of as an optimization problem and solved using a least squares method, an extended Kalman filter technique or in addition the TDOA of multiple transmitted pulses from the emitter may be averaged to improve accuracy, to name but three examples.
The basic equations of our multilateration example are as follows: let the emitter be placed at an unknown location (x,y,z) that we wish to locate. Consider also a multilateration system comprising four receiver sites (L, R, Q, C) at known locations. The travel time (TL) of pulses from the emitter at (x,y,z) to each of the receiver locations at (xL,yL,zL) for example, is simply the distance divided by the speed of sound within the formation c (meters/second):
If the site C is taken to be at the coordinate system origin, we have
The time difference of arrival between pulses arriving directly at site C, for example, and the other sites are:
where (xL, yL, zL) is the location of receiver site L, etc. Each equation defines a separate hyperboloid. The multilateration system solves for the unknown target location (x,y,z), all the other parameters being known.
Multilateration can also be used by a single receiver to help locate itself by measuring the TDOA of signals emitted from three or more synchronized transmitters at known locations (the ‘reciprocal case’).
Now moving on to a more specific horizontal drilling environment, in one embodiment we implement a series of surface sonic transmitters disposed along a planned borehole trajectory.
The receiver as indicated in
In order to estimate the TOF of a waveform we transmit a signal modulated by a pseudo-noise code with desirable autocorrelation and cross correlation characteristics. The transmission of the signal is synchronized to the system clock such that the start time of the transmission is known. The TOA of the signal is then determined by finding the autocorrelation peak of the received signal and comparing the arrival time with the known start of the transmission.
As an example that is intended to clarify our method, consider the case of a signal modulating a sonic carrier traveling through a lossless medium at a speed of v=2500 m/sec. A 7 bit Barker code (1 1 1 −1 −1 1 −1) may be chosen as the pseudo-noise code due to its attractive autocorrelation characteristics as shown in
All seven bits of the code are transmitted at t=0. At t=Δ the signal is arrives at the receiver and is correlated with the receiver's reference waveform. The time of arrival is determined by the time positions of the maximum of the cross-correlation between the reference and received waveforms. Assuming that the receiver has been adequately synchronized with the transmitter the TOF can be calculated using the known sound velocity in the medium, as shown in
The time domain resolution of the calculation of the time of flight, and hence the spatial resolution, is determined by the bit rate of the code. If a spatial accuracy of 1 meter is required for the example, then the correlation peak must be determined within a single bit period of a maximum duration of 400 μsec. This requires a minimum bit rate of 2500 bits per second. Since the sonic carrier for the system is at 2500 Hz, the system may be considered broadband with impacts on the receiver noise bandwidth and SNR.
A more desirable solution is one which maintains the spatial resolution but with a narrower receiver bandwidth requirement. One implementation that accomplishes this is to modulate the pseudo-random code onto a series of sonic packets, such as linear chirps (i.e. a substantially sinusoidal waveform that sweeps linearly from one frequency to another) or a simpler frequency modulated sweep, such that these energy packets are transmitted at a much lower rate than the minimum bit rate. The received waveform is sampled at a high enough rate to ensure that the spatial resolution is achieved. For exemplary purposes, consider the advantage of using chirps because the shape of the autocorrelation waveform can be easily modified by increasing the time/frequency product of the component chirps. For example, the time frequency product X for a linear chirp can be defined as:
X=aT2
where ‘a’ is the frequency range of the linear chirp and T is the duration of the chirp. A typical low frequency sonic chirp (less than 1000 Hz average frequency) would, with suitable parameters as could be assumed by those skilled in the art may produce a time/frequency product of less than 0.1. Simply by increasing the frequency span of the linear chirps by a factor of five results in an improved time/frequency product of greater than 0.6. A comparison of the resulting autocorrelation waveforms at Fs=8000 samples per second is in given in
Examination of
Turning now to the mechanical systems and methods by which sonic energy may be transmitted into the subsurface formations, we cover some of the exemplary embodiments that enable accurate wellbore placement and control within the scope of our invention.
The amplitude of the sonic output generated by this transducer can be determined from the axial force, the applied potential and the strain as follows:
where the parameters have their conventional meanings.
Extensional waves produced by the source travel at a bar wave speed Cb of:
where E=Young's modulus, ρ=density
and has a particle velocity v equal to:
where F=force, Z=impedance
The extensional wave travelling up and away from the earth formation enters the reflector section 81 and travels as a bar wave. The wave is reflected by the free end of the reflector, reverses direction and combines with the downward travelling wave emitting from the PZT transducer. The separation distance between the transducer and the free end controls the phase relationship of the wave superposition, and is chosen such that the waves superimpose constructively, effectively doubling the amplitude. Such transducer/reflectors topographies are known to the art of ultrasonic transducers for non-destructive testing, medical and other applications.
The sonic energy is conveyed to the earth formations through a screw pile 82 adapted for sonic use. Screw piles are well known to the art of structural foundation design, as a means to quickly and economically insert piles into soft ground for the purpose of supporting the enormous weight of buildings constructed thereupon. Their ability to be driven to great depths and their large axial load capacity make them an ideal sonic transmitter earth interface. The screw pile is driven down into the desired earth formation by twisting the tube via surface equipment causing the screw portion 83 to pull the pile downward. Extensional waves travelling downward along the pile are converted into pressure waves (P-waves) in the earth formations by the axially exposed surface area of the screw portion and the end of the tube. This mode conversion causes an increase in the impedance encountered by the extensional waves. The combined bar wave and P-wave impedance at this interface is determined as follows:
ZINTERFACE=ρBARCBARABAR+ρEARTHCEARTHABEARING
where
Taking the soil density in the Athabasca oilsands deposits of 2080 kg/m^3 as exemplary, the oilsand P-wave velocities are in the order of 2500 msec. This now enables the impedance of the soil transducer interface to be easily determined.
Considering that the sonic impedance at the interface is greater than that of the tube section of the pile, without a critical modification much of the sonic energy would be reflected back upwards and not transmitted into the earth material. This inventive modification is the inclusion of an impedance matching transformer 84 immediately above the screw section 83 of the pile. With such a feature included the sonic energy is transmitted from one medium to the other without reflection. In this preferred embodiment an impedance match between the tube impedance and interface impedance is accomplished via a quarter wave transformer, fashioned as a section one-quarter wavelength in length with a sonic impedance determined as follows:
ZQW
Invariably the sonic impedance of the tube section of the screw pile 82 differs from that of the PZT transducer 80. To prevent a deleterious reflection between these sections an impedance matching transformer 85 is placed in between said transducer and said screw pile.
Assuming a lossless system, the particle velocity at the soil interface can be easily determined by equating the sonic energy produced at the source to the sonic energy at the interface:
E=Zbarvbar2=Zsoilvsoil2
Alternatively, the sonic efficiency of this transmitter can be determined by calculating the transmitted energy at each impedance change from the PZT to the soil interface, and the true particle velocity at the interface can be determined using the above relationship.
Once transmitted into the earth formations, the signal will propagate as P-waves emanating from a point source. Therefore the signal will geometrically attenuate according to a 1/R2 relationship. In addition the signal will attenuate due to internal friction within the earth materials producing small amounts of heat. The extent of material attenuation can be determined with suitably designed field measurements.
Another embodiment of the invention involves replacing the sonic screw pile altogether with a simple end plate
The embodiment of
The sonic transformers 101 presented above provide an effective impedance match for a specific frequency.
As an alternative embodiment to the PZT sandwich transducer, extensional sonic waves may be generated using an electromagnetic axial force transducer, as depicted in
Another alternative embodiment to the PZT sandwich transducer involves the implementation of a hydraulic axial force transducer
In an alternative embodiment the location of the sonic transmitter and receiver is reversed. Using
One such embodiment, shown in
Yet another embodiment emits the sonic energy in a radial direction from the well bore
Another embodiment that emits sonic energy in a radial direction involves the implementation of a radially deforming PZT sandwich transducer as shown in
Another embodiment that emits sonic energy in a radial direction is shown in
It is to be understood that while certain aspects of the disclosed subject matter have been shown and described, the disclosed subject matter is not limited thereto and encompasses various other embodiments and aspects. The above-mentioned steps and components are not meant to limit the use or organization of the present invention. The steps for performing the method may be performed in any logical method and the process can be used for other types of image-matching processes when viable.
This application claims priority in U.S. Provisional Patent Application No. 61/152,003, filed Feb. 12, 2009, which is incorporated herein by reference.
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