Method and apparatus for transmitting information to the surface from a drill string down hole in a well

Information

  • Patent Grant
  • 6714138
  • Patent Number
    6,714,138
  • Date Filed
    Friday, September 29, 2000
    24 years ago
  • Date Issued
    Tuesday, March 30, 2004
    20 years ago
Abstract
A method and apparatus for transmitting information to the surface from down hole in a well in which a pulser is incorporated into the bottom hole assembly of a drill string that generates pressure pulses encoded to contain information concerning the drilling operation. The pressure pulses travel to the surface where they are decoded so as to decipher the information. The pulser includes a stator forming passages through which drilling fluid flows on its way to the drill bit. The rotor has blades that obstruct the flow of drilling fluid through the passages when the rotor is rotated into a first orientation and that relieve the obstruction when rotated into a second orientation, so that oscillation of the rotor generates the encoded pressure pulses. An electric motor, under the operation of a controller, drives a drive train that oscillates the rotor between the first and second orientations. The electric motor is located in an air-filled chamber whereas the major portion of the drive train is located in a liquid-filled chamber. The controller controls one or more characteristics of the pressure pulses by varying the oscillation of the rotor. The controller may receive information concerning the characteristics of the pressure pulses from a pressure sensor mounted proximate the bottom hole assembly, as well as information concerning the angular orientation of the rotor by means of an encoder. The controller may also receive instructions for controlling the pressure pulse characteristic from the surface by means of encoded pressure pulses transmitted to the pulser from the surface that are sensed by the pressure sensor and decoded by the controller.
Description




FIELD OF THE INVENTION




The current invention is directed to a method and apparatus for transmitting information from a down hole location in a well to the surface, such as that used in a mud pulse telemetry system employed in a drill string for drilling an oil well.




BACKGROUND OF THE INVENTION




In underground drilling, such as gas, oil or geothermal drilling, a bore is drilled through a formation deep in the earth. Such bores are formed by connecting a drill bit to sections of long pipe, referred to as a “drill pipe,” so as to form an assembly commonly referred to as a “drill string” that extends from the surface to the bottom of the bore. The drill bit is rotated so that it advances into the earth, thereby forming the bore. In rotary drilling, the drill bit is rotated by rotating the drill string at the surface. In directional drilling, the drill bit is rotated by a down hole mud motor coupled to the drill bit; the remainder of the drill string is not rotated during drilling. In a steerable drill string, the mud motor is bent at a slight angle to the centerline of the drill bit so as to create a side force that directs the path of the drill bit away from a straight line. In any event, in order to lubricate the drill bit and flush cuttings from its path, piston operated pumps on the surface pump a high pressure fluid, referred to as “drilling mud,” through an internal passage in the drill string and out through the drill bit. The drilling mud then flows to the surface through the annular passage formed between the drill string and the surface of the bore.




Depending on the drilling operation, the pressure of the drilling mud flowing through the drill string will typically be between 1,000 and 25,000 psi. In addition, there is a large pressure drop at the drill bit so that the pressure of the drilling mud flowing outside the drill string is considerably less than that flowing inside the drill string. Thus, the components within the drill string are subject to large pressure forces. In addition, the components of the drill string are also subjected to wear and abrasion from drilling mud, as well as the vibration of the drill string.




The distal end of a drill string, which includes the drill bit, is referred to as the “bottom hole assembly.” In “measurement while drilling” (MWD) applications, sensing modules in the bottom hole assembly provide information concerning the direction of the drilling. This information can be used, for example, to control the direction in which the drill bit advances in a steerable drill string. Such sensors may include a magnetometer to sense azimuth and accelerometers to sense inclination and tool face.




Historically, information concerning the conditions in the well, such as information about the formation being drill through, was obtained by stopping drilling, removing the drill string, and lowering sensors into the bore using a wire line cable, which were then retrieved after the measurements had been taken. This approach was known as wire line logging. More recently, sensing modules have been incorporated into the bottom hole assembly to provide the drill operator with essentially real time information concerning one or more aspects of the drilling operation as the drilling progresses. In “logging while drilling” (LWD) applications, the drilling aspects about which information is supplied comprise characteristics of the formation being drilled through. For example, resistivity sensors may be used to transmit, and then receive, high frequency wavelength signals (e.g., electromagnetic waves) that travel through the formation surrounding the sensor. By comparing the transmitted and received signals, information can be determined concerning the nature of the formation through which the signal traveled, such as whether it contains water or hydrocarbons. Other sensors are used in conjunction with magnetic resonance imaging (MRI). Still other sensors include gamma scintillators, which are used to determine the natural radioactivity of the formation, and nuclear detectors, which are used to determine the porosity and density of the formation.




In traditional LWD and MWD systems, electrical power was supplied by a turbine driven by the mud flow. More recently, battery modules have been developed that are incorporated into the bottom hole assembly to provide electrical power.




In both LWD and MWD systems, the information collected by the sensors must be transmitted to the surface, where it can be analyzed. Such data transmission is typically accomplished using a technique referred to as “mud pulse telemetry.” In a mud pulse telemetry system, signals from the sensor modules are typically received and processed in a microprocessor-based data encoder of the bottom hole assembly, which digitally encodes the sensor data. A controller in the control module then actuates a pulser, also incorporated into the bottom hole assembly, that generates pressure pulses within the flow of drilling mud that contain the encoded information. The pressure pulses are defined by a variety of characteristics, including amplitude (the difference between the maximum and minimum values of the pressure), duration (the time interval during which the pressure is increased), shape, and frequency (the number of pulses per unit time). Various encoding systems have been developed using one or more pressure pulse characteristics to represent binary data (i.e., bit


1


or


0


)—for example, a pressure pulse of 0.5 second duration represents binary 1, while a pressure pulse of 1.0 second duration represents binary 0. The pressure pulses travel up the column of drilling mud flowing down to the drill bit, where they are sensed by a strain gage based pressure transducer. The data from the pressure transducers are then decoded and analyzed by the drill rig operating personnel.




Various techniques have been attempted for generating the pressure pulses in the drilling mud. One technique involves the use of axially reciprocating valves, such as that disclosed in U.S. Pat. Nos. 3,958,217 (Spinnler); 3,713,089 (Clacomb); and 3,737,843 (Le Peuvedic et al.), each of which is hereby incorporated by reference in its entirety. Another technique involves the use of rotary pursers. Typically, rotary pulsers utilizes a rotor in conjunction with a stator. The stator has vanes that form passages through which the drilling mud flows. The rotor has blades that, when aligned with stator passages, restrict the flow of drilling mud, thereby resulting in an increase in drilling mud pressure, and, when not so aligned, eliminate the restriction. Rotation of the rotor is driven by the flow of drilling mud or an electric motor powered by a battery. Typically, the motor is a brushless DC motor mounted in an oil-filled chamber pressurized to a pressure close to that of the drilling mud to minimize the pressure gradient acting on the housing enclosing the motor.




In one type of rotary pulser, sometimes referred to as a “turbine” or “siren,” the rotor rotates more or less continuously so as to create an acoustic carrier signal within the drilling mud. A siren type rotary pulser is disclosed in U.S. Pat. Nos. 3,770,006 (Sexton et al.) and 4,785,300 (Chin et al.), each of which is hereby incorporated by reference in their entirety. Encoding can be accomplished based on shifting the phase of the acoustic signal relative to a reference signal—for example, a shift in phase may represent one binary bit (e.g., 1), while the absence of a phase shift may indicate another bit (e.g., 0).




In another type of rotary pulser, in which the rotor is typically driven by the mud flow, the rotor increments in discrete intervals. Operation of a latching or escapement mechanism, for example by means of an electrically operated solenoid, may be used to actuate the incremental rotation of the rotor into an orientation in which its blades block the stator passages, thereby resulting in an increase in drilling mud pressure that may be sensed at the surface. The next incremental rotation unblocks the stator passages, thereby resulting in a reduction in drilling mud pressure that may likewise be sensed at the surface. Thus, the incremental rotation of the rotor creates pressure pulses that are transmitted to the surface detector. A rotary pulser of this type is disclosed in U.S. Pat. No. 4,914,637 (Goodsman), incorporated by reference herein in its entirety.




Unfortunately, conventional rotary pulsers suffer from disadvantages that result from the fact that the characteristics of the pressure pulses cannot be adequately controlled in situ to optimize the transmission of information. For example, under any given mud flow situation, each increment of the rotor of an incremental type rotary pulser will result in a constant amplitude pressure pulses being generated at the pulser. As the drilling progresses, the distance between the pulser and the surface detector increases, thereby resulting in increased attenuation of the pressure pulses by the time they reach the surface. This can make it more difficult for the pressure pulses to be detected at the surface. Moreover, from time to time, extraneous pressure pulses from other sources, such as mud pumps, may become more pronounced or may occur at a frequency closer to that of the pressure pulses containing the data to be transmitted, making data acquisition by the surface detection system more difficult. In such situations, data transmission could be improved by increasing the amplitude or varying the frequency or even the shape of the pressure pulses generated by the pulser.




In prior art systems, such situations can only be remedied by removing the pulser, which requires cessation of drilling and withdrawal of the drill string from the well so that physical adjustments can be made to the pulser, for example, mechanically increasing the size of the rotor increment so as to increase the amplitude and duration of the pulses, or adjusting the motor control to alter the pulser speed.




Note that although increasing the magnitude of the rotor increment will increase the duration, and often the amplitude, of the pressure pulses, it will also increase the time necessary to create the pulse, thereby reducing the data transmission rate. Thus, optimal performance will not be obtained by generating pressure pulses of greater than necessary duration or amplitude, and there are some situations in which it may be desirable to decrease the amplitude of the pressure pulses as the drilling progresses. Current systems, however, do not permit such optimization of the data transmission rate.




Conventional pulsers suffer from other disadvantages as well. For example, due to the high pressure of the drilling mud, rotary seals between the rotor shaft and the stationary components are subject to leakage. Moreover, the brushless DC motors used to drive the rotor consume relatively large amounts of power, limiting battery life. While brushed DC motors consume less power, they cannot be used in an oil-filled pulser housing of the type typically used in an MWD/LWD system.




Consequently, it would be desirable to provide a method and apparatus for generating pressure pulses in a mud pulse telemetry system in which one or more characteristics of the pressure pulses generated at the pulser could be adjusted in situ at the down hole location—that is, without withdrawing the drill sting from the well. It would also be desirable to provide a pulser having a durable seal that was resistant to leakage and powered by a low power consuming brushed DC motor.




SUMMARY OF THE INVENTION




It is an object of the current invention to provide an improved method of transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth. This and other objects are achieved in a method of transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth comprising the steps of (i) generating pressure pulses in the drilling fluid flowing through the drill string that are encoded to contain the information to be transmitted, and (ii) controlling a characteristic of the pressure pulses, such as amplitude, duration, frequency, or phase, in situ at the down hole location.




In one embodiment, the method comprises the steps of (i) directing drilling fluid along a flow path extending through the down hole portion of the drill string, (ii) directing the drilling fluid over a rotor disposed in the down hole portion of the drill string, the rotor capable of at least partially obstructing the flow of fluid through the flow path by rotating in a first direction and of thereafter reducing the obstruction of the flow path by rotating in an opposite direction, (iii) creating pressure pulses encoded to contain the information in the drilling fluid that propagate toward the surface location, each of the pressure pulses created by oscillating the rotor by rotating the rotor in the first direction through an angle of rotation so as to obstruct the flow path and then reversing the direction of rotation and rotating the rotor in the opposite direction so as to reduce the obstruction of the flow path, and (iv) making an adjustment to at least one characteristic of the pressure pulses by adjusting the oscillation of the rotor, the adjustment of the oscillation of the rotor performed in situ at the down hole location.




In a preferred embodiment, the method includes the step of transmitting instructional information from the surface to the down hole location for controlling the pressure pulse characteristic. In one embodiment, the instructional information is transmitted by generating pressure pulses at the surface and transmitting them to the down hole location where they are sensed by a pressure sensor and deciphered.




The invention also encompasses an apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, the drill string having a passage through which a drilling fluid flows, comprising (i) a housing for mounting in the drill string passage, first and second chambers formed in the housing, the first and second chambers being separated from each other, the first chamber filled with a gas, the second chamber filled with a liquid, (ii) a rotor capable of at least partially obstructing the flow of the drilling fluid through the passage when rotated into a first angular orientation and of reducing the obstruction when rotated into a second angular orientation, whereby rotation of the rotor creates pressure pulses in the drilling fluid, (iii) a drive train for rotating the rotor, at least a first portion of the drive train located in the liquid filled second chamber, (iv) an electric motor for driving rotation of the drive train, the electric motor located in the gas-filled first chamber.




In a preferred embodiment, the apparatus also includes a stator in which the passage is formed. A seal is fixedly attached at one end to the rotor and at the other end to the stator, so that the seal undergoes torsional deflection as the rotor oscillates. The clearance between the rotor and stator is tapered so as to prevent jamming by debris in the drilling fluid.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a diagram, partially schematic, showing a drilling operation employing the mud pulse telemetry system of the current invention.




FIG.


1


(


a


) is a graph showing the amplitude and shape of the pressure pulses in the drilling fluid as-generated at the pulser (lower curve) and as-received at the surface pressure sensor.





FIG. 2

is a schematic diagram of a mud pulser telemetry system according to the current invention.





FIG. 3

is a diagram, partially schematic, of the mechanical arrangement of a pulser according to the current invention.





FIGS. 4-6

are consecutive portions of a longitudinal cross-section through a portion of the bottom hole assembly of the drill string shown in

FIG. 1

incorporating the pulser shown in FIG.


3


.





FIG. 7

is a transverse cross-section taken through line VII—VII shown in

FIG. 4

, showing the pressure compensation system.





FIG. 8

is a detailed view of the portion of the pulser shown in

FIG. 5

in the vicinity of the magnetic coupling.





FIG. 9

is a transverse cross-section taken through line IX—IX shown in

FIG. 6

, showing the pressure sensor.




FIG.


9


(


a


) is an exploded, isometric view of the pressure sensor shown in FIG.


9


.





FIG. 10

is a transverse cross-section taken through line X—X shown in

FIG. 4

, showing the stator.





FIG. 11

is a transverse cross-section taken through line XI—XI shown in

FIG. 4

, showing the rotor and stator.





FIG. 12

is a longitudinal cross-section taken through line XII—XII shown in

FIG. 11

showing the rotor and stator.





FIG. 13

is a cross-section taken along line XIII—XIII shown in

FIG. 12

showing portions of the rotor and stator.




FIG.


13


(


a


) is a view similar to

FIG. 13

showing an alternate embodiment of the rotor blade shown in FIG.


13


.




FIGS.


14


(


a


) and (


b


) are isometric views of two embodiments of the seal shown in FIG.


12


.




FIGS.


15


(


a


)-(


c


) show the rotor in three orientations relative to the stator.





FIG. 16

is a graph showing the timing relationship of the electrical power e transmitted from the motor driver to the motor (lower curve) to the angular orientation of the rotor θ (middle curve) and the resulting pressure pulse ΔP generated at the pulser (upper curve).











DESCRIPTION OF THE PREFERRED EMBODIMENT




A drilling operation incorporating a mud pulse telemetry system according to the current invention is shown in

FIG. 1. A

drill bit


2


drills a bore hole


4


into a formation


5


. The drill bit


2


is attached to a drill sting


6


that, as is conventional, is formed of sections of piping joined together. As is also conventional, a mud pump


16


pumps drilling mud


18


downward through the drill string


6


and into the drill bit


2


. The drilling mud


18


flows upward to the surface through the annular passage between the bore


4


and the drill string


6


, where, after cleaning, it is recirculated back down the drill string by the mud pump


16


. As is conventional in MWD and LWD systems, sensors


8


, such as those of the types discussed above, are located in the bottom hole assembly portion


7


of the drill string


6


. In addition, a surface pressure sensor


20


, which may be a transducer, senses pressure pulses in the drilling mud


18


. According to a preferred embodiment of the invention, a pulser device


22


, such as a valve, is located at the surface and is capable of generating pressure pulses in the drilling mud.




As shown in

FIGS. 1 and 2

, in addition to the sensors


8


, the components of the mud pulse telemetry system according to the current invention include a conventional mud telemetry data encoder


24


, a power supply


14


, which may be a battery or turbine alternator, and a down hole pulser


12


according to the current invention. The pulser comprises a controller


26


, which may be a microprocessor, a motor driver


30


, which includes a switching device


40


, a reversible motor


32


, a reduction gear


44


, a rotor


36


and stator


38


. The motor driver


30


, which may be a current limited power stage comprised of transistors (FET's and bipolar), preferably receives power from the power supply


14


and directs it to the motor


32


using pulse width modulation. Preferably, the motor is a brushed DC motor with an operating speed of at least about 600 RPM and, preferably, about 6000 RPM. The motor


32


drives the reduction gear


44


, which is coupled to the rotor shaft


34


. Although only one reduction gear


44


is shown, it should be understood that two or more reduction gears could also be utilized. Preferably, the reduction gear


44


achieves a speed reduction of at least about 144:1. The sensors


8


receive information


100


useful in connection with the drilling operation and provide output signals


102


to the data encoder


24


. Using techniques well known in the art, the data encoder


24


transforms the output from the sensors


8


into a digital code


104


that it transmits to the controller


26


. Based on the digital code


104


, the controller


26


directs control signals


106


to the motor driver


30


. The motor driver


30


receives power


107


from the power source


14


and directs power


108


to a switching device


40


. The switching device


40


transmits power


111


to the appropriate windings of the motor


32


so as to effect rotation of the rotor


36


in either a first (e.g., clockwise) or opposite (e.g., counterclockwise) direction so as to generate pressure pulses


112


that are transmitted through the drilling mud


18


. The pressure pulses


112


are sensed by the sensor


20


at the surface and the information is decoded and directed to a data acquisition system


42


for further processing, as is conventional. As shown in FIG.


1


(


a


), the pressure pulses


112


generated at the down hole pulser


12


have an amplitude “a”. However, since the down hole pulser


12


may be as much as 5 miles from the surface, as a result of attenuation, the amplitude of the pressure pulses when they arrive at the surface will be only a′. In addition, the shape of the pulses may be less distinct and noise may be superimposed on the pulses.




Preferably, a down hole static pressure sensor


29


is incorporated into the drill string to measure the pressure of the drilling mud in the vicinity of the pulser


12


. As shown in

FIG. 2

, the static pressure sensor


29


, which may be a strain gage type transducer, transmits a signal


105


to the controller


26


containing information on the static pressure. As is well known in the art, the static pressure sensor


29


may be incorporated into the drill collar of the drill bit


2


. However, the static pressure sensor


29


could also be incorporated into the down hole pulser


12


.




In a preferred embodiment of the invention, the down hole pulser


12


also includes a down hole dynamic pressure sensor


28


that senses pressure pulsations in the drilling mud


18


in the vicinity of the pulser


12


. The pressure pulsations sensed by the sensor


28


may be the pressure pulses generated by the down hole pulser


12


or the pressure pulses generated by the surface pulser


22


. In either case, the down hole dynamic pressure sensor


28


transmits a signal


115


to the controller


26


containing the pressure pulse information, which may be used by the controller in generating the motor control signals


106


. The down hole pulser


12


may also include an orientation encoder


24


suitable for high temperature applications, coupled to the motor


32


. The orientation encoder


44


directs a signal


114


to the controller


26


containing information concerning the angular orientation of the rotor


36


, which may also be used by the controller in generating the motor control signals


106


. Preferably, the orientation encoder


44


is of the type employing a magnet coupled to the motor shaft that rotates within a stationary housing in which Hall effect sensors are mounted that detect rotation of the magnetic poles.




A preferred mechanical arrangement of the down hole pulser


12


is shown schematically in

FIG. 3

mounted in a section of drill pipe


64


forming a portion of the bottom hole assembly


7


of the drill string


6


. The drill pipe


64


forms a central passage


62


through which the drilling mud


18


flows on its way down hold to the drill bit


2


. The rotor


36


is preferably located upstream of a stator


38


, which includes a collar portion


39


supported in the drill pipe


64


. The rotor


36


is driven by a drive train mounted in a pulser housing. The pulser housing is comprised of housing portions


66


,


68


, and


69


. The rotor


36


includes a rotor shaft


34


mounted on upstream and downstream bearings


56


and


58


in a chamber


63


. The chamber


63


is formed by upstream and downstream housing portions


66


and


68


together with a seal


60


and a barrier member


110


(as used herein, the terms upstream and downstream refer to the flow of drilling mud toward the drill bit). The chamber


63


is filled with a liquid, preferably a lubricating oil, that is pressurized to an internal pressure that is close to that of the external pressure of the drilling mud


18


by a piston


162


mounted in the upstream oil-filed housing portion


66


.




The rotor shaft


34


is coupled to the reduction gear


46


, which may be a planetary type gear train, such as that available from Micromo, of Clearwater, Fla., and which is also mounted in the downstream oil-filled housing portion


68


. The input shaft


113


to the reduction gear


46


is supported by a bearing


54


and is coupled to inner half


52


of a magnetic coupling


48


, such as that available through Ugimag, of Valparaiso, Ind. The outer half


50


of the magnetic coupling


48


is mounted within housing portion


69


, which forms a chamber


65


that is filled with a gas, preferably air, the chambers


63


and


65


being separated by the barrier


110


. The outer magnetic coupling half


50


is coupled to a shaft


94


which is supported on bearings


55


. A flexible coupling


90


couples the shaft


94


to the electric motor


32


, which rotates the drive train. The orientation encoder


44


is coupled to the motor


32


. The down hole dynamic pressure sensor


28


is mounted on the drill pipe


64


.




In operation, the motor


32


rotates the shaft


94


which, via the magnetic coupling


48


, transmits torque through the housing barrier


110


that drives the reduction gear input shaft


113


. The reduction gear drives the rotor shaft


34


, thereby rotating the rotor


36


.




Pressurizing the chamber


63


with oil to a pressure close to that of the drilling mud


18


reduces the likelihood of drilling mud


18


leaking into the chamber


63


. In addition, it reduces the forces imposed on the housings portions


66


and


68


, which are subject to erosion. Moreover, as discussed further below, in a preferred embodiment of the invention, a novel flexible seal


60


seals between the rotor


36


and the stator


38


at the upstream end of the housing portion


66


to further prevent leakage.




According to one aspect of the current invention, although the rotor


32


and reduction gear


46


are mounted in the oil-filled chamber


63


, the motor


32


is mounted in the air filled chamber


65


, which is maintained at atmospheric pressure. This allows the use of a brushed reversible DC motor, which is capable of the high efficiency and high motor speeds preferably used according to the current invention. This high efficiency results in consumption of relatively little power, thereby conserving the battery


14


. The high speed allows a faster data transmission rate. It also results in a motor drive train with high resistance to rotation which, as discussed below, permits the rotor to maintain its orientation without the use of mechanical stops. Moreover, the use of the magnetic coupling


48


allows the motor


32


to transmit power to the rotor shaft


34


even though the chambers


63


and


65


in which the rotor shaft and motor are mounted are mechanically isolated from each other, effectively eliminating any leakage path between the oil-filled and air-filled chambers. Although in the preferred embodiment, the separate chambers


63


and


65


are formed in contiguous housing portions separated by a barrier


110


, the chambers could also be formed in spaced apart housing portions.




A preferred embodiment of the down hole pulser


12


, installed in the bottom hole portion


7


of the drill string


6


, is shown in

FIGS. 4-14

. As previously discussed, the outer housing of the drill string


6


is formed by the section of drill pipe


64


, which forms the cental passage


62


through which the drilling mud


18


flows. As is conventional, the drill pipe


64


has threaded couplings on each end, shown in

FIGS. 4 and 6

, that allow it to be mated with other sections of drill pipe. As shown in

FIG. 4

, at its upstream end, the down hole pulser


12


is supported within the drill pipe


64


by the stator collar


39


. As shown in

FIG. 6

, the downstream end of the pulser


12


is attached via coupling


180


to a centralizer


122


that further supports it within the passage


62


. The stator


38


, which is mounted within the stator collar


39


, is coupled to the housing portions


66


,


68


and


69


.




As shown in

FIG. 4

, the upstream and downstream housing portions


66


and


68


forming the oil filled chamber


63


are threaded together, with the joint being sealed by O-rings


193


. The rotor


36


is located immediately upstream of the stator


38


and includes a rotor shaft


34


, which is mounted within the oil-filled chamber


63


by the upstream and downstream bearings


58


and


56


. A nose


61


, which is threaded onto the upstream end of the rotor shaft


34


, forms the forward most portion of the pulser


12


. The downstream end of the rotor shaft


34


is attached by a coupling


182


to the output shaft of the reduction gear


46


.




As shown in

FIG. 7

, an opening


161


is formed in housing portion


66


that allows the chamber


63


to be filled with oil, after which the opening


161


is closed by a plug


160


. Three pistons


162


slide in cylinders


164


formed in the housing portion


66


to create the pressure equalization system. The drilling mud


18


flowing through the passage


62


displaces the pistons


162


radially inward until the pressure of the oil inside the chamber


63


is approximately equal to that of the outside drilling mud.




As shown in

FIG. 8

, the air-filed housing portion


69


is threaded onto the downstream oil-filed housing portion


68


, with O-rings


191


sealing the threaded joint. The housing barrier


110


closes the downstream end of the oil-filled housing portion


68


, with O-rings


114


providing a seal between the barrier


110


and the housing portion


68


. A passage


108


in the barrier


110


facilitates filling the chamber


63


with oil and is thereafter closed with a plug


102


. The input shaft


113


of the reduction gear


46


is supported within the housing barrier


110


by the bearings


54


at its upstream end. The inner half


52


of the magnetic coupling


48


is attached to the downstream end of the input shaft


113


. The outer half


50


of the magnetic coupling


48


is attached to the upstream portion of shaft


94


, which is disposed in the air-filled chamber


65


. Thus, although shaft


94


transfers power to shaft


113


, there is no physical connection extending through the two chambers that could create a leakage path. Shaft


94


is mounted on bearings


55


supported on the downstream end of the housing barrier


110


and is driven by a clevis


92


and pin


96


that permits axial displacement between the two halves of the shafting. The clevis


92


is attached by a clamp


106


to a flexible coupling


90


, which accommodates radial misalignment of the components.




As shown in

FIG. 5

, the motor


32


and orientation encoder


44


are also mounted within the air-filled chamber


65


formed by the housing portion


69


, with the output shaft of the motor


32


being coupled to the clevis


92


via the flexible coupling


90


. As shown in

FIGS. 5 and 6

, the controller


26


is comprised of a central support plate


170


on which printed circuit boards are mounted, such as printed circuit boards


171


. The support plate


170


is supported on upstream and downstream ends


174


that are supported within the housing portion


69


and sealed by O-rings. The downstream support end


174


is coupled to an adapter


180


that mates to the upstream end of the centralizer


122


. A housing


199


is threaded onto the downstream end of the housing portion


69


and mates with the centralizer


122


. O-rings seal both the joint between the housing portion


69


and housing


199


and the joint between the housing


199


and the centralizer


122


.




The printed circuit boards


171


contain electronics components that are programed with associated information and soft-ware for operating the pulser


12


. Such software will include that necessary to translate the digital code from the data encoder


24


into operating instructions for the motor


32


. In some embodiments, this software will also include that necessary to analyze the signals from the down hole static pressure sensor


29


and/or the orientation encoder


44


and/or the dynamic down hole pressure sensor


28


, including that required to decipher encoded instructions from the surface that are received by the down hole dynamic sensor, and to control the operation of the motor


32


based on these signals, as explained further below. The creation of such software is well within the routine capabilities of those skilled in the art, when armed with the teachings disclosed herein.




A coupling


124


is formed on the downstream end of the centralizer


122


that allows it to be mechanically coupled with other portions of the bottom hole assembly


7


, which include the power supply


14


and data encoder


24


. An electrical connector


126


is mounted at the downstream end of the centralizer that allows the down hole pulser


12


to receive electrical signals from the power supply and data encoder


24


. A central passage


120


in the centralizer


122


allows conductors


128


from the connector


126


to extend to a connector


195


for the pulser


12


, which are then transmitted to the controller


26


via conductors, not shown.




As shown in

FIG. 6

, the down hole dynamic pressure sensor


28


is mounted in a recess


132


in the centralizer section


122


, although other locations could also be utilized. As shown best in FIGS.


9


and


9


(


a


), the down hole dynamic pressure sensor


28


is comprised of a diaphragm


144


formed by a circular face portion


145


and a rearwardly extending cylindrical skirt portion


148


. The diaphragm


144


must be sufficiently strong to withstand the pressure of the drilling mud


18


, which can be as high as 25,000 psi. However, it should also have a relatively low modulus of elasticity so as to be sufficiently elastic to dynamically respond to the pressure pulsations, the magnitude of which may be low at the pressure sensor


28


. Preferably, the diaphragm


144


is formed from titanium. Threaded holes are formed in the front surface of the diaphragm face


145


to facilitate removal of the sensor assembly


28


.




The piezoelectric element


150


is mounted adjacent, and in surface contact with, the diaphragm


144


. While piezoelectric elements can be made from a variety of materials, preferably, the piezoelectric element


150


is a piezoceramic element, which has a relatively high temperature capability (by contrast, piezoplastics, for example, cannot be used at temperatures in excess of 150° F.) and creates a relatively high voltage output when subjected to a minimum amount of strain. According to the piezoelectric phenomenon, certain crystalline substances, such as quartz and come ceramics, develop an electrical field when subjected to pressure. The piezoceramic element


50


according to the invention is preferably formed by forming a dielectric material, such as lead Metaniebate or lead zirconate titanate, into the desired shape, in this case, a thin disk. Electrodes are then applied to the material. The dielectric material is heated to an elevated temperature in the presence of a strong DC electric field, which polarizes the ceramic so that the molecular dipoles are aligned in the direction of the applied field, thereby imparting dielectric properties to the element. A piezoceramic element


150


has several attributes that make it especially suitable for down hole pressure pulsation sensing. It is compact. In one embodiment of a pressure pulsation sensor


16


, the piezoceramic element


50


is approximately only 0.8 inch in diameter and 0.02 inch thick. Piezoelectric elements consume relatively little electric power compared to strain gage based pressure transducers. Also, unlike strain gage based pressure transducers, the piezoceramic element


150


is not affected by static pressure, which would otherwise create a DC offset, because the voltage change that occurs when a piezoceramic element is stressed is transient, returning to zero in a short time even if the stress is maintained. Suitable piezoceramic elements are available from Piezo Kinetics Incorporated, Pine Street and Mill Road, Bellefonte, Pa. 16823.




The dynamic pressure sensor


28


also includes a plug


146


mounted behind the piezoceramic element


50


. The plug


146


is preferably formed from an electrically insulating material, such as a thermoplastic. It has external threads formed on its outside surface that mate with internal threads formed on a skirt portion of the diaphragm


144


. A dowel pin


154


is disposed in mating holes prevents rotation of the sensor assembly


28


.




In the preferred embodiment of the current invention, the piezoceramic element


150


is maintained in intimate surface contact with the diaphragm


144


by compressing the edges of the element between the rear face of the diaphragm and the plug


146


. The plug


146


is threaded into the diaphragm skirt


148


so that it rests on the piezoelectric element


150


, not the rear surface of the diaphragm face


145


, thereby leaving a gap between the plug and the diaphragm face. In operation, the high pressure of the drilling mud causes static deflection of the diaphragm face


145


, while pressure pulsations in the drilling mud cause vibratory deflection of the diaphragm face. Compressing the edges of the ceramic element


150


against the face of the diaphragm


144


ensures that the ceramic element will undergo vibratory deflections in response to vibratory deflections of the diaphragm face


145


, thereby enhancing the sensitivity of the sensor.




However, although the compressive force supplied by the plug


146


is sufficient to restrain the piezoceramic element


150


axially—that is, in the direction parallel to the axis of the diaphragm skirt


148


—it does not prevent relative sliding motion of the piezoceramic element in the radial direction—that is, in the plane of the element


150


. This prevents the piezoceramic element


150


from experiencing a large, static, tensile strain as a result of the static deflection of the diaphragm face


145


, such as would occur if the piezoceramic element


150


were glued or otherwise completely restrained with respect to the diaphragm face


145


. Such large tensile strains could result in failure of the piezoelectric element


150


, which is relatively brittle. In one embodiment of the invention, the plug


146


is threaded into the diaphragm skirt


148


so as to apply a 100 pound preloaded to the piezoelectric element


150


.




In operation, the high pressure of the drilling mud


18


causes static deflection of the diaphragm face


145


, while pressure pulsations in the drilling mud cause vibratory deflection of the diaphragm face which are transmitted to the piezoceramic element


150


. These vibratory deflections cause the voltage from the piezoceramic element


150


to varying in proportion to the deflection.




The conductor lead


156


from the piezoceramic element


150


extends through a potted grommet


157


on an intermediate support plate


155


formed in the plug


146


, and then through the passage


120


in the centralizer


122


before terminating at the controller


26


. As previously discussed, the printed circuit boards


171


of the controller


26


incorporate the electronics and software necessary to receive and analyze the voltage signal from the piezoceramic element


50


—for example, so as to determine the amplitude of the pressure pulses generated by the pulser


12


or to decode other instructions from the surface for operation of the pulser.




The construction and operation of the rotor


36


and stator


38


are shown in more detail in

FIGS. 10-14

. As shown in

FIG. 10

, the stator


38


is comprised of the collar


39


and an inner member


37


. Radially extending vanes


31


form axially extending passages


80


that are spaced circumferentially around the stator


38


. When the passages


80


are unobstructed, they allow drilling mud


18


to flow through the pulser


12


with minimum pressure drop. The rotor


36


is comprised of a sleeve


33


mounted by a key onto the rotor shaft


34


and from which blades


35


extend radially. Although four stator passages


80


and four rotor blades


35


are illustrated, other quantities of stator passages and rotor blades could also be used.




As discussed in detail below, preferably, the down hole pulser


12


operates by oscillating rotational motion—rotating first in one direction and then in an opposite direction. This mode of operation prevents flow blockages and jams. In a system that uses continuous rotation in a single direction, it is possible for a piece of debris to become lodged between the rotor and stator. This will have the effect of jamming the rotor and simultaneously obstructing one of the passages for the flow of drilling mud. In the current invention, any such obstruction will be alleviated during the normal course of operation, without disruption of data transmission, because reversal of the direction of rotor rotation during the next cycle will free the debris, allowing it to be carried away by the flow of drilling mud. This effect can be enhanced by shaping the rotor blades so that the clearance between the rotor and stator are increased when rotation occurs in one direction, as discussed below.




According to the preferred embodiment, the radial length l


2


of one of the edges


47


of each of the rotor blades


35


, shown as the trailing edge in

FIG. 11

, is slightly longer than the radial length l


1


of the opposite edge


45


, shown as the leading edge FIG.


11


—it should be appreciated that which edges are leading and trailing reverses each time the direction of rotation of the rotor reverses. Preferably, l


2


is about 0.010 inch longer than l


1


. In addition, as shown in

FIG. 13

, the downstream face


41


of each of the rotor blades


35


is preferably oriented at an angle φ with respect to the upstream face of the stator


38


so that the circumferential gap G by which the rotor blades are axially displaced from the stator increases from edge


47


to edge


45


. Preferably, the angle φ is at least about 5° so that the gap G


2


at edge


45


is at least about 0.040 inch larger than the gap G


1


at edge


47


, with G


1


preferably being about 0.080 inch. These two features—the unequal edge length and unequal axial gap—prevent jamming of the rotor since any debris trapped between the stator


38


and a rotor blade


35


during rotation in one direction will tend to be automatically dislodged when the rotor reverses its direction of rotation during the next cycle since such reversal will increase the radial and axial clearance between the rotor blades


35


and the stator


38


and thus allow the drilling fluid


18


to wash away the debris.




In an alternate embodiment, the downstream face


41


′ of the rotor blade is concave, as shown in FIG.


13


(


a


), so that any debris sufficiently small to pass between the axial gap G


3


between the edges


45


and


47


of the blades


35


′ and the stator


38


will end up being lodged in an area of increased axial gap G


4


and, thus, less likely to prevent rotation of the rotor.




As shown in

FIG. 12

, a novel annular seal


60


extends from the upstream end of the rotor


33


to the stator


38


. As a result of the pressure equalization system, described above, the pressure is approximately the same both inside and outside of the seal


60


. The upstream end of the seal


60


is secured by an interference fit onto a ring


85


, which, in turn, is press fit into the rotor sleeve


33


by a shim


87


. An O-ring


84


provides a seal between the ring


85


and the rotor shaft


34


. Note that although it rotates along with the rotor


36


, the O-ring


84


is considered a “stationary seal” because there is no relative rotation between the two members across which the seal is formed, in this case, the ring


85


and the rotor shaft


34


. Similarly, the downstream end of the seal


60


is press fit into the bore of the stator


38


by another shim


87


. O-rings


86


mounted in stationary seal rings


89


form stationary seals between the seal rings


89


and the stator


38


. In the illustrated embodiment, rotating seals


88


are mounted in the two downstream stationary seal rings


89


and form “rotating” seals between the rotating rotor shaft


34


and the stationary stator


38


. However, in many applications, the rotating seals


88


could be dispensed with so that there were no rotating seals and sealing accomplished exclusively with stationary seals—that is, seals between components that did not “rotate” relative to each other.




According to a preferred embodiment of the current invention, the seal


60


is generally cylindrical and preferably has helically extending corrugations so as to form a bellows type construction to facilitate torsion deflection without buckling, as well as axial expansion, as shown in FIG.


14


(


a


). Alternatively, a seal


60


′ having axial corrugations, which facilitate torsional deflection, could be employed, as shown in FIG.


14


(


b


). The seal


60


is preferably made from a resilient material, such as an elastomer, most preferably nitrile rubber, that is able to withstand the torsional deflects resulting from repeated angular oscillations—for example, through an angle of 45° associated with the operation of the rotor


36


, discussed below. Note that since the rotor


36


does not create pressure pulses by continuously rotating in a given direction, but rather by rotating in a first direction and then reversing and rotating in the opposite direction so as to only oscillate, conventional rotating seals can be dispensed with, as discussed above.




The operation of the rotor


36


according to the current invention, and the resulting pressure pulses in the drilling mud


18


are shown in

FIGS. 15 and 16

, respectively. Preferably, the circumferential expanse of the rotor blades


35


is about the same as, or slightly less than, that of the stator vanes


31


. Thus, when the rotor


36


is a first angular orientation, arbitrarily designated as the 0° orientation in FIG.


15


(


a


), the rotor blades


35


provide essentially no obstruction of the flow of drilling mud


18


through the passage


80


, thereby minimizing the pressure drop across the pulser


12


. However, when the rotor


36


has been rotated in the clockwise direction by an angle θ


1


, the rotor blades


35


partially obstruct the passages


80


, thereby increasing the pressure drop across the pulser


12


. (Whether a circumferential direction is “clockwise” or “counterclockwise” depends on whether the viewer is oriented upstream or downstream from the pulser


12


.




Therefore, as used herein, the terms clockwise and counterclockwise are arbitrary and intended to convey only opposing circumferential directions.) If the rotor


36


is thereafter rotated back to the 0° orientation, a pressure pulse is created having a particular shape and amplitude a


1


, such as that shown in FIG.


16


. If, in another cycle, the rotor


36


is rotated further in the circumferential direction from the 0° orientation to angular orientation θ


2


, the degree of obstruction and, therefore, the pressure drop will be increased, resulting in a pressure pulse having another shape and a larger amplitude a


2


, such as that also shown in FIG.


16


. Therefore, by adjusting the magnitude and speed of the rotational oscillation θ of the rotor


36


, the shape and amplitude of the pressure pulses generated at the pulser


12


can be adjusted. Further rotation beyond θ


2


will eventually result a rotor orientation providing the maximum blockage of the passage


80


. However, in the preferred embodiment of the invention, the expanse of the rotor blades


35


and stator passages


80


is such that complete blockage of flow is never obtained regardless of the rotor orientation.




The control of the rotor rotation so as to control the pressure pulses will now be discussed. In general, the controller


26


translates the coded data from the data encoder


24


into a series of discrete motor operating time intervals. For example, as shown in

FIG. 16

, in one operating mode, at time t


1


, the controller


26


directs the motor driver


30


to transmit an increment of electrical power of amplitude e


1


to the motor


32


. After a short time lag, due to inertia, the motor


32


will begin rotating in the circumferential direction, thereby rotating the rotor


36


, which is assumed to initially be at the 0° orientation, in the same direction.




At time t


2


, after an elapse of time interval Δt


1


, the controller will direct the motor driver


30


to cease the transmission of electrical power to the motor


32


so that, after a short lag time due to inertia, the rotor


36


will stop, at which time it will have reached angular orientation θ


1


, which, for example, may be 20°, as shown in FIG.


15


(


b


). This will result in an increase in the pressure sensed by the surface sensor


20


of a


1


. At time t


3


, after an elapse of time interval Δt


2


, the controller


26


directs the motor driver


30


to again transmit electrical power of amplitude e


1


to the motor


32


for another time interval Δt


1


, but now in the opposite—that is, the counterclockwise—direction, so that the rotor


36


returns back to the 0° orientation, thereby returning the pressure to its original magnitude. The result is the creation of a discrete pressure pulse having amplitude a


1


. Generally, the shape of the pressure pulse will depend upon the relative lengths of the timer intervals Δt


1


and Δt


2


and the speed at which the rotor moved between the 0° and θ


1


orientations—the faster the speed, the more square-like the pressure pulse, the slower the speed, the more sinusoidal the pressure pulse.




It will be appreciated that the time intervals Δt


1


and Δt


2


may be very short, for example, Δt


1


might be on the order of 0.18 second and Δt


2


on the order of 0.32 seconds. Moreover, the interval Δt


2


between operations of the motor could be essentially zero so that the motor reversed direction as soon as stopped rotating in the first direction.




After an elapse of another timer interval, which might be equal to Δt


2


or a longer or shorter time interval, the controller


26


will again direct the motor driver


30


to transmit electrical power of e


1


to the motor


32


for another time interval Δt


1


in the clockwise direction and the cycle is repeated, thus generating pressure pulses of a particular amplitude, duration, and shape and at particular intervals as required to transmit the encoded information.




The control of the characteristics of the pressure pulses, including their amplitude, shape and frequency, afforded by the present invention provides considerably flexibility in encoding schemes. For example, the coding scheme could involve variations in the duration of the pulses or the time intervals between pulses, or variations in the amplitude or shape of the pulses, or combinations of the foregoing. In addition to allowing adjustment of pressure pulse characteristics (including amplitude, shape and frequency) to improve data reception, a more complex pulse pattern could be also be effected to facilitate efficient data transmission. For example, the pulse amplitude could be periodically altered—e.g., every third pulse having an increased or decreased amplitude. Thus, the ability to control one or more of the pressure pulse characteristics permits the use of more efficient and robust coding schemes. For example, coding using a combination of pressure pulse duration and amplitude results in fewer pulses being necessary to transmit a given sequence of data.




Although the rotational movement of the rotor in each direction necessary to create a pressure pulse discussed above was effected by a continuous transmission of electrical power e so as to energize the motor over time interval Δt


1


, in order to minimize power consumption, the motor could also be energized over time interval Δt


1


by transmitting a series of very short duration power pulses, for example on the order of 10 milliseconds each, that spanned time interval Δt


1


so that, after the initial pulse of electrical power, each pulse of electrical power during Δt


1


was transmitted while the rotation of the motor was coasting down, but had not yet stopped, from the previous transmission a pulse of electrical power.




As discussed above, the controller


26


could direct power to the motor


32


over a predetermined time interval Δt


1


so as to result in an assumed amount of rotation θ. Alternatively, the controller could control one or more characteristics of the pressure pulses by making use of information concerning the angular orientation of the rotor


36


, such as the angular orientation itself or the change in angular orientation, provided by the orientation encoder


44


. This allows the controller


26


to operate the motor until a predetermined angular orientation, or change in angular orientation, was achieved. For example, the controller


26


could rotate the motor continuously until a given orientation was reached and then cease operation, if necessary taking into account inertia in the system to estimate the final orientation achieved. Or the controller


26


could repeatedly rotate the motor over discrete short time intervals until the orientation encoder


44


indicated that the desired amount of rotation had been obtained.




Significantly, according to one aspect of the current invention, as a result of the resistance to rotation by the rotor drive train, ceasing rotation of the motor


32


will cause the rotor


36


to remain at angular orientation θ


1


throughout the time period Δt


2


. Thus, the magnitude of the angular oscillation of the rotor


36


is set without the use of mechanical stops to stop rotation of the rotor at a predetermined location. Nor are stops used to maintain the rotor


36


in a given orientation. Such stops, when used continuously, are a source of wear and failure. Nevertheless, mechanical safety stops could be utilized to ensure that rotation beyond a maximum amount, such as that capable of being safety accommodated by the seal


60


, did not occur.




Significantly, the control over the characteristics of the pressure pulses afforded by the current invention allows adjustment of these characteristics in situ in order to optimize data transmission. Thus, it is not necessary to cease drilling and withdraw the pulser in order to adjust the amplitude, duration, shape or frequency of the pressure pulses as would have been required with prior art systems.




Operation in the mode discussed above can be continued so that the pulser


12


continuously oscillates over angle θ


1


, generating a series of pressure pulses the amplitude, shape, duration and frequency of which is set by the timing of the signals operating the motor.




However, after a period of time, one or more of the characteristics of the pressure pulses thus generated may create problems in terms of data reception at the surface pressure sensor


20


. This can occur for a variety of reasons, such as a change in mud flow conditions (such as flow rate or viscosity), or an increase in the distance between the pulser


12


and the surface pressure sensor


20


as drilling progresses, thereby increasing pressure pulse attenuation, or the introduction of noise or other sources of pressure pulsations into the drilling mud. According to the current invention, the controller


26


will then direct the motor driver


30


to alter one or more characteristics of the pressure pulses as appropriate.




For example, the amplitude of the pressure pulses could be increased by increasing the time interval Δt


1


′ during which the motor operates (for example, by increasing the duration over which electrical power of amplitude e


1


is transmitted to the motor). The increased motor operation increases the amount of rotation of the rotor


36


so that it assumes angular orientation θ


24


, for example 40°, as shown in FIG.


15


(


c


), thereby increasing the obstruction of the stator passages


80


by the rotor blades


35


and the pressure drop across the pulser


12


. Counter rotation of the rotor


36


back to the 0° orientation will result in the completion of the generation of a pressure pulse of increased amplitude a


2


. Operation is this mode will improved reception of data by the surface pressure sensor


20


.




Alternatively, data reception at the surface may be improved by altering the shape of the pressure pulse. For example, suppose that, after a period of time, the pressure pulses of increased amplitude a


2


also became difficult to decipher at the surface. According to the invention, the controller


26


could then direct the motor driver


30


to increase the amplitude of the electrical power transmitted to the motor to amplitude e


2


while also decreasing the time interval Δt


1


″ during which such power was supplied. The transmission of increased electrical power will increase the speed of rotation of the rotor


36


so that it assumes angular orientation θ


2


sooner and also returns to its initial position sooner, resulting in a pressure pulse that more nearly approximates a square wave. This type of operation is depicted by the dashed lines in FIG.


16


.




Alternatively, if it were desired to increase the frequency of the pressure pulses, for example, to avoid confusion with noise existing at a certain frequency, the time intervals Δt


1


and Δt


2


during which the rotor is operative and inoperative, respectively, could be shortened or lengthened by the controller


26


. Further, in situations in which there were no problems with data reception, the time intervals could be shortened to increase the rate of data transmission, resulting in the transmission of more data over a given timer interval.




Various schemes can be developed for controlling the pressure pulses according to the current invention. For example, the controller


26


could be programmed to automatically increase the pressure pulse amplitude, or automatically make the shape of the pressure pulse more square-like, as the drilling time increased, or as the depth of the bottom hole assembly or its distance from the surface increased. The controller


26


could increase the pulse amplitude as a function of the magnitude of the static pressure of the drilling mud in the vicinity of the pulser


12


as sensed by the static pressure transducer


29


—the higher the pressure, the greater the amplitude.




According to a preferred embodiment, proper control is effected by monitoring the pressure pulses generated by the down hole pulser


12


so as to create a feed back loop. This can be done by having the controller


26


make use of the signal from the down hole dynamic pressure sensor


28


and operate the motor so as to satisfy one or more predetermined criteria for the pressure pulse characteristics. For example, the controller


26


could ensure that the pressure pulse amplitude is maintained within a predetermined range or exceeds a predetermined minimum as the drilling progresses and despite changes in drilling mud flow conditions.




As another example, the controller


26


can analyze the characteristics of extraneous pressure pulses in the drilling mud sensed by the pressure sensor


28


, for example from the mud pumps, by temporarily ceasing operation of the down hole pulser


12


. The controller can then compare the pressure pulses generated by the down hole pulser


12


to those extraneous pressure pulses that were within a predetermined frequency range around that of the frequency of the pressure pulses generated by the pulser. The controller


26


would then increase or decrease the frequency of the pressure pulses generated by the down hole pulser


12


whenever the amplitude of such extraneous pressure pulses exceeded a predetermined absolute or relative amplitude. Alternatively, the shape of the pressure pulses generated by the down hole pulser


12


could be varied to better able the surface detection equipment to distinguish them from extraneous pressure pulses.




In one preferred embodiment of the invention, the down hole dynamic pressure sensor


28


is capable of receiving instructional information from the surface for controlling the pressure pulses. In one version of this embodiment, the information contains direct instructions for setting the timing of the power signals to be supplied by the motor driver


30


. For example, the instructions might call for the controller


26


to increase the magnitude of the electrical power supplied to the motor by a specific amount so that the rotor rotated more rapidly thereby altering the shape of the pressure pulses, or increase the duration of each interval during which the motor was energized thereby increasing the duration and amplitude of the pressure pulses, or increase the time interval between each energizing of the motor thereby decreasing the frequency, or data rate.




In another version, instructional information is provided that allows the controller


26


to make the necessary adjustment in motor control based on the sensed characteristics of the pressure pulses generated by the pulser


12


. For example, the information transmitted to the pressure sensor


28


could be revised settings for a particular pressure pulse characteristic, such a new range of pressure pulse amplitude within which to operate or a new value for the pressure pulse duration or frequency. Using logic programmed into it, the controller


26


would then adjust the operation of the motor


32


accordingly until the signal from pressure sensor


28


indicated that the new setting for the characteristic had been achieved.




In one version of this embodiment, the instructional information is transmitted to the controller


26


by the surface pulser


22


, which generates its own pressure pulses


110


encoded so as to contain the instructional information. The pressure pulses


110


are sensed by the down hole pressure sensor


28


and, using software well know in the art, are decoded by the controller


26


. The controller


26


can then effect the proper adjustment and control of the motor operation to ensure that the pressure pulses


112


generated by the down hole pulser


12


have the proper characteristics.




In one version, this is accomplished by having the controller


26


automatically direct the down hole pulser


12


to transmit pressure pulses


112


in a number of predetermined formats, such as a variety of data rates, pulse frequencies or pulse amplitudes, at prescribed intervals. The down hole pulser


12


would then cease operation while the surface detection system analyzed these data, selected the format that afforded optimal data transmission, and, using the surface pulser


22


, generated encoded pressure pulses


110


instructing the controller


26


as to the down hole pulser operating mode to be utilized for optimal data transmission.




Alternatively, the controller


26


could be informed that it was about to receive instructions for operating the down hole pulser


12


by sending to the controller the output signal from a conventional flow switch mounted in the bottom hole assembly, such as a mechanical pressure switch that senses the pressure drop in the drilling mud across an orifice, with a low ΔP indicating the cessation of mud flow and a high ΔP indicating the resumption of mud flow, or an accelerometer that sensed vibration in the drill string, with the absence of vibration indicating the cessation of mud flow and the presence of vibration indication the resumption of mud flow. The cessation of mud flow, created by shutting down the mud pump, could then be used to signal the controller


26


that, upon resumption of mud flow, it would receive instructions for operating the pulser


12


.




According to the invention, the mud pump


16


can be used as the surface pulser


22


by using a very simple encoding scheme that allowed the pressure pulses generated by mud pump operation to contain information for setting a characteristic of the pressure pulses generated by the down hole pulser


12


. For example, the speed of the mud pump


16


could be varied so as to vary the frequency of the mud pump pressure pulses that, when sensed by the down hole dynamic pressure sensor


29


, signal the controller


26


that a characteristic of the pressure pulses being generated by the down hole pulser


12


should be adjusted in a certain manner.




Although the foregoing aspect of the invention has been discussed by reference to transmitting instructions from the surface down hole to the controller via pressure pulses, other methods of transmitting instructions down hole could also be utilized. For example, the starting and stopping of the mud pump in a prescribed sequence could be used to transmit instructions to the controller


26


by means of a conventional flow switch, such as that discussed above, that sensed the starting and stopping of mud flow. As another example, information can be communicated by modulating the speed of rotation of the drill string in a predetermined pattern so as to transmit encoded data to the controller. In such an communications scheme, triaxial magnetometers and/or accelerometers, such as those conventionally used in positional sensors in bottom hole assemblies, can be used to detect rotation of the drill string. The output signals from these sensors can be transmitted to the controller, which would deciphered encoded instructions from these signals.




Although, according to the current invention, pressure pulses are preferably generated using the oscillating rotary pulser


12


described above, the principle of controlling one or more characteristics of the pressure pulses transmitted to the surface by sensing the generated pressure pulses or by transmitting instructions to the down hole pulser is also applicable to other types of pulsers, including reciprocating valve type pulsers and convention rotary pulsers, provided that, by employing the principals of the current invention, they can be adapted to permit variations in one or more characteristics of the pressure pulses. For example, a special controller, motor driver, variable speed motor and down hole dynamic pressure transducer constructed according to the teachings of the current invention could be incorporated, as required, into a conventional siren type rotary pulser system, discussed above. This would allow the surface detection system to transmit information, by way of pressure pulses generated at the surface as discussed above, to the controller of the down hole pulser instructing it, for example, to increase the rotational speed of the siren because data reception at the surface was being impaired by inference from extraneous pressure pulses at a frequency close to that of the siren frequency. The controller would then instruct the motor driver to increase the electrical power to the motor so as to increase the siren frequency. Alternatively, the controller could instruct the motor so as to adjust the phase shift of the pressure pulses relative to a reference signal that is used to encode the data. As another example, a conventional rotary pulser employing an escapement mechanism actuated by an electrically operated solenoid, such as that discussed above, could be modified with a controller that varied the operation of the solenoid so as to vary the duration or frequency of the pulses, for example, based on a comparison between the sensed duration or frequency of the pressure pulses generated by the down hole pulser or based upon instructions from the surface system deciphered by the down hole dynamic pressure transducer.




Thus, although the current invention has been illustrated by reference to certain specific embodiments, those skilled in the art, armed with the foregoing disclosure, will appreciate that many variations could be employed. For example, although the invention has been discussed with reference to a reversible electric motor, other motors, such as hydraulic motors capable of being quickly energized, could also be utilized.




Therefore, it should be appreciated that the current invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof and, accordingly, reference should be made to the appended claims, rather than to the foregoing specification, as indicating the scope of the invention.



Claims
  • 1. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string through a flow path thereof having a rotor disposed therein, comprising the steps of:a) generating a sequence of pressure pulses in the drilling fluid at said down hole location that propagate to said surface location, said sequence of pressure pulses generated by operating a drive train that drives said rotor so as to create rotational oscillations in said rotor that alternately block and unblock at least a portion of said drill string flow path by a predetermined amount, said sequence of pressure pulses being encoded with said information to be transmitted, said sequence of pressure pulses having an amplitude defined by the difference between the maximum and minimum values of the pressure of said drilling fluid; and b) controlling said amplitude of said generated encoded sequence of pressure pulses in situ at said down hole location by operating said drive train so as to vary the magnitude of said rotational oscillations of said rotor thereby varying said amount by which said portion of said flow path is alternately blocked and unblocked.
  • 2. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) generating pressure pulses in the drilling fluid at said down hole location that propagate to said surface location, said pressure pulses being encoded with said information to be transmitted; b) controlling at least one characteristic of said generated pressure pulses in situ at said down hole location; and c) transmitting instructional information from said surface location to said down hole location for controlling said pressure pulse characteristic, and wherein the step of controlling said pressure pulse characteristic comprises controlling said characteristic based upon said transmitted instruction.
  • 3. The method according to claim 2, wherein said at least one pressure pulse characteristic is selected from the group consisting of amplitude, duration, shape, and frequency.
  • 4. The method according to claim 3, wherein said at least one pressure pulse characteristic is amplitude.
  • 5. The method according to claim 2, further comprising the step of sensing said at least one characteristic of said pressure pulses at said down hole location, and wherein the step of controlling said pressure pulse characteristic comprises controlling said pressure characteristic based on said sensing thereof.
  • 6. The method according to claim 2, wherein said pressure pulses generated at said down hole location are first pressure pulses, and wherein the step of transmitting said instructional information to said down hole location comprises (i) generating second pressure pulses proximate said surface location that propagate to said down hole location, said second pressure pulses encoded with said instructional information, and (ii) sensing said second pressure pules at said down hole location.
  • 7. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) directing said drilling fluid along a flow path extending through said down hole portion of said drill string; b) directing said drilling fluid over a rotor disposed in said down hole portion of said drill string, said rotor capable of at least partially obstructing the flow of fluid through said flow path by rotating in a first direction and of thereafter reducing said obstruction of said flow path by rotating in an opposite direction, said rotation of said rotor driven by a drive train, said rotor drive train comprising a motor; c) creating a sequence of pressure pulses in said drilling fluid that propagate toward said surface location, said sequence of pressure pulses encoded to contain said information to be transmitted, said sequence of pressure pulses created by oscillating the rotation of said rotor, said rotor oscillated by operating said rotor drive train so as to rotate said rotor in said first direction through an angle of rotation thereby at least partially obstructing said flow path and then operating said rotor drive train so as to reverse said direction of rotation of said rotor so that said rotor rotates in said opposite direction thereby reducing said obstruction of said flow path; and d) making an adjustment to at least one characteristic of said sequence of pressure pulses by adjusting said operation of said rotor drive train so as to alter said oscillation of said rotor, said at least one pressure pulse characteristic selected from the group consisting of amplitude, duration, shape, and frequency, said adjustment of said oscillation of said rotor performed in situ at said down hole location.
  • 8. The method according to claim 7, wherein said pressure pulse characteristic adjusted in step (d) comprises said amplitude of said pressure pulses.
  • 9. The method according to claim 7, wherein said pressure pulse characteristic adjusted in step (d) comprises said shape of said pressure pulses.
  • 10. The method according to claim 9, wherein the step of adjusting said shape of said pressure pulses comprises changing the speed at which said rotor rotates in at least one of said first and second directions.
  • 11. The method according to claim 7, wherein said pressure pulse characteristic adjusted in step (d) comprises said duration of each of said pressure pulses.
  • 12. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) directing said drilling fluid along a flow path extending through said down hole portion of said drill string; b) directing said drilling fluid over a rotor disposed in said down hole portion of said drill string, said rotor capable of at least partially obstructing the flow of fluid through said flow path by rotating in a first direction and of thereafter reducing said obstruction of said flow path by rotating in an opposite direction, said rotation of said rotor driven by a drive train, said rotor drive train comprising a motor; c) creating a sequence of pressure pulses in said drilling fluid that propagate toward said surface location, said sequence of pressure pulses encoded to contain said information to be transmitted, said sequence of pressure pulses created by oscillating the rotation of said rotor, said rotor oscillated by operating said rotor drive train so as to rotate said rotor in said first direction through an angle of rotation thereby at least partially obstructing said flow path and then operating said rotor drive train so as to reverse said direction of rotation of said rotor so that said rotor rotates in said opposite direction thereby reducing said obstruction of said flow path; d) sensing the pressure of said drilling fluid at a location proximate said down hole portion of said drill string; and e) making an adjustment to at least the amplitude of said sequence of pressure pulses by adjusting said operation of said rotor drive train so as to alter said oscillation of said rotor, said adjustment of said oscillation of said rotor performed in situ at said down hole location by varying said angle of rotation of said rotor based on said sensed pressure of said drilling fluid.
  • 13. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) progressively drilling said well bore further into the earth, thereby further displacing said portion of said drill string from said surface location; b) directing said drilling fluid along a flow path extending through said down hole portion of said drill string; c) directing said drilling fluid over a rotor disposed in said down hole portion of said drill string, said rotor capable of at least partially obstructing the flow of fluid through said flow path by rotating in a first direction and of thereafter reducing said obstruction of said flow path by rotating in an opposite direction, said rotation of said rotor driven by a drive train, said rotor drive train comprising a motor; d) creating a sequence of pressure pulses in said drilling fluid that propagate toward said surface location, said sequence of pressure pulses encoded to contain said information to be transmitted, said sequence of pressure pulses created by oscillating the rotation of said rotor, said rotor oscillated by operating said rotor drive train so as to rotate said rotor in said first direction through an angle of rotation thereby at least partially obstructing said flow path and then operating said rotor drive train so as to reverse said direction of rotation of said rotor so that said rotor rotates in said opposite direction thereby reducing said obstruction of said flow path; and e) making an adjustment to at least the amplitude of said sequence of pressure pulses by adjusting said operation of said rotor drive train so as to alter said oscillation of said rotor, said adjustment of said oscillation of said rotor performed in situ at said down hole location by increasing said angle of rotation of said rotor so as to increase said amplitude of said pressure pulses as said drilling progresses.
  • 14. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) directing said drilling fluid along a flow path extending through said down hole portion of said drill string; b) directing said drilling fluid over a rotor disposed in said down hole portion of said drill string, said rotor capable of at least partially obstructing the flow of fluid through said flow path by rotating in a first direction and of thereafter reducing said obstruction of said flow path by rotating in an opposite direction; c) creating pressure pulses in said drilling fluid that propagate toward said surface location, said pressure pulses encoded to contain said information to be transmitted, each of said pressure pulses created by oscillating said rotor by rotating said rotor in said first direction through an angle of rotation so as to obstruct said flow path and then reversing said direction of rotation and rotating said rotor in said opposite direction so as to reduce said obstruction of said flow path, wherein a motor drives said rotation of said rotor, and wherein said rotor is oscillated by operating said motor over discrete time intervals; and d) making an adjustment to at least one characteristic of said pressure pulses by adjusting said oscillation of said rotor by translating said information to be transmitted into a series of said discrete motor operating time intervals, said at least one pressure pulse characteristic selected from the group consisting of amplitude, duration, shape, and frequency, said adjustment of said oscillation of said rotor performed in situ at said down hole location.
  • 15. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) directing said drilling fluid along a flow path extending through said down hole portion of said drill string; b) directing said drilling fluid over a rotor disposed in said down hole portion of said drill string, said rotor capable of at least partially obstructing said flow path by rotating in a first direction and of thereafter reducing said obstruction of said flow path by rotating in an opposite direction; c) oscillating rotation of said rotor by repeatedly rotating said rotor in said first direction through an angle of oscillation so as to at least partially obstruct said flow path and then rotating said rotor in said opposite direction so as to reduce said obstruction, thereby creating in said drilling fluid pressure pulses that are encoded to contain said information to be transmitted from said down hole location and that propagate toward said surface location; d) transmitting instructional information from said surface location to said down hole portion of said drill string for controlling at least one characteristic of said pressure pulses, said at least one pressure pulse characteristic selected from the group consisting of amplitude, duration, shape, frequency, and phase; e) receiving and deciphering said instructional information at said down hole portion of said drill string so as to determine said instruction for controlling said at least one characteristic of said pressure pulses; and f) controlling said at least one characteristic of said pressure pulses based upon said deciphered instruction,
  • 16. The method according to claim 15, wherein said pressure pulse characteristic controlled in step (f) comprises said amplitude of said pressure pulses.
  • 17. The method according to claim 16, wherein the step of controlling said amplitude of said pressure pulses comprises adjusting said angle through which said rotor oscillates.
  • 18. The method according to claim 16, further comprising the step of sensing said amplitude of said pressure pulses proximate said down hole location, wherein said instruction for controlling said amplitude of said pressure pulses comprises a criteria for said sensed amplitude of said pressure pulses, and wherein said angle of oscillation of said rotor is adjusted so as to satisfy said criteria.
  • 19. The method according to claim 16, wherein said pressure pulses propagating toward said surface location are first pressure pulses in said drilling fluid, and wherein the step of transmitting instructional information from said surface location to said down hole portion of said drill string comprises creating second pressure pulses in said drilling fluid, said second pressure pulses created at said surface location and propagating through said drilling fluid to said down hole portion of said drill string.
  • 20. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) directing said drilling fluid along a flow path extending through said down hole portion of said drill string; b) creating first pressure pulses in said drilling fluid by operating a first pulser disposed at said down hole location, said first pressure pulses propagating to said surface location, said first pressure pulses encoded to contain said information to be transmitted to said surface location; d) creating second pressure pulses in said drilling fluid by operating a second pulser disposed proximate said surface location, said second pressure pulses propagating to said down hole location, said second pressure pulses encoded to contain an instruction for setting at least one characteristic of said first pressure pulses, said at least one characteristic of said first pressure pulses selected from the group consisting of amplitude, duration, shape, frequency, and phase; and e) sensing said second pressure pulses at said down hole location and deciphering said instruction encoded therein; and f) setting said at least one characteristic of said first pressure pulses based upon said deciphered instruction, said setting of said characteristic performed by adjusting said operation of said first pulser in situ at said down hole location.
  • 21. The method according to claim 20, wherein said pressure pulse characteristic set in step (f) comprises said amplitude of said first pressure pulses.
  • 22. The method according to claim 20, wherein said pressure pulse characteristic set in step (f) comprises said duration of each of said first pressure pulses.
  • 23. The method according to claim 20, wherein said pressure pulse characteristic set in step (f) comprises said shape of said first pressure pulses.
  • 24. The method according to claim 20, wherein said pressure pulse characteristic set in step (f) comprises said frequency of said first pressure pulses.
  • 25. The method according to claim 20, wherein said pressure pulse characteristic set in step (f) comprises said phase of said first pressure pulses relative to a reference signal.
  • 26. The method according to claim 20, wherein second pulser is a pump for pumping said drilling fluid through said drill string.
  • 27. A method for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising the steps of:a) directing said drilling fluid to flow along a flow path extending through said down hole portion of said drill string; b) directing said drilling fluid over a rotor driven by a motor, said rotor capable of obstructing said flow path when rotated by said motor into a first angular orientation and of reducing said obstruction of said flow path when rotated by said motor into a second angular orientation; c) creating a series of pressure pulses in said drilling fluid that are encoded to contain said information to be transmitted and that propagate toward said surface location, each of said pressure pulses created by: (i) rotating said rotor in a first direction from said second angular orientation toward said first angular orientation by energizing said motor for a first period of time, (ii) stopping rotation of said rotor in said first direction by de-energizing said motor at the end of said first period of time, whereby said rotor stops at said first angular orientation without resort to mechanical stops, (iii) after a second period of time, rotating said rotor in an opposite direction toward said second angular orientation by energizing said motor for a third period of time, and (iv) stopping rotation of said rotor in said opposite direction by de-energizing said motor at the end of said third period of time.
  • 28. The method according to claim 27, wherein each of said pressure pulses has an amplitude, and further comprising the step of controlling the amplitude of said pressure pulses by varying said first period of time.
  • 29. The method according to claim 27, wherein said series of pressure pulses are created at a frequency, and further comprising the step of controlling said frequency by varying said second period of time.
  • 30. The method according to claim 27, further comprising the step of sensing the angular orientation of said rotor, and wherein the end of said first period of time is based upon said sensed angular orientation of said rotor.
  • 31. The method according to claim 27, wherein said first and third periods of time are equal.
  • 32. The method according to claim 27, wherein said second period of time is essentially zero.
  • 33. The method according to claim 27, wherein rotation of said rotor is stopped at said second angular orientation without resort to mechanical stops.
  • 34. The method according to claim 27, wherein said motor is energized for said first period of time by energizing said motor over a series of discrete time increments spanning said period of time.
  • 35. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, said drill string having a passage through which a drilling fluid flows, comprising:a) a housing for mounting in said drill string passage, first and second chambers formed in said housing, said first and second chambers being separated from each other, said first chamber filled with a gas, said second chamber filled with a liquid; b) a rotor capable of at least partially obstructing the flow of said drilling fluid through said passage when rotated into a first angular orientation and of reducing said obstruction when rotated into a second angular orientation, whereby rotation of said rotor creates pressure pulses in said drilling fluid; c) a drive train for rotating said rotor, at least a first portion of said drive train located in said liquid filled second chamber; d) an electric motor for driving rotation of said drive train, said electric motor located in said gas-filled first chamber.
  • 36. The apparatus according to claim 35, wherein said first portion of said drive train comprises a reduction gear.
  • 37. The apparatus according to claim 35, further comprising a piston driven by said drilling fluid for pressurizing said liquid-filled second chamber.
  • 38. The apparatus according to claim 35, wherein said drive train comprises a magnetic coupling.
  • 39. The apparatus according to claim 36, wherein said magnetic coupling comprises first and second magnets, said first magnet disposed in said gas-filled first chamber and said second magnet disposed in said liquid-filled second chamber.
  • 40. The apparatus according to claim 35, further comprising means for adjusting at least one characteristic of said pressure pulses.
  • 41. The apparatus according to claim 40, wherein said at least one pressure characteristic is the amplitude of said pressure pulses, and wherein said means for adjusting said amplitude of said pressure pulses comprises a transducer for sensing the amplitude of said pressure pulses proximate said housing.
  • 42. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, said drill string having a passage through which a drilling fluid flows, comprising:a) a pulser disposed at said down hole location for creating a sequence of pressure pulses in said drilling fluid that propagate toward said surface location, said pulser having oscillating means for alternately blocking and unblocking at least a portion of said passage so as to create a sequence of pressure pulses that are encoded to contain said information to be transmitted, said sequence of pressure pulses having an amplitude defined by the difference between the maximum and minimum values of the pressure of said drilling fluid; and b) means for adjusting said amplitude of said sequence of pressure pulses by adjusting operation of said pulser oscillating means in situ at said down hole location so as to vary the amount by which said portion of said passage is alternately blocked and unblocked.
  • 43. The apparatus according to claim 42, wherein said means for adjusting said amplitude of said pressure pulse comprises a transducer for sensing pressure pulses in said drilling fluid proximate said down hole location.
  • 44. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, said drill string having a passage through which a drilling fluid flows, comprising:a) a pulser disposed at said down hole location for creating pressure pulses in said drilling fluid that propagate toward said surface location and that are encoded to contain said information to be transmitted, said pulser comprising a rotor capable of at least partially obstructing the flow of fluid through said passage by rotating in a first direction through an angle of rotation and of thereafter reducing said obstruction of said passage by rotating in an opposite direction; and b) means for adjusting at least one characteristic of said pressure pulses by adjusting operation of said pulser in situ at said down hole location, said means for adjusting operation of said pulser comprising means for adjusting said rotation of said rotor.
  • 45. The apparatus according to claim 44, wherein said at least one characteristic of said pressure pulses is the amplitude of said pressure pulses, and wherein said means for means for adjusting said amplitude of said pressure pulses comprises means for varying said angle of rotation of said rotor.
  • 46. The apparatus according to claim 44, wherein said pulser further comprises a motor for rotating said rotor in said first and opposition directions, and wherein said means for adjusting said pressure pulse characteristic comprises means for translating said information to be transmitted into a series of time intervals during which said motor is operated in said first and opposite directions.
  • 47. The apparatus according to claim 44, wherein said means for adjusting said pressure pulse characteristic comprises means for translating said information into a series of angular rotations of said rotor.
  • 48. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, said drill string having a passage through which a drilling fluid flows, comprising:a) a pulser disposed at said down hole location for creating pressure pulses in said drilling fluid that propagate toward said surface location and that are encoded to contain said information to be transmitted; b) means for adjusting at least one characteristic of said pressure pulses by adjusting operation of said pulser in situ at said down hole location; and c) means for receiving information transmitted from said surface location to said down hole location encoded to contain an instruction for adjusting said characteristic of said pressure pulses.
  • 49. The apparatus according to claim 48, wherein said information receiving means comprises means for sensing pressure pulsations in said drilling fluid.
  • 50. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, a drilling fluid flowing through said drill string, comprising:a) a first pulser for creating first pressure pulses in said drilling fluid that propagate to said surface location, said first pulser disposed at said down hole location, said first pressure pulses encoded to contain said information to be transmitted to said surface location; b) a second pulser for creating second pressure pulses in said drilling fluid that propagate to said down hole location, said second pulser disposed proximate said surface location, said second pressure pulses encoded to contain an instruction for setting at least one characteristic of said first pressure pulses; and c) means for setting, in situ at said down hole location, said at least one characteristic of said first pressure pulses based upon said instruction encoded in said second pressure pulses.
  • 51. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, said drill string through which a drilling fluid flows, comprising:a) a stationary assembly for mounting in said drill string and having at least one passage through which said drilling fluid flows; b) a rotor mounted in said drill string proximate said stationary member and capable of at least partially obstructing the flow of said drilling fluid through said passage when rotated into a first angular orientation and of reducing said obstruction when rotated into a second angular orientation, whereby oscillation of said rotor between said first and second angular orientations creates pressure pulses in said drilling fluid encoded to contain said information; and c) a flexible seal spanning from said rotor to said stationary assembly, said seal having a first end fixedly attached to said rotor and a second end fixedly attached to said stationary assembly, whereby oscillation of said rotor causes said seal to undergo torsional deflection.
  • 52. An apparatus for transmitting information from a portion of a drill string operating at a down hole location in a well bore to a location proximate the surface of the earth, said drill string through which a drilling fluid flows, comprising:a) a stationary assembly for mounting in said drill string and having at least one passage through which said drilling fluid flows; b) a rotor mounted in said drill string proximate said stationary member and capable of at least partially obstructing the flow of said drilling fluid through said passage when rotated into a first angular orientation and of reducing said obstruction when rotated into a second angular orientation, whereby oscillation of said rotor between said first and second angular orientations creates pressure pulses in said drilling fluid encoded to contain said information; c) means for preventing debris in said drilling fluid from jamming rotation of said rotor.
  • 53. The apparatus according to claim 52, wherein said rotor has a plurality of blades extending radially outward therefrom, each of said blades having a first radially extending edge having a length l1 and a second radially extending edge opposite said first edge, said second edge having a length l2, and wherein said means for preventing jamming comprises l2 being longer than l1.
  • 54. The apparatus according to claim 52, wherein said rotor has a plurality of blades extending radially outward therefrom, each of said blades having a first radially extending edge and a second radially extending edge circumferentially displaced from said first edge, each of said blades being axially displaced from said stationary assembly by a circumferentially extending gap, and wherein said means for preventing jamming comprises said gap varying as it extends circumferentially from said first edge to said second edge.
US Referenced Citations (52)
Number Name Date Kind
2901685 Alder Aug 1959 A
2964116 Peterson Dec 1960 A
2973505 Johannesen Feb 1961 A
3065416 Jeter Nov 1962 A
3302457 Mayes Feb 1967 A
3309656 Godbey Mar 1967 A
3693428 LePeuvedic et al. Sep 1972 A
3713089 Clacomb Jan 1973 A
3732728 Fitzpatrick May 1973 A
3736558 Cubberly, Jr. May 1973 A
3737843 LePeuvedic et al. Jun 1973 A
3739331 Godbey et al. Jun 1973 A
3742443 Foster et al. Jun 1973 A
3764968 Anderson Oct 1973 A
3764969 Cubberly, Jr. Oct 1973 A
3764970 Manning Oct 1973 A
3770006 Sexton et al. Nov 1973 A
3958217 Spinnler May 1976 A
3964556 Gearhart et al. Jun 1976 A
4007805 Reber Feb 1977 A
RE29734 Manning Aug 1978 E
RE30055 Claycomb Jul 1979 E
4351037 Scherbatskoy Sep 1982 A
4462469 Brown Jul 1984 A
4499563 Jürgens Feb 1985 A
4628495 Peppers et al. Dec 1986 A
4630244 Larronde Dec 1986 A
RE32463 Westlake et al. Jul 1987 E
4698794 Kruger et al. Oct 1987 A
4734892 Kotlyar Mar 1988 A
4785300 Chin et al. Nov 1988 A
4790393 Larronde et al. Dec 1988 A
4796699 Upchurch Jan 1989 A
4847815 Malone Jul 1989 A
4914637 Goodsman Apr 1990 A
4915168 Upchurch Apr 1990 A
4956823 Russell et al. Sep 1990 A
5073877 Jeter Dec 1991 A
5079750 Scherbatskoy Jan 1992 A
5113379 Scherbatskoy May 1992 A
5119344 Innes Jun 1992 A
5182731 Hoelscher et al. Jan 1993 A
5189645 Innes Feb 1993 A
5215152 Duckworth Jun 1993 A
5357483 Innes Oct 1994 A
5517464 Lerner et al. May 1996 A
5586084 Barron et al. Dec 1996 A
5691712 Meek et al. Nov 1997 A
5787052 Gardner et al. Jul 1998 A
6105690 Biglin, Jr. et al. Aug 2000 A
6289998 Krueger et al. Sep 2001 B1
6469637 Seyler et al. Oct 2002 B1
Foreign Referenced Citations (1)
Number Date Country
2156405 Oct 1985 GB