Apparatus for weight on bit measurements, and methods of using same

Information

  • Patent Grant
  • 6802215
  • Patent Number
    6,802,215
  • Date Filed
    Wednesday, October 15, 2003
    20 years ago
  • Date Issued
    Tuesday, October 12, 2004
    19 years ago
Abstract
The present invention is generally directed to a tool for obtaining weight-on-bit (WOB) measurements and methods of using such a tool. In one illustrative embodiment the tool comprises a body, at least one strain gauge cavity in the body, the strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge operatively coupled to the mounting face above the region of approximately zero axial strain. In another illustrative embodiment, the method comprises providing a weight-on-bit measurement tool comprised of a body, at least one strain gauge cavity in the body, the strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge coupled to the mounting face above the region of approximately zero axial strain. The method further comprises positioning the tool in a drill string comprised of a drill bit, drilling a well bore with the drill string, and obtaining weight-data-on-bit measurement data using the weight-on-bit strain gauge in the tool.
Description




BACKGROUND OF INVENTION




1. Field of the Invention




The present invention is generally directed to tools and methods employed to obtain downhole measurements regarding the drilling of a well bore, and, more particularly, to a tool for obtaining weight-on-bit (WOB) measurements and methods of using such a tool.




2. Description of the Related Art




Oil and gas wells are formed by a rotary drilling process. To that end, a drill bit is mounted on the end of a drill string which may be very long, e.g., several thousand feet. At the surface, a rotary drive mechanism turns the drill string and the attached drill bit at the bottom of the hole. In some cases, a downhole motor may provide the desired rotation to the drill bit. During drilling operations, a drilling fluid (so-called drilling mud) is pumped through the drill string and back up-hole by pumps located on the surface. The purpose of the drilling fluid is to, among other things, remove the earthen cuttings resulting from the drilling process.




Weight-on-bit (hereinafter WOB) is generally recognized as being an important parameter in controlling the drilling of a well. The weight is applied to the bit by a string of heavy drill collars that is attached immediately above the bit and suspended in the borehole on smaller diameter drill pipe. In conventional drilling practice, the entire length of the drill pipe and an upper portion of the drill collar string are suspended at the surface from the derrick in tension, so that the amount of WOB can be varied by changing the indicated surface hookload. Properly controlled WOB is necessary to optimize the rate that the bit penetrates a particular type of earth formation, as well as the rate of bit wear. WOB also is utilized in controlling the direction of the hole, and accurate measurement thereof can be used in analyzing drilling rate “breaks” indicative of entry of the bit into more porous earth formations. Thus, precise and accurate measurements of the WOB parameter may be important in the drilling process. Torque also is an important measure useful in estimating the degree of wear on the bit, particularly when considered together with measurements of WOB.




In the past, WOB measurements have sometimes been made at the surface by comparing indicated hookload weight to off-bottom weight of the drill string. However, surface measurement of WOB is not always reliable due to the drag of the drill string on the borehole wall, and other factors.




In other cases, a strain gauge bridge positioned in a downhole tool has been used to obtain various data, including WOB measurement data. During drilling operations, there is a pressure difference between the internal pressure within the drill pipe and the external pressure in the well bore annulus between the drill pipe and the well bore. This pressure differential may be quite large, e.g., on the order of approximately 200-800 psi for a typical well. A large percentage of pressure differential is due to the pressure drop as the drilling fluid circulates throughout the drill bit. The downhole pressures result in strains that act in the same sense as the axial strains associated with the WOB, thereby creating the possibility that the strains associated with the downhole pressures can be misinterpreted as reflecting WOB values. While the differential pressure may be on the order of 200-850 psi, the overall pressure may be as high as approximately 10,000 psi. Pressures of this magnitude may cause massive errors in WOB measurements.




At least theoretically, the strains induced by the downhole pressures can be compensated for by various pressure correction factors that are based upon various calculations. However, there are several drawbacks to such a methodology. For example, if the strains from the downhole pressures are combined with the strains from the WOB, the overall strain values that may be obtained are much higher than the strain value for the WOB alone. In turn, this requires that a data acquisition system used to obtain such strain data must have a relatively larger analog input range, thereby resulting in a lower resolution of the strain values of interest. Second, if the internal and external pressures are not measured, or at least not accurately measured, it is very difficult to accurately apply pressure correction factors. Moreover, such pressure correction factors have inherent inaccuracies that, all other things being equal, would preferably be avoided.




The present invention is directed to an apparatus and methods that may solve, or at least reduce, some or all of the aforementioned problems.




SUMMARY OF INVENTION




The present invention is generally directed to a tool for obtain weight-on-bit (WOB) measurements and methods of using such a tool. In one illustrative embodiment the tool comprises a body, at least one strain gauge cavity in the body, the strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge operatively coupled to the mounting face above the region of approximately zero axial strain.




In another illustrative embodiment, the method comprises providing a weight-on-bit measurement tool comprised of a body, at least one strain gauge cavity in the body, the strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge coupled to the mounting face above the region of approximately zero axial strain. The method further comprises positioning the tool in a drill string comprised of a drill bit, drilling a well bore with the drill string, and obtaining weight-on-bit measurement data using the weight-on-bit strain gauge in the tool.




In a further illustrative embodiment, the method comprises identifying a region of approximately zero axial strain due to downhole pressures for a body to be positioned in a drill string when the body is subjected to downhole pressures during drilling operations, providing a strain gauge cavity in the body such that a strain gauge mounting face within the cavity is located at a position wherein the region of approximately zero axial strain exists on the mounting face when the body is subjected to downhole pressures during drilling operations, and coupling a weight-on-bit strain gauge to the mounting face above the region of approximately zero axial strain.











BRIEF DESCRIPTION OF DRAWINGS




The invention may be understood by reference to the following description taken in conjunction with the accompanying drawings, in which like reference numerals identify like elements.





FIG. 1

is a partial cross-sectional side view of a downhole tool in accordance with one illustrative embodiment of the present invention.





FIG. 2

is a cross-sectional plan view of a downhole tool in accordance with one illustrative embodiment of the present invention.





FIGS. 3A-3B

are a front and a cross-sectional side view, respectively, of one illustrative embodiment of a strain gauge cavity that may be employed with the present invention.





FIG. 4

is a strain plot depicting one illustrative embodiment wherein a WOB strain gauge is positioned in the strain gauge cavity above a region of approximately zero strain.





FIG. 5

is a graph depicting axial strain levels at different positions along the strain gauge surface.





FIG. 6

depicts an alternative embodiment of a strain gauge cavity that may be employed with the present invention.





FIG. 7

depicts another alternative embodiment of a strain gauge cavity that may be employed with the present invention.











While the invention is susceptible to various modifications and alternative forms, specific embodiments thereof have been shown by way of example in the drawings and are herein described in detail. It should be understood, however, that the description herein of specific embodiments is not intended to limit the invention to the particular forms disclosed, but on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope of the invention as defined by the appended claims.




DETAILED DESCRIPTION




Illustrative embodiments of the invention are described below. In the interest of clarity, not all features of an actual implementation are described in this specification. It will, of course, be appreciated that in the development of any such actual embodiment, numerous implementation-specific decisions must be made to achieve the developers” specific goals, such as compliance with system-related and business-related constraints, which will vary from one implementation to another. Moreover, it will be appreciated that such a development effort might be complex and time-consuming, but would nevertheless be a routine undertaking for those of ordinary skill in the art having the benefit of this disclosure.




The present invention will now be described with reference to the attached drawings which are included to describe and explain illustrative examples of the present invention. The words and phrases used herein should be understood and interpreted to have a meaning consistent with the understanding of those words and phrases by those skilled in the relevant art. No special definition of a term or phrase, i.e., a definition that is different from the ordinary and customary meaning as understood by those skilled in the art, is intended to be implied by consistent usage of the term or phrase herein. To the extent that a term or phrase is intended to have a special meaning, i.e., a meaning other than that understood by skilled artisans, such a special definition will be expressly set forth in the specification in a definitional manner that directly and unequivocally provides the special definition for the term or phrase.




The present invention will now be initially described with reference to

FIGS. 1 and 2

. As depicted therein, a downhole tool


10


is comprised of a body


12


, an internal bore


14


, having a longitudinal centerline


16


, an inner surface


18


and an outer surface


20


. As depicted in

FIG. 1

, the tool


10


is adapted to be positioned in a well bore


22


formed in the earth


24


. A well bore annulus


26


is defined between the outer surface


20


of the body


12


and the earth


24


. During drilling operations, drilling fluid (or “mud”) is circulated down through the internal bore


14


, out a drill bit (not shown) and returned to the surface via the annulus


26


.




In the illustrative embodiment depicted in

FIG. 1

, the tool


10


is further comprised of a plurality of strain gauge cavities


30


. A schematically depicted strain gauge


32


is mounted on a strain gauge mounting face


34


in each of the cavities


30


. The strain gauge


32


is adapted to provide WOB data, and it is part of a strain gauge bridge (not shown) positioned within the cavity


30


. Such strain gauge bridges are well known to those skilled in the relevant art, and, thus, will not be depicted or discussed in any further detail so as not to obscure the present invention. As indicated in

FIG. 2

, in one illustrative embodiment, the tool


10


is comprised of two cavities


30


that are positioned approximately 180 degrees apart from one another on approximately opposite sides of the body


12


and located at approximately the same vertical height. Also depicted in

FIG. 1

is an electronics compartment


36


where data from the strain gauges


32


may be transmitted and stored, processed or otherwise analyzed by various devices. Typically, the electronics compartment


36


will contain a data acquisition system (not shown) that may be useful in acquiring and manipulating data obtained from the strain gauge


32


positioned within the cavity


30


. Wire paths


38


are provided to allow proper wiring of the strain gauges


32


to components in the electronics compartment


36


.




Also depicted in

FIG. 1

is a protective cover


40


for each of the cavities


30


. In one illustrative embodiment, the covers


40


may be threadingly coupled to the cavity


30


and a seal may be provided by a seal ring (not shown). As thus configured, an air pocket


44


is defined by the internal surfaces of the cavity


30


and the cover


40


. However, the present invention is not limited to the cavity


30


and cover


40


configuration depicted in FIG.


1


. That is, as will be described further in the application, the embodiment depicted in

FIG. 1

is but one illustrative example of a cavity


30


and cover


40


that may be employed with the present invention.





FIGS. 3A-3B

are provided to provide further details with respect to one illustrative embodiment of the present invention. More specifically,

FIG. 3A

is a front view of an illustrative strain gauge cavity


30


in accordance with one illustrative embodiment of the present invention, and

FIG. 3B

is an enlarged, partial cross-sectional view of such an illustrative cavity


30


. In the embodiment depicted therein, the cavity


30


has a circular cross-sectional configuration. However, after a complete reading of the present application, those skilled in the art will understand that the cavity


30


may be formed to any desired shape. Thus, the present invention should not be considered as limited to cavities


30


having a circular configuration unless such limitations are clearly set forth in the appended claims. Moreover, the size of the cavity


30


may also vary depending upon the particular application. In one illustrative embodiment for a tool with a 6.25″ outside diameter, the cavity


30


has a diameter of approximately


1½″ and a depth 48 of approximately




1⅛″, although such dimensions may vary depending on the particular application. For ease of reference, the labels


0°, 90°, 180°and 270° have been added to

FIG. 3A

, which is a frontal view of the cavity


30


. The longitudinal centerline


16


of the tool


10


runs approximately parallel to the 0°-180°line depicted in

FIG. 3A

, with 0° representing the surface or uphole direction and 180°representing the downhole direction.




In general, the present invention involves locating the strain gauge mounting face


34


of the strain gauge cavity


30


at a position where a line or region of approximately zero axial strain is present on the mounting face


34


of the cavity


30


when the tool


10


is subjected to downhole pressures during operation. The position of the mounting face


34


at which a line or region of approximately zero axial strain will exist on the mounting face


34


will vary depending upon the particular application. More specifically, the distance 50 between the inner surface


18


of the body


12


and the mounting surface


34


will vary depending upon the particular application. A variety of factors, such as the internal pressure within the internal bore


14


, the external pressure in the well bore annulus


26


, the pressure difference between the internal and external pressures, the mechanical configuration of the tool


10


, the mechanical configuration of the cavity


30


, the material from which the body


12


is made, and the pressure within the cavity


30


, etc., may have an impact regarding the location in the body


12


where a line or region of approximately zero axial strain occurs.




Determining the correct position at which to locate the mounting face


34


such that a line or region of approximately zero axial strain exists on the mounting face


34


may involve analysis of the various stresses and strains produced on the body


12


under anticipated loading conditions. Such analytical techniques may involve finite element analysis and/or computational analysis techniques that are well known to those skilled in the art. Typically, such a stress/strain analysis may be performed to generate a strain diagram that depicts a range of strain values, both positive and negative, within the body


12


. At some point, a location in the body


12


will be identified wherein the strain diagram indicates that a region of approximately zero axial strain will occur at that location when the tool


10


is subjected to downhole pressures during drilling operations. For example, with reference to

FIG. 3B

, the analysis will result in a strain diagram wherein, at a radial distance 50, a region of approximately zero axial strain will exist within the body


12


on the mounting face


34


of the cavity


30


. The strain diagram from the analysis will typically identify a range of axial strain values, plus and minus, that will exist on the mounting face


34


during operating conditions. Once this strain diagram is obtained, the strain pattern may be laid out or otherwise identified on the mounting face


34


of the tool


10


. Then, as described more fully below, the strain gauge


32


is operatively coupled to the mounting face


34


above at least the region of approximately zero axial strain.





FIG. 4

depicts an illustrative strain diagram superimposed on the mounting face


34


of the cavity


30


. The strain diagram reflects axial strains from the combined loadings due to anticipated downhole pressures wherein the location of the mounting surface


34


within the body


12


is selected such that a line or area of approximately zero axial strain is present on the mounting face


34


. More specifically, in

FIG. 4

, the strain diagram reflects the situation where the cavity


30


is at approximately atmospheric pressure and there is an internal pressure of approximately 5000 psi (within the internal bore


14


) and an external pressure (in the annulus


26


) of approximately 4000 psi, for a pressure differential of approximately 1000 psi. In the illustrative embodiment depicted in

FIG. 4

, there are five regions or areas


51


,


53


,


55


,


57


and


59


that reflect different axial strain values, ranging from the highest (in a relative sense) negative strain values in region


59


to the highest positive strain values in region


51


. For simplicity and ease of explanation, only five such regions are indicated in FIG.


4


. Moreover, the regions


51


,


53


,


55


,


57


and


59


may be somewhat exaggerated in size, as compared to such regions in practice, for ease of explanation. In practice, depending upon the level of detail obtained from the stress analysis, there may be many such regions identified. In the example depicted in

FIG. 4

, the region


53


indicates positive strain values ranging from 0 to +2 e−6, while the region


55


indicates negative strain values ranging from 0 to −2 e−6. Thus, in this illustrative example, the line or region of approximately zero axial strain would actually be at the interface between the regions


53


and


55


. As indicated in

FIG. 4

, the WOB strain gauge


32


is positioned above at least the area or region of approximately zero axial strain. Any of a variety of commercially available strain gauges may be employed as the WOB strain gauge


32


as long as it is properly positioned and operatively coupled to the mounting face


34


, which is also properly located based upon the stress analysis. The strain gauge


32


may be mounted to the mounting face


34


by any of a variety of known techniques, e.g., spot-welding, gluing, bonding, etc.




In general, the strain gauge


32


should be positioned as close as practical to the region of approximately zero axial strain. However, in practicing the present invention, due to the physical size of the strain gauges


32


and the size of the areas of approximately zero axial strain, it may be difficult to precisely locate the strain gauge such that it is actually positioned only on a region of zero axial strain. When the strain gauge


32


is operatively coupled to the mounting face


34


, the strain gauge


32


may actually extend into areas on the mounting face


34


that have slightly positive or negative values of strain. Simply put, according to one embodiment of the present invention, the strain gauge


32


should be positioned as close as practical to the area on the mounting face


34


that exhibits zero axial strain due to the anticipated downhole pressure conditions when the tool


10


is in service.




By identifying the region of approximately zero axial strain, and locating the strain gauges at that position, the strains due to pressure do not adversely impact the WOB measurements, or at least such impact is greatly reduced. Stated another way, the strains due to pressure may be approximately zeroed out by properly locating the mounting face


34


within the body


12


, and positioning the strain gauge


32


at that location. A strain gauge


32


would also be positioned in the cavity


30


on the opposite side of the tool


10


such that strains due to bending are effectively cancelled out.




In one illustrative aspect, the present invention may be optimized to work best at a particular ratio of external pressure and internal pressure, e.g., 4000 psi/5000 psi. Such a design would work equally as well at other pressures, as long as the ratio of the applied pressures is approximately the same, e.g., 2000 psi external/2500 psi internal pressure. In general, the WOB measurement provided in accordance with the present invention should be relatively insensitive to the overall pressure (combined loading) on the tool. Since the pressure drop through the bit is relatively small and more consistent compared to overall loading of the tool, a tool in accordance with the present invention may generally be effective in varying conditions. Attached as

FIG. 5

is a diagram that is useful in describing the usefulness of the present invention. As shown therein,

FIG. 5

depicts the overall level of axial strain (vertical axis) due to the combined pressure loads. Three pressure loads, which would be typical of drilling conditions, are shown in FIG.


5


. The graph shows that all of the pressure loads have a point where the axial strain is approximately zero. The points of approximately zero axial strain do not overlap precisely for all of the various loading combinations. However, for each individual loading condition, the point of approximately zero axial strain may be more precisely identified. More importantly, even in the case where multiple loadings are experienced, by locating the strain gauges at the regions of approximately zero axial strain for most, if not all, anticipated loading conditions, pressure-induced errors in WOB measurements may be reduced relative to the errors that would be introduced if the strain gauges were positioned in a haphazard or random manner without regard to the pressure-induced axial strains that will exist on the strain gauge mounting face


34


.





FIG. 6

depicts an alternative embodiment of the present invention wherein the strain gauge cavity


30


may be defined by use of a cavity insert


60


. As depicted therein, the cavity insert


60


is a separate device that may be positioned in an opening


61


formed in the body


12


of the tool


10


. In the depicted embodiment, the cavity insert


60


has a generally conical configuration and it has a surface


64


that is adapted to be approximately flush with the inner surface


18


of the body


12


when installation is complete. The cavity insert


60


has a strain gauge mounting face


34


that is positioned and located as described above. In the depicted embodiment, the cavity insert


60


is secured within the body


12


by the protective cap


40


, which is threadingly engaged with the body


12


. A seal


69


is positioned between the cavity insert


60


and the body


12


. As described previously, the thickness


68


of the bottom portion of the cavity insert


60


is controlled such that, for its intended application, an area of approximately zero axial strain exists on the mounting face


34


.





FIG. 7

depicts yet another illustrative embodiment of a cavity


30


in accordance with the present invention. As shown therein, the cavity insert


60


has a generally cylindrical configuration and a strain gauge mounting face


34


. The cavity insert


60


is secured in place by the cover


40


that is threadingly coupled to the body


12


. In this illustrative embodiment, a passageway


70


is provided in the body


12


between the cavity insert


60


and the inner bore


14


of the tool


10


. The passageway


70


may, in one embodiment, be a hole having a diameter that may vary from approximately 0.125-1.0 inches depending upon the particular application. A seal


72


is provided between the cavity insert


60


and the body


12


. In this embodiment, the passageway


70


is provided to insure that the internal pressure within the bore


14


acts on the cavity insert


60


. As with other embodiments, the cavity insert


60


depicted in

FIG. 7

is sized and positioned such that the strain gauge mounting face


34


is located at a position such that a line or region of approximately zero axial strain exists on the mounting face


34


when the tool


10


is subjected to downhole pressures during drilling.




In the embodiments depicted herein, the strain gauge cavities


30


are designed and configured such that an air pocket


44


is provided in the cavities


30


. However, those skilled in the art will recognize that the present invention may be employed in situations where the cavity


30


is flooded with an appropriate inert fluid, and a diaphragm (not shown) is employed instead of the cover


40


. Such configurations are well known to those skilled in the art and, thus, will not be described in any further detail. In some cases, it may be desirable to employ such a flooded cavity


30


design to properly locate the strain gauge mounting face


34


at an appropriate position within the body


12


. However, it should be understood that if a flooded cavity design is adapted, the size, location and configuration of the design may need to be significantly redesigned due to the reduce differential pressure between the mounting face


34


of the strain gauge


32


and the internal bore


14


.




The body


12


may take on a variety of configurations and it may or may not be symmetrical through its entire axial length. If the body is asymmetrical, that factor may have to be accounted for in determining the location of the mounting face


34


in a particular region of the tool


10


as compared to other regions. The body


12


may be comprised of a variety of materials, e.g., an austenitic stainless steel, such as NMS


140


, a carbon steel, such as Type


4340


carbon steel, titanium, etc. Moreover, the body


12


may be made from a forging or it may simply be a section of pipe. The cavities


30


disclosed herein may be located at any location along the axial length of the drill string. Normally, the cavities


30


, and strain gauges


32


therein, will be positioned as close as practical to the drill bit such that the gauges


32


more accurately reflect the true WOB. For example, the drill string may be configured in a bit tool drill collar arrangement, a bit tool downhole motor arrangement, or a bit tool rotary steerable tool arrangement. The present invention may be employed with vertical wells or deviated wells.




The data obtained from the strain gauges


32


located within the tool


10


in accordance with the present invention may be employed in a number of ways. For example, the data obtained by the strain gauge


32


may simply be stored in a data acquisition system (not shown) positioned in the electronics compartment


36


, or it may be provided on a real-time basis to the drilling operators via any of a variety of known telemetry systems or techniques. In the case where multiple wells are to be drilled in a relatively small region, it may be sufficient to simply use the WOB data from the strain gauge


32


to assist in planning or designing the drilling operations on subsequently drilled wells. In the situation where real-time data is supplied to the drilling operators, the WOB data may actually be employed to control the WOB as the well is being drilled.




The present invention is generally directed to a tool for obtaining weight-on-bit (WOB) measurements and methods of using such a tool. In one illustrative embodiment the tool comprises a body, at least one strain gauge cavity in the body, the strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge operatively coupled to the mounting face above the region of approximately zero axial strain.




In another illustrative embodiment, the tool comprises a body, at least two strain gauge cavities in the body, each of the strain gauge cavities having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge operatively coupled to the mounting face above the region of approximately zero axial strain.




In yet another illustrative embodiment, the method comprises providing a weight-on-bit measurement tool comprised of a body, at least one strain gauge cavity in the body, the strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on the mounting surface when the tool is subjected to downhole pressures during drilling operations, and a weight-on-bit strain gauge coupled to the mounting face above the region of approximately zero axial strain. The method further comprises positioning the tool in a drill string comprised of a drill bit, drilling a well bore with the drill string, and obtaining weight-on-bit measurement data using the weight-on-bit strain gauge in the tool.




In a further illustrative embodiment, the method comprises identifying a region of approximately zero axial strain due to downhole pressures for a body to be positioned in a drill string when the body is subjected to downhole pressures during drilling operations, providing a strain gauge cavity in the body such that a strain gauge mounting face is located at a position wherein the region of approximately zero axial strain exists on the mounting face when the body is subjected to downhole pressures during drilling operations, and coupling a weight-on-bit strain gauge on the mounting face above the region of approximately zero axial strain.




The particular embodiments disclosed above are illustrative only, as the invention may be modified and practiced in different but equivalent manners apparent to those skilled in the art having the benefit of the teachings herein. For example, the process steps set forth above may be performed in a different order. Furthermore, no limitations are intended to the details of construction or design herein shown, other than as described in the claims below. It is therefore evident that the particular embodiments disclosed above may be altered or modified and all such variations are considered within the scope and spirit of the invention. Accordingly, the protection sought herein is as set forth in the claims below.



Claims
  • 1. A weight-on-bit measurement tool, comprising:a body; at least one strain gauge cavity in said body, said strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on said mounting surface when said tool is subjected to said downhole pressures during drilling operations; and a weight-on-bit strain gauge operatively coupled to said mounting face above said region of approximately zero axial strain.
  • 2. The tool of claim 1, further comprising a cover plate positioned in an opening of said cavity.
  • 3. The tool of claim 2, wherein said cover plate and said cavity define a chamber substantially free of liquids.
  • 4. The tool of claim 2, wherein said cavity defines a space that is filled with a liquid.
  • 5. The tool of claim 1, wherein said cavity has a circular cross-sectional configuration.
  • 6. The tool of claim 1, wherein said tool is comprised of at least one of stainless steel, a carbon steel and titanium.
  • 7. The tool of claim 1, wherein said cavity has a circular cross-sectional configuration of a diameter of approximately 1½″ and said mounting face is positioned at a depth of approximately 1⅛″ below an outer surface of said body.
  • 8. The tool of claim 1, wherein said cavity is formed in said body.
  • 9. The tool of claim 1, wherein said cavity is defined, at least partially, by a cavity insert positioned in said body.
  • 10. The tool of claim 9, further comprising an internal passageway formed between an internal bore of said body and said cavity insert.
  • 11. The tool of claim 9, wherein at least a portion of said cavity insert has a conical configuration.
  • 12. A weight-on-bit measurement tool, comprising:a body; at least two strain gauge cavities in said body, each of said strain gauge cavities having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on said mounting surface when said tool is subjected to said downhole pressures during drilling operations; and a weight-on-bit strain gauge operatively coupled to said mounting face above said region of approximately zero axial strain.
  • 13. The tool of claim 12, wherein said cavities are positioned on opposite sides of said tool body.
  • 14. The tool of claim 12, further comprising a cover plate positioned in an opening of each of said cavities.
  • 15. The tool of claim 14, wherein said cover plate and each of said cavities define a chamber substantially free of liquids.
  • 16. The tool of claim 14, wherein each of said cavities a space that is filled with a liquid.
  • 17. The tool of claim 12, wherein each of said cavities have a circular cross-sectional configuration.
  • 18. The tool of claim 12, wherein said tool is comprised of at least one of stainless steel, a carbon steel and titanium.
  • 19. The tool of claim 12, wherein each of said cavities have a circular cross-sectional configuration of a diameter of approximately 1½″ and said mounting face is positioned at a depth of approximately 1⅛″ below an outer surface of said body.
  • 20. The tool of claim 12, wherein each of said cavities are formed in said body.
  • 21. The tool of claim 12, wherein each of said cavities are defined, at least partially, by a cavity insert positioned in said body.
  • 22. The tool of claim 21, further comprising an internal passageway formed between an internal bore of said body and said cavity insert.
  • 23. The tool of claim 21, wherein at least a portion of said cavity insert has a conical configuration.
  • 24. A method, comprising:providing a weight-on-bit measurement tool comprised of: a body; at least one strain gauge cavity in said body, said strain gauge cavity having a strain gauge mounting surface that is located at a position such that a region of approximately zero axial strain due to downhole pressures during drilling operations exists on said mounting surface when said tool is subjected to said downhole pressures during drilling operations; and a weight-on-bit strain gauge operatively coupled to said mounting face above said region of approximately zero axial strain; positioning said tool in a drill string comprised of a drill bit; drilling a well bore with said drill string; and obtaining weight-on-bit measurement data using said weight-on-bit strain gauge in said tool.
  • 25. The method of claim 24, wherein said weight-on-bit measurement data is provided on a real-time basis.
  • 26. The method of claim 24, wherein said weight-on-bit measurement data is provided on a non-real-time basis.
  • 27. The method of claim 24, further comprising a cover plate positioned in an opening of said cavity.
  • 28. The method of claim 27, wherein said cover plate and said cavity define a chamber substantially free of liquids.
  • 29. The method of claim 27, wherein said cavity defines a space that is filled with a liquid.
  • 30. The method of claim 24, wherein said cavity has a circular cross-sectional configuration.
  • 31. The method of claim 24, wherein said tool is comprised of at least one of stainless steel, a carbon steel and titanium.
  • 32. The method of claim 24, wherein said cavity has a circular cross-sectional configuration of a diameter of approximately 1½″ and said mounting face is positioned at a depth of approximately 1⅛″ below an outer surface of said body.
  • 33. The method of claim 24, wherein said cavity is formed in said body.
  • 34. The method of claim 24, wherein said cavity is defined, at least partially, by a cavity insert positioned in said body.
  • 35. The method of claim 34, further comprising an internal passageway formed between an internal bore of said body and said cavity insert.
  • 36. The method of claim 34, wherein at least a portion of said cavity insert has a conical configuration.
  • 37. A method, comprising:identifying a region of approximately zero axial strain due to downhole pressures for a body to be positioned in a drill string when said body is subjected to downhole pressures during drilling operations; providing a strain gauge cavity in said body such that a strain gauge mounting face within said cavity is located at a position wherein said region of approximately zero axial strain exists on said mounting face when said body is subjected to said downhole pressures during said drilling operations; and coupling a weight-on-bit strain gauge to said mounting face above said region of approximately zero axial strain.
  • 38. The method of claim 37, wherein providing a strain gauge cavity in said body comprises machining a cavity in said body.
  • 39. The method of claim 37, wherein providing a strain gauge cavity in said body comprises forming an opening in said body and positioning a cavity insert in said opening.
  • 40. The method of claim 37, further comprising a cover plate positioned in an opening of said cavity.
  • 41. The method of claim 37, wherein said cover plate and said cavity define a chamber substantially free of liquids.
  • 42. The method of claim 37, wherein said cavity defines a space that is filled with a liquid.
  • 43. The method of claim 37, wherein said cavity has a circular cross-sectional configuration.
  • 44. The method of claim 37, wherein said tool is comprised of at least one of stainless steel, a carbon steel and titanium.
  • 45. The method of claim 37, wherein said cavity has a circular cross-sectional configuration of a diameter of approximately 1½″ and said mounting face is positioned at a depth of approximately 1⅛″ below an outer surface of said body.
  • 46. The method of claim 37, wherein said cavity is formed in said body.
  • 47. The method of claim 37, wherein said cavity is defined, at least partially, by a cavity insert positioned in said body.
  • 48. The method of claim 47, further comprising an internal passageway formed between an internal bore of said body and said cavity insert.
  • 49. The method of claim 47, wherein at least a portion of said cavity insert has a conical configuration.
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