The present invention relates to drill bit assemblies, specifically drill bit assemblies for use in subterranean drilling. More particularly the present invention relates to drill bits that include engaging members that degrade the formation through shear and/or compressive forces.
U.S. Pat. No. 7,270,196 to Hall, which is herein incorporated by reference for all that it contains, discloses a drill bit assembly comprising a body portion intermediate a shank portion and a working portion. The working portion has at least one cutting element. The body portion has at least a portion of a reactive jackleg apparatus which has a chamber at least partially disposed within the body portion and a shaft movable disposed within the chamber, the shaft having at least a proximal end and a distal end. The chamber also has an opening proximate the working portion of the assembly.
Also, U.S. Pat. No. 5,038,873 to Jürgens, which is herein incorporated by reference for all that it contains, discloses a drill tool including a retractable pilot drilling unit driven by a fluid operated motor, the motor comprising a stator mounted on the interior of a tubular outer housing and a rotor mounted on the exterior of a tubular inner housing axially supported in said outer housing and rotationally free with respect thereto. The pilot drilling unit is rotationally fixed within the inner housing, but axially moveable therewithin so that pressure of drilling fluid used to drive the motor will also act on reaction surfaces of the pilot drilling unit to urge it axially forward. The top of the pilot drilling unit includes a fishing head for retracting the pilot drilling unit from the drilling tool, and reinserting it therein.
In one aspect of the present invention, a drill bit for downhole drilling comprises a bore, cutting face, and an indenting element. The indenting element is disposed within the bore and comprises a shank connected to a distal end that is configured to engage a downhole formation. A support assembly is disposed within the bore and comprises a ring with a larger diameter than the shank. The support assembly further comprises a plurality of resilient arms which connect the shank to the ring.
The indenting element may be disposed coaxially with the drill bit and configured to protrude from the drill bit's cutting face.
The support assembly may be configured to push the indenting element towards the downhole formation such that an annular surface of the ring contributes to loading the indenting element. A plurality of fluid channels may be disposed intermediate the plurality of resilient arms.
The resilient arms may be configured to act as a spring that vibrates the indenting element or dampens an axial and/or side loads imposed on the indenting element. Instrumentation may be connected to the ring opposite of the indenting element and disposed between the ring and a thrusting surface within the bore. The instrumentation may be connected to a telemetry system or an electronic circuitry system.
The instrumentation may include an actuator and/or a sensor. The actuator may be configured to push off of the thrusting surface and the sensor may use the thrusting surface as a measurement reference. The actuator may comprise a piezoelectric or magnetostrictive material, and may be configured to vibrate the indenting element at a harmonic frequency that promotes destruction of downhole formation. The plurality of resilient arms may be configured to amplify a vibration generated by the actuator. The sensor may comprise a strain gauge or pressure gauge.
In some embodiments, the instrumentation may comprise a plurality of sensors and/or actuators disposed between the ring and the thrusting surface. These actuators and/or sensors may be configured to act together or independently.
In some embodiments, instrumentation may be disposed within each of the plurality of resilient arms. The instrumentation may be configured to move the resilient arms or to record data about the strain in the resilient arms.
In some embodiments, the support assembly may be configured to translate axially with respect to the drill bit. At least one valve may be disposed within the drill bit that controls the axial position of the indenting element by directing drilling fluid to push the indenting element either outwards or inwards.
In another aspect of the present invention, a drilling assembly comprises a drill bit comprising a bit body and a cutting surface. A formation engaging element protrudes from the cutting surface and is configured to engage a formation. At least one compliant member is disposed intermediate the bit body and formation engaging element and is configured to provide compliancy in a lateral direction for the formation engaging element.
The at least one compliant member may be configured to vibrate the formation engaging element or to dampen an axial and/or side load imposed on the formation engaging element. The at least one compliant member may comprise at least one hollow area in its wall thickness that is configured to provide compliance. The at least one hollow area may comprise a generally circular or polygonal cross-section. The at least one compliant member may be press fit into the bit body. A plurality of compliant members may be disposed intermediate the bit body and formation engaging element. The plurality of compliant members may be disposed around and/or behind the formation engaging element.
In some embodiments, the at least one compliant member may comprise a cylindrical shape configured to surround the formation engaging element. In some embodiments, the at least one compliant member may comprise a semi-cylindrical shape.
Instrumentation may be disposed within the at least one compliant member and may be connected to a telemetry system or an electronic circuitry system. The instrumentation may comprise at least one actuator and at least one sensor. The at least one actuator may be configured to pulse the formation engaging element. The at least one sensor may be configured to measure a load on the formation engaging element. The sensor may comprise a strain gauge or a pressure gauge. The instrumentation may comprise a plurality of sensors and/or actuators configured to act together or independently of each other. The instrumentation may also comprise a piezoelectric or magnetostrictive material.
The formation engaging element may comprise a downhole drilling cutting element. The formation engaging element may be press fit into the at least one compliant member.
a is a perspective view of an embodiment of a compliant member.
b is a perspective view of another embodiment of a compliant member.
c is a perspective view of another embodiment of a compliant member.
d is a perspective view of another embodiment of a compliant member.
e is a perspective view of another embodiment of a compliant member.
f is a perspective view of another embodiment of a compliant member.
a is an orthogonal view of an embodiment of a cutting element.
b is a perspective view of another embodiment of a cutting element.
c is a perspective view of another embodiment of a cutting element.
a is a perspective view of another embodiment of a compliant member.
b is a cross-sectional view of another embodiment of a compliant member.
a is a cross-sectional view of another embodiment of a drill bit.
b is a perspective view of another embodiment of a compliant member.
c is a perspective view of another embodiment of a cutting element.
Referring now to the figures,
An indenting element 202 may be disposed coaxially with a rotational axis of the drill bit 103 and configured to protrude from the cutting face 201. By disposing the indenting element 202 coaxial with the drill bit 103, the indenting element 202 may stabilize the downhole tool string and help prevent bit whirl. The indenting element 202 may also increase the drill bit's rate of penetration by focusing the tool string's weight into the formation. During normal drilling operation, the indenting element 202 may be the first to come into contact with the formation and may weaken the formation before the cutters on the drill bit blades engage the formation.
The ring is positioned to abut against a thrusting surface 307 formed in the drill bit 103. It is believed that a ring with a larger diameter than the indenting element is advantageous because the ring's enlarged surface area may pick up more thrust than the indenting element's diameter would otherwise pick up. Therefore, more weight from the drill string may be loaded onto the indenting element.
The distal end 304 of the indenting element 202 may comprise a tip 310 comprising a superhard material. The superhard material may reduce wear on the tip 310 so that the tip 310 has a longer life. The superhard material may comprise polycrystalline diamond, synthetic diamond, vapor deposited diamond, silicon bonded diamond, cobalt bonded diamond, thermally stable diamond, polycrystalline diamond with a binder concentration of 1 to 40 weight percent, infiltrated diamond, layered diamond, monolithic diamond, polished diamond, course diamond, fine diamond, cubic boron nitride, diamond impregnated matrix, diamond impregnated carbide, silicon carbide, metal catalyzed diamond, or combinations thereof.
This embodiment also discloses instrumentation 308 connected to the ring 305. The instrumentation 308 may be disposed opposite of the indenting element 202 and be intermediate the support assembly 301 and the thrusting surface 307. The instrumentation 308 may be connected to a telemetry system or an electronic circuitry system 309 that sends and receives information from the surface or other downhole locations. The instrumentation 308 may be in communication with the indenting element 202 through the resilient arms 306. The instrumentation may perform a variety of functions such as increasing the rate of penetration by vibrating the indenting element. The instrumentation may also be configured to measure the stresses and/or strains in the indenting element and/or support assembly. These measurements may provide information that may contribute to determining the drilling mechanics and/or formation properties.
During normal drilling operations, the downhole formation 105 may push on the indenting element 202. The indenting element 202 may axially retract, forcing the resilient arms 306 to compress. The sensor 501 may capture data by sensing the forces acting on the indenting element 202 and how the resilient arms 306 compress. The data captured by the sensor 501 may result from the axial forces acting on the indenting element 202. The sensor 501 may be in communication with the piezoelectric material 401 such that the sensor 501 sequentially compresses the piezoelectric material 401. When compressed, the piezoelectric material 401 may produce an electrical current 502. The electrical current 502 may be sent through the electronic circuitry system 309 to the surface or may be stored within the downhole drill string.
Now referring to
Further, a compliant support sleeve may dampen the lateral forces on the indenting element, thereby increasing the indenting member's capacity to withstand side loads.
At least one compliant member 1206 may be disposed intermediate the bit body 1203 and the formation engaging element 1202. The compliant member 1206 may be configured to provide compliancy in both axial and lateral directions with respect to the formation engaging element 1202. During normal drilling operations, the formation 1205 may exert forces on the formation engaging element 1202, and the compliant member 1206 dampens these forces on the formation engaging element 1202. In the present embodiment, a plurality of compliant members is disposed around and behind the formation engaging element 1202.
Instrumentation 1207 may be disposed within at least one compliant member 1206. The instrumentation 1207 may comprise at least one actuator and/or sensor. The actuator may be configured to pulse the formation engaging element 1202 to induce a vibration into the formation. In some embodiments, the vibrations may comprise a waveform characteristic that is destructive to the formation. In some embodiments, the actuator may control an angle or precise position of the engaging element. In embodiments where the instrumentation is a sensor, the sensor may be configured to measure loads in at least one direction on the engaging element 1202. The sensor may comprise a strain gauge or a pressure gauge that may capture data about the downhole conditions. In some embodiments, the instrumentation may induce a vibration into the formation, measure the formation's reflected vibration, and induce the formation with an adjusted vibration. In this manner, induced vibrations may be customized for the formation's characteristics.
The instrumentation 1207 may be in communication with a telemetry system or an electronic circuitry system. Information may be passed between surface equipment or data processors within the drill string and the instrumentation 1207. In the present embodiment, the instrumentation 1207 is connected to an electronic circuitry system 1208. The telemetry or electronic circuitry system may pass data from the instrumentation to other components or send control instructions to the instrumentation. The instrumentation 1207 may also comprise a piezoelectric or magnetostrictive material.
a through 13f disclose embodiments of compliant members 1301. Each disclosed embodiment comprises a cylindrical shape configured to surround a formation engaging element. The compliant members may each comprise at least one hollow area 1302, in the wall thickness that is configured to provide compliancy for the formation engaging element. The hollow areas 1302 may provide space for the compliant members 1301 to deform as forces from the downhole formation are exerted on the formation engaging element. Hollow areas may comprise a generally polygonal or a generally circular cross-section.
a through 16c disclose embodiments of a shear cutter 1503 that may be compatible with the present invention.
The cutting face 1601 may be disposed on a substrate 1603 and the substrate 1603 may be brazed onto the cutter body 1602 at a braze joint 1650.
a and 17b disclose embodiments of the compliant member 1504. The compliant member 1504 may comprise instrumentation 1701 comprising a plurality of sensors and/or actuators. The plurality of sensors and/or actuators may be configured to act together or independently of each other. Electrical wiring 1703 may connect the instrumentation in each hollow area 1702.
a through 18c disclose an embodiment of a formation engaging element 1802 and a compliant member 1803. The formation engaging element 1802 may comprise a shear cutter 1810 comprising a cutting face 1804 and a substrate 1805. The shear cutter 1810 may be positioned on the drill bit 1801 such that at least part of the substrate's diameter may be exposed to the formation. The compliant member 1803 may comprise a semi-cylindrical shape to surround just a part of the substrate's diameter. In this embodiment, the compliant member will be away from the engagement point between the engaging member and the formation. However, this shape may still provide sufficient contact with the drill bit's blade to dampen and/or measure side load forces.
Whereas the present invention has been described in particular relation to the drawings attached hereto, it should be understood that other and further modifications apart from those shown or suggested herein, may be made within the scope and spirit of the present invention.
This application is a continuation-in-part of U.S. patent application Ser. No. 12/619,305, filed Nov. 16, 2009 which is a continuation-in-part of U.S. patent application Ser. No. 11/766,975 and was filed on Jun. 22, 2007. This application is also a continuation-in-part of U.S. patent application Ser. No. 11/774,227 now U.S. Pat. No. 7,669,938 which was filed on Jul. 6, 2007. U.S. patent application Ser. No. 11/774,227 is a continuation-in-part of U.S. patent application Ser. No. 11/773,271 now U.S. Pat. No. 7,997,661 which was filed on Jul. 3, 2007. U.S. patent application Ser. No. 11/773,271 is a continuation-in-part of U.S. patent application Ser. No. 11/766,903 filed on Jun. 22, 2007. U.S. patent application Ser. No. 11/766,903 is a continuation of U.S. patent application Ser. No. 11/766,865 filed on Jun. 22, 2007. U.S. patent application Ser. No. 11/766,865 is a continuation-in-part of U.S. patent application Ser. No. 11/742,304 now U.S. Pat. No. 7,475,948 which was filed on Apr. 30, 2007. U.S. patent application Ser. No. 11/742,304 is a continuation of U.S. patent application Ser. No. 11/742,261 now U.S. Pat. No. 7,469,971 which was filed on Apr. 30, 2007. U.S. patent application Ser. No. 11/742,261 is a continuation-in-part of U.S. patent application Ser. No. 11/464,008 now U.S. Pat. No. 7,338,135 which was filed on Aug. 11, 2006. U.S. patent application Ser. No. 11/464,008 is a continuation-in-part of U.S. patent application Ser. No. 11/463,998 now U.S. Pat. No. 7,384,105 which was filed on Aug. 11, 2006. U.S. patent application Ser. No. 11/463,998 is a continuation-in-part of U.S. patent application Ser. No. 11/463,990 now U.S. Pat. No. 7,320,505 which was filed on Aug. 11, 2006. U.S. patent application Ser. No. 11/463,990 is a continuation-in-part of U.S. patent application Ser. No. 11/463,975 now U.S. Pat. No. 7,445,294 which was filed on Aug. 11, 2006. U.S. patent application Ser. No. 11/463,975 is a continuation-in-part of U.S. patent application Ser. No. 11/463,962 now U.S. Pat. No. 7,413,256 which was filed on Aug. 11, 2006. U.S. patent application Ser. No. 11/463,962 is a continuation-in-part of U.S. patent application Ser. No. 11/463,953, now U.S. Pat. No. 7,464,993 which was also filed on Aug. 11, 2006. The present application is also a continuation-in-part of U.S. patent application Ser. No. 11/695,672 now U.S. Pat. No. 7,396,086 which was filed on Apr. 3, 2007. U.S. patent application Ser. No. 11/695,672 is a continuation-in-part of U.S. patent application Ser. No. 11/686,831 now U.S. Pat. No. 7,568,770 filed on Mar. 15, 2007. This application is also a continuation in part of U.S. patent application Ser. No. 11/673,634 filed Feb. 12, 2007 now U.S. Pat. No. 8,109,349. All of these applications are herein incorporated by reference for all that they contain.
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Number | Date | Country | |
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20110180324 A1 | Jul 2011 | US |
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Number | Date | Country | |
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Parent | 11463998 | Aug 2006 | US |
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Parent | 11463975 | Aug 2006 | US |
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Parent | 11463962 | Aug 2006 | US |
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Parent | 11695672 | Apr 2007 | US |
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