US20120061094A1 - Ball-seat apparatus and method - Google Patents
Ball-seat apparatus and method Download PDFInfo
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- US20120061094A1 US20120061094A1 US12/880,853 US88085310A US2012061094A1 US 20120061094 A1 US20120061094 A1 US 20120061094A1 US 88085310 A US88085310 A US 88085310A US 2012061094 A1 US2012061094 A1 US 2012061094A1
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- 239000012530 fluid Substances 0.000 claims abstract description 77
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- 239000000969 carrier Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 239000011800 void material Substances 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000004035 construction material Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
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- 230000004048 modification Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
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Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B34/00—Valve arrangements for boreholes or wells
- E21B34/06—Valve arrangements for boreholes or wells in wells
- E21B34/14—Valve arrangements for boreholes or wells in wells operated by movement of tools, e.g. sleeve valves operated by pistons or wire line tools
- E21B34/142—Valve arrangements for boreholes or wells in wells operated by movement of tools, e.g. sleeve valves operated by pistons or wire line tools unsupported or free-falling elements, e.g. balls, plugs, darts or pistons
Definitions
- Ball-seat assemblies are used with, for example, hydraulic disconnects, circulating subs and inflatable packers.
- Actuation of a ball-seat assembly generally includes releasing a ball or other plug into a fluid conduit and allowing the ball to drop or be pumped onto the ball seat and restrict fluid flow therein.
- the impact between the ball and the ball seat can produce pressure waves, which can cause wear and/or damage to components of the assembly, vibrations and tubing failure.
- fluid in downhole applications can be pumped at rates of up to about 80 bbl/min, which can cause an enormous pressure surge upon impact of a plug or ball on a seat, which causes wear and potential damage to downhole components.
- An apparatus for restricting fluid flow includes: a ball receiving element disposed in a fluid conduit and configured to receive a ball that has been advanced through the fluid conduit and at least partially restrict fluid flow, the fluid conduit having a longitudinal axis; and at least one feature disposed at the fluid conduit and configured to at least one of reduce a rate of deceleration of the ball due to actuation of the apparatus and reduce pressure waves generated by an impact between the ball and the ball receiving element.
- a method of restricting fluid flow includes: releasing a ball into a fluid conduit and receiving the ball in a ball receiving element disposed at the fluid conduit and at least partially restricting fluid flow, the fluid conduit having a longitudinal axis; and at least one of reducing a rate of deceleration of the ball due to actuation of the apparatus and reducing pressure waves generated by an impact between the ball and the ball receiving element by at least one feature disposed at the fluid conduit.
- FIG. 1 is a cross-sectional view of an embodiment of a ball-seat assembly
- FIG. 2 is a partial cross-sectional view of an embodiment of the ball-seat assembly of FIG. 1 ;
- FIG. 3 is a perspective view of another embodiment of the ball-seat assembly of FIG. 1 ;
- FIG. 4 is a flow diagram depicting a method of restricting fluid flow in a conduit.
- a ball seat assembly includes a ball receiving element such as a ball seat.
- the ball seat includes a plurality of axially offset ball seat assemblies or seating components disposed at a fluid conduit and protruding at least partially into the fluid conduit.
- each seating component has a cross-sectional shape that is contoured to create one or more fluid passageways when a ball contacts the seating component.
- the contoured seating components may be circumferentially offset so that a portion of the fluid in the conduit flows through the ball seat as the ball contacts each seating component.
- one or more of the seating components is axially contoured and/or compliant to reduce the impact of the ball on each component and control the reduction in velocity resulting from contact with each seating component.
- the configuration of the seating components acts to incrementally slow the ball as it engages the ball seat and may also incrementally reduce fluid flow as the ball is seated to reduce impact on the ball seat assembly and reduce pressure waves resulting from the ball-seat impact.
- a downhole tool 10 such as a ball seat sub, configured to be disposed in a borehole 11 , includes a housing 12 having a longitudinal bore or fluid conduit 14 .
- a ball seat assembly includes a ball seat 16 included in the conduit 14 to retain a ball 18 that is released into the conduit 14 .
- the ball 18 is a spherical metal or plastic plug, although “ball” may refer to any type of moveable or droppable plugging element, such as a drop plug, and may take any desired shape or size.
- Actuation of the ball seat assembly includes releasing the ball into the fluid conduit 14 , for example by dropping the ball 18 into and/or pumping the ball 18 through the fluid conduit 14 from a surface or downhole location.
- axial refers to a direction that is at least generally parallel to a central longitudinal axis of the conduit 14 .
- Ring refers to a direction along a line that is orthogonal to the longitudinal axis and extends from the longitudinal axis.
- downstream refers to the direction of movement of the ball and/or the downhole fluid
- upstream refers to a direction opposite the direction of movement of the ball and/or the downhole fluid.
- the ball seat 16 includes a plurality of axially offset seating members or seating components 22 disposed at the conduit 14 and protruding radially into the conduit 14 .
- the plurality of seating components 22 include one or more upstream seating components, such as seating component 24 , axially disposed relative to a downstream seating component, such as seating component 26 , to create an axial contouring that reduces the overall deceleration of the ball 18 and brings the ball 18 to a relatively gentle stop. This in turn reduces the amplitude of pressure waves due to an incremental or fractional change in velocity of the ball 18 .
- the ball seat 16 and/or seating components 22 are directly disposed on and/or attached to the inner surface of the conduit 14 or is formed from a reduced diameter portion of the conduit 14 .
- the ball seat 16 is disposed on or is part of a movable component such as a sliding sleeve or other movable seat carrier 20 for use, for example, as an actuator or valve.
- the plurality of seating components 22 reduces the total rate of deceleration and increases the time rate of ball seat assembly closure during actuation of the ball seat assembly. Seating loads can thereby be reduced as they depend on the time rate of velocity change.
- the ball 18 is slowed in several increments, defined by the initial velocity of the ball 18 , the resistance to movement of the seating components 22 , and the axial as well as any radial offset between the components.
- the number of increments can be represented by:
- ⁇ v is the total change in velocity
- ⁇ v i is the change in velocity for each incremental closure “i” of the flow passage.
- Each closure may correspond to one or more seating components 22 contacting the ball 18 . Since the ball impact load and the surge pressures are proportional to change in velocity, the loading occurs in this embodiment in small increments, resulting in smaller pressure waves, instead of the total loading being applied all at once.
- At least one seating component 22 has a cross-sectional profile, i.e., a profile in a plane at least partially orthogonal to the longitudinal axis of the conduit 14 , so that contact between the ball 18 and the seating component only partially stops fluid flow as the ball 18 moves downstream.
- one or more of the seating components 22 has a cross sectional shape configured to form one or more conduits, or passageways upon contact with the ball 18 . The passageways are configured to allow fluid flow therethrough when the ball is in contact with a respective seating component 22 . In this way, as the ball 18 contacts each seating component 22 , fluid voids are formed that allow a portion of the fluid to pass through, thereby disrupting or otherwise reducing the effect of pressure waves produced during ball-seat impact.
- seating components 24 and 26 each include a plurality of circumferentially arrayed protrusions or members extending into the conduit 14 .
- the separation between adjacent members forms a fluid void formed when the ball 18 contacts each assembly.
- the assemblies 24 and 26 are circumferentially offset so that contact with the upstream seating component 24 forms a fluid void, and as the ball 18 advances further along the ball seat 16 and contacts the downstream component 26 , the fluid voids may be closed to fully cut off fluid flow through the ball seat 16 .
- the fluid voids in each seating component 24 , 26 are circumferentially offset or otherwise arranged relative to other seating components so that in each successive contact closure the flow velocity and volume reduces fractionally rather than all at once.
- the ball seat 16 includes at least one additional seating component 28 axially offset at least one of the other seating components 24 , 26 .
- Each component 24 , 26 and 28 is sequentially contacted by the ball 18 during actuation, and the ball 18 is thus incrementally slowed until it comes to a stop and is seated.
- each seating component is circumferentially offset from an axially adjacent seating component, so that the fluid voids formed become incrementally smaller as the ball 18 advances through the ball seat 16 .
- the ball 18 has a circumference sufficient so that the ball 18 remains in contact with each seating component 22 as it advances through the ball seat 16 .
- the seating components are circumferentially offset so that when the ball 18 comes to a rest and is seated, the ball 18 is in continuous circumferential contact with the seating components 22 so that fluid flow is completely cut off
- Each successive seating component can be configured to control the incremental reduction in velocity of the ball 18 .
- each seating component 22 may have a selected resistance to movement that causes the ball 18 to reduce its velocity by a desired amount. “Resistance to movement” may include a stiffness, compliance or elasticity of each component or constituent member, a mechanical resistance generated by a spring or other device, or an axial shape of the seating component.
- a seating component 22 may include an internal spring.
- a seating component 22 may have a selected axial contour, such as a gradual increase in radial extension as the seating component (e.g., an elliptical shape as shown in FIGS. 1-3 ) extends axially downstream.
- the resistance to movement and/or contour may be selected so that the seating components 22 have the same or varying resistances to movement to control the incremental velocity changes.
- the reduction of velocity may depend on the geometrical profiles of the seating components 22 and the ball 18 (or other plugging device), the axial and angular spacing of the seating components 22 , the load-deformation behavior of the contacting bodies, and/or fluid flow rates.
- the seating components 22 are not limited to the embodiments described herein, and may take any shape or configuration suitable for gradually or incrementally slowing the ball as it engages the ball seat 16 .
- Examples of such configurations include a ring-shaped or toroidal elastic seat disposed on an interior surface, resilient flaps, and resistant mechanisms such as spring loaded and/or articulated member that protrude into the conduit 14 and having a selected resistance to movement.
- the seating components may be formed from an axial contour or shape of a single seating component.
- the downhole tool 10 is not limited to that described herein.
- the downhole tool 10 may include any tool, carrier or component that includes a ball seat assembly.
- the carriers described herein, such as a production string and a screen, are not limited to the specific embodiments disclosed herein.
- a “carrier” as described herein means any device, device component, combination of devices, media and/or member that may be used to convey, house, support or otherwise facilitate the use of another device, device component, combination of devices, media and/or member.
- Exemplary non-limiting carriers include borehole strings of the coiled tube type, of the jointed pipe type and any combination or portion thereof.
- Other carrier examples include casing pipes, wirelines, wireline sondes, slickline sondes, drop shots, downhole subs, bottom-hole assemblies, and drill strings.
- the tool 10 is not limited to components configured for downhole use.
- FIG. 4 illustrates a method 40 of restricting fluid flow in a component.
- the method includes, for example, actuating a valve or packer in a downhole assembly.
- the method 40 includes one or more stages 41 - 43 .
- the method is described in conjunction with the tool 10 and the ball seat 16 , the method can be utilized in conjunction with any device or system (configured for downhole or surface use) that utilizes a ball-seat assembly.
- the tool 10 is disposed at a downhole location, via for example a borehole string or wireline.
- the ball-seat assembly is actuated by releasing the ball 18 into the conduit 14 , for example by dropping the ball 18 into the conduit 14 and/or pumping the ball 18 through the conduit 14 .
- the ball 18 advances through the conduit 14 and engages the ball seat 16 .
- the ball 18 is incrementally slowed by the seating components 24 , 26 and/or 28 .
- the ball 18 comes to a stop, and fluid flow is completely cut off or reduced by a selected amount.
- the systems and methods described herein provide various advantages over existing processing methods and devices.
- the systems and methods result in a more gradual reduction in impact velocity versus instantaneous arrest and reduces pressure waves formed by ball-seat impact. This in turn reduces damage to the ball seat assembly and improves reliability, and can enable the use of a wider range of construction materials and reduce the complexity of ball-seat design, for example by reducing the need for relatively complex ball seat designs to reduce impact.
- Reduced pressure wave loading can also reduce the burst or collapse loading on downhole tubing.
- the apparatuses described herein provide an alternative lower complexity design relative to prior art applications such as embedded springs.
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Abstract
An apparatus for restricting fluid flow includes: a ball receiving element disposed in a fluid conduit and configured to receive a ball that has been advanced through the fluid conduit and at least partially restrict fluid flow, the fluid conduit having a longitudinal axis; and at least one feature disposed at the fluid conduit and configured to at least one of reduce a rate of deceleration of the ball due to actuation of the apparatus and reduce pressure waves generated by an impact between the ball and the ball receiving element.
Description
- In the drilling and completion industry and for example in hydrocarbon exploration and recovery operations, a variety of components and tools are lowered into a borehole for various operations such as production operations, for example. Some downhole tools utilize ball-seat assemblies to act as a valve or actuator. Ball-seat assemblies are used with, for example, hydraulic disconnects, circulating subs and inflatable packers.
- Actuation of a ball-seat assembly generally includes releasing a ball or other plug into a fluid conduit and allowing the ball to drop or be pumped onto the ball seat and restrict fluid flow therein. The impact between the ball and the ball seat can produce pressure waves, which can cause wear and/or damage to components of the assembly, vibrations and tubing failure. For example, fluid in downhole applications can be pumped at rates of up to about 80 bbl/min, which can cause an enormous pressure surge upon impact of a plug or ball on a seat, which causes wear and potential damage to downhole components.
- An apparatus for restricting fluid flow includes: a ball receiving element disposed in a fluid conduit and configured to receive a ball that has been advanced through the fluid conduit and at least partially restrict fluid flow, the fluid conduit having a longitudinal axis; and at least one feature disposed at the fluid conduit and configured to at least one of reduce a rate of deceleration of the ball due to actuation of the apparatus and reduce pressure waves generated by an impact between the ball and the ball receiving element.
- A method of restricting fluid flow includes: releasing a ball into a fluid conduit and receiving the ball in a ball receiving element disposed at the fluid conduit and at least partially restricting fluid flow, the fluid conduit having a longitudinal axis; and at least one of reducing a rate of deceleration of the ball due to actuation of the apparatus and reducing pressure waves generated by an impact between the ball and the ball receiving element by at least one feature disposed at the fluid conduit.
- The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
-
FIG. 1 is a cross-sectional view of an embodiment of a ball-seat assembly; -
FIG. 2 is a partial cross-sectional view of an embodiment of the ball-seat assembly ofFIG. 1 ; -
FIG. 3 is a perspective view of another embodiment of the ball-seat assembly ofFIG. 1 ; and -
FIG. 4 is a flow diagram depicting a method of restricting fluid flow in a conduit. - The apparatuses, systems and methods described herein provide for the reduction of a ball-seat impact and the mitigation of pressure waves caused by actuation of a ball-seat assembly. A ball seat assembly includes a ball receiving element such as a ball seat. The ball seat includes a plurality of axially offset ball seat assemblies or seating components disposed at a fluid conduit and protruding at least partially into the fluid conduit. In one embodiment, each seating component has a cross-sectional shape that is contoured to create one or more fluid passageways when a ball contacts the seating component. The contoured seating components may be circumferentially offset so that a portion of the fluid in the conduit flows through the ball seat as the ball contacts each seating component. In one embodiment, one or more of the seating components is axially contoured and/or compliant to reduce the impact of the ball on each component and control the reduction in velocity resulting from contact with each seating component. The configuration of the seating components acts to incrementally slow the ball as it engages the ball seat and may also incrementally reduce fluid flow as the ball is seated to reduce impact on the ball seat assembly and reduce pressure waves resulting from the ball-seat impact.
- Referring to
FIG. 1 , a downhole tool 10, such as a ball seat sub, configured to be disposed in aborehole 11, includes ahousing 12 having a longitudinal bore orfluid conduit 14. A ball seat assembly includes aball seat 16 included in theconduit 14 to retain aball 18 that is released into theconduit 14. In one embodiment, theball 18 is a spherical metal or plastic plug, although “ball” may refer to any type of moveable or droppable plugging element, such as a drop plug, and may take any desired shape or size. Actuation of the ball seat assembly includes releasing the ball into thefluid conduit 14, for example by dropping theball 18 into and/or pumping theball 18 through thefluid conduit 14 from a surface or downhole location. Theball 18 falls and/or is advanced by downhole fluid toward theball seat 16 and is seated on theball seat 16 to restrict fluid flow through theconduit 14. As described herein, “axial” refers to a direction that is at least generally parallel to a central longitudinal axis of theconduit 14. “Radial” refers to a direction along a line that is orthogonal to the longitudinal axis and extends from the longitudinal axis. As described herein, “downstream” refers to the direction of movement of the ball and/or the downhole fluid, and “upstream” refers to a direction opposite the direction of movement of the ball and/or the downhole fluid. - Referring to
FIG. 2 , theball seat 16 includes a plurality of axially offset seating members orseating components 22 disposed at theconduit 14 and protruding radially into theconduit 14. The plurality ofseating components 22 include one or more upstream seating components, such asseating component 24, axially disposed relative to a downstream seating component, such asseating component 26, to create an axial contouring that reduces the overall deceleration of theball 18 and brings theball 18 to a relatively gentle stop. This in turn reduces the amplitude of pressure waves due to an incremental or fractional change in velocity of theball 18. The reduction in amplitude reduces impact loading between theball 18 and theball seat 16, which reduces pressure waves, wear on the ball seat assembly and the potential for damage to the ball seat assembly. In one embodiment, theball seat 16 and/orseating components 22 are directly disposed on and/or attached to the inner surface of theconduit 14 or is formed from a reduced diameter portion of theconduit 14. In one embodiment, theball seat 16 is disposed on or is part of a movable component such as a sliding sleeve or othermovable seat carrier 20 for use, for example, as an actuator or valve. - The plurality of
seating components 22 reduces the total rate of deceleration and increases the time rate of ball seat assembly closure during actuation of the ball seat assembly. Seating loads can thereby be reduced as they depend on the time rate of velocity change. In one embodiment, theball 18 is slowed in several increments, defined by the initial velocity of theball 18, the resistance to movement of theseating components 22, and the axial as well as any radial offset between the components. The number of increments can be represented by: -
Δv=ΣΔv i, - where “Δv” is the total change in velocity, and “Δvi” is the change in velocity for each incremental closure “i” of the flow passage. Each closure may correspond to one or
more seating components 22 contacting theball 18. Since the ball impact load and the surge pressures are proportional to change in velocity, the loading occurs in this embodiment in small increments, resulting in smaller pressure waves, instead of the total loading being applied all at once. - In one embodiment, at least one
seating component 22 has a cross-sectional profile, i.e., a profile in a plane at least partially orthogonal to the longitudinal axis of theconduit 14, so that contact between theball 18 and the seating component only partially stops fluid flow as theball 18 moves downstream. In one embodiment, one or more of theseating components 22 has a cross sectional shape configured to form one or more conduits, or passageways upon contact with theball 18. The passageways are configured to allow fluid flow therethrough when the ball is in contact with arespective seating component 22. In this way, as theball 18 contacts eachseating component 22, fluid voids are formed that allow a portion of the fluid to pass through, thereby disrupting or otherwise reducing the effect of pressure waves produced during ball-seat impact. - For example, as shown in
FIG. 3 ,seating components conduit 14. The separation between adjacent members forms a fluid void formed when theball 18 contacts each assembly. - In one embodiment, as shown in
FIG. 3 , theassemblies upstream seating component 24 forms a fluid void, and as theball 18 advances further along theball seat 16 and contacts thedownstream component 26, the fluid voids may be closed to fully cut off fluid flow through theball seat 16. The fluid voids in eachseating component - In one embodiment, the
ball seat 16 includes at least oneadditional seating component 28 axially offset at least one of theother seating components component ball 18 during actuation, and theball 18 is thus incrementally slowed until it comes to a stop and is seated. In one embodiment, each seating component is circumferentially offset from an axially adjacent seating component, so that the fluid voids formed become incrementally smaller as theball 18 advances through theball seat 16. In one embodiment, theball 18 has a circumference sufficient so that theball 18 remains in contact with eachseating component 22 as it advances through theball seat 16. In one embodiment, the seating components are circumferentially offset so that when theball 18 comes to a rest and is seated, theball 18 is in continuous circumferential contact with theseating components 22 so that fluid flow is completely cut off - Each successive seating component can be configured to control the incremental reduction in velocity of the
ball 18. For example, eachseating component 22 may have a selected resistance to movement that causes theball 18 to reduce its velocity by a desired amount. “Resistance to movement” may include a stiffness, compliance or elasticity of each component or constituent member, a mechanical resistance generated by a spring or other device, or an axial shape of the seating component. In one example, aseating component 22 may include an internal spring. In another example, aseating component 22 may have a selected axial contour, such as a gradual increase in radial extension as the seating component (e.g., an elliptical shape as shown inFIGS. 1-3 ) extends axially downstream. The resistance to movement and/or contour may be selected so that theseating components 22 have the same or varying resistances to movement to control the incremental velocity changes. The reduction of velocity may depend on the geometrical profiles of theseating components 22 and the ball 18 (or other plugging device), the axial and angular spacing of theseating components 22, the load-deformation behavior of the contacting bodies, and/or fluid flow rates. - The
seating components 22 are not limited to the embodiments described herein, and may take any shape or configuration suitable for gradually or incrementally slowing the ball as it engages theball seat 16. Examples of such configurations include a ring-shaped or toroidal elastic seat disposed on an interior surface, resilient flaps, and resistant mechanisms such as spring loaded and/or articulated member that protrude into theconduit 14 and having a selected resistance to movement. In other embodiments, the seating components may be formed from an axial contour or shape of a single seating component. - The downhole tool 10 is not limited to that described herein. The downhole tool 10 may include any tool, carrier or component that includes a ball seat assembly. The carriers described herein, such as a production string and a screen, are not limited to the specific embodiments disclosed herein. A “carrier” as described herein means any device, device component, combination of devices, media and/or member that may be used to convey, house, support or otherwise facilitate the use of another device, device component, combination of devices, media and/or member. Exemplary non-limiting carriers include borehole strings of the coiled tube type, of the jointed pipe type and any combination or portion thereof. Other carrier examples include casing pipes, wirelines, wireline sondes, slickline sondes, drop shots, downhole subs, bottom-hole assemblies, and drill strings. In addition, the tool 10 is not limited to components configured for downhole use.
-
FIG. 4 illustrates amethod 40 of restricting fluid flow in a component. The method includes, for example, actuating a valve or packer in a downhole assembly. Themethod 40 includes one or more stages 41-43. Although the method is described in conjunction with the tool 10 and theball seat 16, the method can be utilized in conjunction with any device or system (configured for downhole or surface use) that utilizes a ball-seat assembly. - In the first stage 41, in one embodiment, the tool 10 is disposed at a downhole location, via for example a borehole string or wireline. In the
second stage 42, the ball-seat assembly is actuated by releasing theball 18 into theconduit 14, for example by dropping theball 18 into theconduit 14 and/or pumping theball 18 through theconduit 14. Theball 18 advances through theconduit 14 and engages theball seat 16. In thethird stage 43, theball 18 is incrementally slowed by theseating components seating component 26 or 28), theball 18 comes to a stop, and fluid flow is completely cut off or reduced by a selected amount. - The systems and methods described herein provide various advantages over existing processing methods and devices. The systems and methods result in a more gradual reduction in impact velocity versus instantaneous arrest and reduces pressure waves formed by ball-seat impact. This in turn reduces damage to the ball seat assembly and improves reliability, and can enable the use of a wider range of construction materials and reduce the complexity of ball-seat design, for example by reducing the need for relatively complex ball seat designs to reduce impact. Reduced pressure wave loading can also reduce the burst or collapse loading on downhole tubing. Furthermore, the apparatuses described herein provide an alternative lower complexity design relative to prior art applications such as embedded springs.
- While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications will be appreciated by those skilled in the art to adapt a particular instrument, situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention.
Claims (20)
1. An apparatus for restricting fluid flow, comprising:
a ball receiving element disposed in a fluid conduit and configured to receive a ball that has been advanced through the fluid conduit and at least partially restrict fluid flow, the fluid conduit having a longitudinal axis; and
at least one feature disposed at the fluid conduit and configured to at least one of reduce a rate of deceleration of the ball due to actuation of the apparatus and reduce pressure waves generated by an impact between the ball and the ball receiving element.
2. The apparatus of claim 1 , wherein the at least one feature is included in the ball receiving element, and the at least one feature includes:
at least one first seating component disposed at the conduit and protruding radially into the conduit, the at least one first seating component configured to contact the ball and reduce a velocity of the ball; and
a second seating component protruding radially into the conduit and disposed at a downstream location relative to the first seating assembly, the second seating assembly configured to prevent downstream movement of the ball.
3. The apparatus of claim 2 , wherein the at least one first seating component has a cross-sectional shape configured to form one or more first fluid passageways therethrough upon contact with the ball.
4. The apparatus of claim 3 , wherein the at least one first seating component includes a plurality of axially successive circumferentially offset seating components.
5. The apparatus of claim 4 , wherein respective fluid passageways in each of the plurality of seating components are offset from one another so that a total cross-sectional area of the fluid passageways successively decreases as the ball advances through the ball receiving element.
6. The apparatus of claim 3 , wherein the second seating component has a cross-sectional shape configured to form one or more second fluid passageways therethrough upon contact with the ball, and the second fluid passageways are circumferentially offset relative to the one or more first fluid passageways.
7. The apparatus of claim 6 , wherein the ball forms a complete fluid seal with the first and second seating components when seated.
8. The apparatus of claim 3 , wherein the at least one first seating component includes a plurality of first axially tapered members, each first axially tapered member arranged circumferentially and forming a first fluid passage with an adjacent first tapered member.
9. The apparatus of claim 8 , wherein the second seating component includes a plurality of second axially tapered members circumferentially offset relative to the plurality of first members, each second axially tapered member arranged circumferentially and forming a second fluid passage with an adjacent second tapered member.
10. The apparatus of claim 2 , wherein each of the first and second seating components have an axial contour that increases gradually in the downstream direction.
11. The apparatus of claim 2 , wherein each of the at least one first seating component and the second seating component include at least one of a selected resistance to movement and axial contour configured to reduce a velocity of the ball by a selected amount upon contact with the ball.
12. The apparatus of claim 11 , wherein at least one of the resistance to movement and the axial contour of the second seating component is sufficient to stop the ball after contact with the first seating component.
13. A method of restricting fluid flow, comprising:
releasing a ball into a fluid conduit and receiving the ball in a ball receiving element disposed at the fluid conduit and at least partially restricting fluid flow, the fluid conduit having a longitudinal axis; and
at least one of reducing a rate of deceleration of the ball due to actuation of the apparatus and reducing pressure waves generated by an impact between the ball and the ball receiving element by at least one feature disposed at the fluid conduit.
14. The method of claim 13 , wherein the at least one feature is included in the ball receiving element, and the at least one feature includes:
at least one first seating component disposed at the conduit and protruding radially into the conduit, the at least one first seating component configured to contact the ball and reduce a velocity of the ball; and
a second seating component protruding radially into the conduit and disposed at a downstream location relative to the first seating component, the second seating component configured to prevent downstream movement of the ball.
15. The method of claim 14 , further comprising reducing a velocity of the ball in successive increments by successively contacting the first seating component and the second seating component by the ball as the ball engages the ball receiving element.
16. The method of claim 14 , wherein the at least one first seating component has a cross-sectional shape configured to form one or more first fluid passageways therethrough upon contact with the ball.
17. The method of claim 16 , further comprising reducing a fluid flow through the ball seat in successive increments by successively contacting the first seating component and the second seating component by the ball as the ball engages the ball receiving element.
18. The method of claim 17 , wherein the ball forms a complete fluid seal with the first and second seating components when seated.
19. The method of claim 16 , wherein the at least one first seating component includes a plurality of axially successive circumferentially offset seating components, and respective fluid passageways in each of the plurality of seating components are offset from one another so that a total cross-sectional area of the respective fluid passageways successively decreases as the ball advances through the ball receiving element.
20. The method of claim 16 , wherein the second seating component has a cross-sectional shape configured to form one or more second fluid passageways therethrough upon contact with the ball, and the one or more second fluid passageways are circumferentially offset relative to the one or more first fluid passageways.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/880,853 US20120061094A1 (en) | 2010-09-13 | 2010-09-13 | Ball-seat apparatus and method |
PCT/US2011/043039 WO2012036774A1 (en) | 2010-09-13 | 2011-07-06 | Ball-seat apparatus and method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/880,853 US20120061094A1 (en) | 2010-09-13 | 2010-09-13 | Ball-seat apparatus and method |
Publications (1)
Publication Number | Publication Date |
---|---|
US20120061094A1 true US20120061094A1 (en) | 2012-03-15 |
Family
ID=45805541
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/880,853 Abandoned US20120061094A1 (en) | 2010-09-13 | 2010-09-13 | Ball-seat apparatus and method |
Country Status (2)
Country | Link |
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US (1) | US20120061094A1 (en) |
WO (1) | WO2012036774A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015094241A1 (en) * | 2013-12-18 | 2015-06-25 | Halliburton Energy Services Inc. | Decelerator device for ball activated downhole tools |
CN111058826A (en) * | 2019-12-12 | 2020-04-24 | 陕西延长石油(集团)有限责任公司研究院 | Method for calculating impact speed and impact force of oil well pipe rod |
US20240133266A1 (en) * | 2022-10-19 | 2024-04-25 | Deltatek Oil Tools Limited | Downhole sealing apparatus |
Citations (3)
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---|---|---|---|---|
US6848511B1 (en) * | 2002-12-06 | 2005-02-01 | Weatherford/Lamb, Inc. | Plug and ball seat assembly |
US20060243455A1 (en) * | 2003-04-01 | 2006-11-02 | George Telfer | Downhole tool |
US20090065257A1 (en) * | 2005-06-21 | 2009-03-12 | Joe Noske | Apparatus and methods for utilizing a downhole deployment valve |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6634428B2 (en) * | 2001-05-03 | 2003-10-21 | Baker Hughes Incorporated | Delayed opening ball seat |
GB0409619D0 (en) * | 2004-04-30 | 2004-06-02 | Specialised Petroleum Serv Ltd | Valve seat |
US7673677B2 (en) * | 2007-08-13 | 2010-03-09 | Baker Hughes Incorporated | Reusable ball seat having ball support member |
US7628210B2 (en) * | 2007-08-13 | 2009-12-08 | Baker Hughes Incorporated | Ball seat having ball support member |
-
2010
- 2010-09-13 US US12/880,853 patent/US20120061094A1/en not_active Abandoned
-
2011
- 2011-07-06 WO PCT/US2011/043039 patent/WO2012036774A1/en active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6848511B1 (en) * | 2002-12-06 | 2005-02-01 | Weatherford/Lamb, Inc. | Plug and ball seat assembly |
US20060243455A1 (en) * | 2003-04-01 | 2006-11-02 | George Telfer | Downhole tool |
US20090065257A1 (en) * | 2005-06-21 | 2009-03-12 | Joe Noske | Apparatus and methods for utilizing a downhole deployment valve |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015094241A1 (en) * | 2013-12-18 | 2015-06-25 | Halliburton Energy Services Inc. | Decelerator device for ball activated downhole tools |
US20160177656A1 (en) * | 2013-12-18 | 2016-06-23 | Halliburton Energy Services Inc. | Decelerator device for ball activated downhole tools |
CN111058826A (en) * | 2019-12-12 | 2020-04-24 | 陕西延长石油(集团)有限责任公司研究院 | Method for calculating impact speed and impact force of oil well pipe rod |
US20240133266A1 (en) * | 2022-10-19 | 2024-04-25 | Deltatek Oil Tools Limited | Downhole sealing apparatus |
Also Published As
Publication number | Publication date |
---|---|
WO2012036774A1 (en) | 2012-03-22 |
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Legal Events
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Owner name: BAKER HUGHES INCORPORATED, TEXAS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SONI, MOHAN;AGRAWAL, GAURAV;SIGNING DATES FROM 20100928 TO 20101001;REEL/FRAME:025422/0864 |
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STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |