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:
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
Referring to
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, 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:
Δv=ΣΔvi,
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 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.
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 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. In one embodiment, 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.
For example, as shown in
In one embodiment, as shown in
In one embodiment, 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. 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 the ball 18 advances through the ball seat 16. In one embodiment, 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. In one embodiment, 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. For example, 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. In one example, a seating component 22 may include an internal spring. In another example, 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
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. 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.
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 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. In the third stage 43, the ball 18 is incrementally slowed by the seating components 24, 26 and/or 28. Upon contact with the most downstream seating component (e.g., seating component 26 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. 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.