A casing string is typically cemented within a wellbore by pumping cement slurry down, through the casing string and radially-outward from the lower end of the casing string. The cement slurry flows upward within an annulus formed between the casing string the wellbore wall, where it is then allowed to set. When the entire length of the casing string cannot be cemented within the wellbore in this manner, a procedure generally known as “multi-stage cementing” is used.
During multi-stage cementing, the cement slurry is pumped into the annulus between the casing string and the wellbore wall from at least two different locations along the length of the casing string. The first location is typically at the bottom of the casing string, commonly referred to as the first stage cementing position. The second and subsequent (if any) locations or “positions” are between the top and bottom of the casing. One or more additional locations/stages may also be employed.
What is needed is an improved multi-stage cementing tool and methods of use.
Embodiments of the disclosure may provide a downhole tool including a body having a bore axially therethrough and an opening radially therethrough, and a first sleeve positioned at least partially in the bore of the body. The first sleeve has an opening radially therethrough that is axially aligned with the opening of the body when the downhole tool is in a first configuration. An inner surface of the first sleeve defines a first seat. The tool also includes a second sleeve positioned at least partially in the first sleeve. The second sleeve is aligned with the opening of the first sleeve and prevents fluid flow therethrough when the downhole tool is in the first configuration. The second sleeve is configured to move axially and engage the first seat of the first sleeve when the downhole tool is in a second configuration, so as to resist relative rotation between the first and second sleeves.
Embodiments of the disclosure may also provide a multi-stage cementing tool including a body having an axially-extending bore therethrough and a radially-extending opening in communication with the bore, and a first sleeve positioned in the bore of the body. The first sleeve has a radially-extending opening that is axially aligned with the opening in the body when the cementing tool is in a first configuration. An inner surface of the first sleeve forms first and second seats that are axially-offset from one another. The tool also includes a second sleeve positioned at least partially in the first sleeve and defining a seat. The second sleeve is aligned with the opening in the first sleeve and prevents fluid flow therethrough when the cementing tool is in the first configuration, and the second sleeve is axially-offset from the opening in the first sleeve when the tool is in a second configuration such that a path of fluid communication exists from the bore, through the openings in the first sleeve and the body, to an exterior of the body. The tool further includes a third sleeve positioned in the first sleeve and axially-offset from the second sleeve. The third sleeve is configured to engage the second seat of the first sleeve when the cementing tool is in a third configuration. The tool also includes a guide assembly configured to maintain an impediment received in the seat of the second sleeve in substantial alignment with a central longitudinal axis through the body.
Embodiments of the disclosure further provide a method for cementing a portion of a wellbore. The method includes running a downhole tool into the wellbore in a first configuration. The downhole tool includes a body having a bore axially therethrough and an opening radially therethrough, and a first sleeve positioned at least partially in the bore of the body. The first sleeve has an opening radially therethrough that is aligned with the opening of the body when the downhole tool is in a first configuration. An inner surface of the first sleeve defines a first seat. The tool also includes a second sleeve positioned at least partially in the first sleeve. The second sleeve is axially aligned with the opening of the first sleeve and prevents fluid flow therethrough when the downhole tool is in the first configuration. The second sleeve is configured to move axially and engage the first seat of the first sleeve when the downhole tool is in a second configuration, so as to resist relative rotation between the first and second sleeves. The method also includes pumping a first fluid into the wellbore from a surface location. At least a portion of the first fluid flows through the bore in the body and out a lower end of the body.
The foregoing summary is intended merely to introduce a few of the aspects of the present disclosure, and should not be considered exhaustive, an identification of key elements, or otherwise limiting on the present disclosure.
The disclosure may best be understood by referring to the following description and accompanying drawings that are used to illustrate aspects of the present embodiments. In the drawings:
The following disclosure describes several embodiments for implementing different features, structures, or functions of the present disclosure. Embodiments of components, arrangements, and configurations are described below to simplify the present disclosure; however, these embodiments are provided merely as examples and are not intended to limit the scope of the invention. Additionally, the present disclosure may repeat reference characters (e.g., numerals) and/or letters in the various embodiments and across the Figures provided herein. This repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or configurations discussed in the Figures. Moreover, the formation of a first feature over or on a second feature in the description that follows may include embodiments in which the first and second features are formed in direct contact, and may also include embodiments in which additional features may be formed interposing the first and second features, such that the first and second features may not be in direct contact. Finally, the embodiments presented below may be combined in any combination of ways, e.g., any element from one exemplary embodiment may be used in any other exemplary embodiment, without departing from the scope of the disclosure.
Additionally, certain terms are used throughout the following description and claims to refer to particular components. As one skilled in the art will appreciate, various entities may refer to the same component by different names, and as such, the naming convention for the elements described herein is not intended to limit the scope of the invention, unless otherwise specifically defined herein. Further, the naming convention used herein is not intended to distinguish between components that differ in name but not function. Additionally, in the following discussion and in the claims, the terms “including” and “comprising” are used in an open-ended fashion, and thus should be interpreted to mean “including, but not limited to.” All numerical values in this disclosure may be exact or approximate values unless otherwise specifically stated. Accordingly, various embodiments of the disclosure may deviate from the numbers, values, and ranges disclosed herein without departing from the intended scope. In addition, unless otherwise provided herein, “or” statements are intended to be non-exclusive; for example, the statement “A or B” should be considered to mean “A, B, or both A and B.”
In general, embodiments of the present disclosure may include a downhole tool that includes a plurality of sleeves. At least one of the sleeves may provide a tapered surface, and another of the sleeves may provide a tapered seat. The tapered surface may be configured to engage the tapered seat. This engagement causes the sleeves to wedge together, thereby increasing friction forces between the sleeves during such engagement. This, in turn, causes the sleeves to resist rotation relative to one another. In addition, some embodiments may optionally include a guide assembly configured to prevent misalignment between an impediment (e.g., a plug) and a bore in the downhole tool. The prevention of such misalignment may promote the integrity of the seal between the impediment and the seat that receives the impediment.
Turning now to the specific, illustrated embodiments,
The downhole tool 100 may include a tubular body 110. As shown, the body 110 may include two or more portions (two are shown: 110-1, 110-2) that are coupled together. The first portion or “box sub” 110-1 may at least partially overlap or surround the second portion or “pin sub” 110-2, and the portions 110-1, 110-2 may be coupled together via a threaded connection 116.
The body 110 may have an axial bore 112 formed at least partially therethrough. The body 110 may include one or more openings 114 formed radially-therethrough (i.e., through a wall thereof) that provide a path of fluid communication from the bore 112 to the exterior of the body 110. The openings 114 may be circumferentially-offset from one another and/or axially-offset from one another with respect to a central longitudinal axis through the body 110.
One or more sleeves (three are shown: 120, 140, 160) may be positioned in the bore 112 of the body 110 (e.g., in the first portion 110-1 of the body 110). The first or “inner” sleeve 120 may include one or more openings 124 formed radially-therethrough. The openings 124 may be circumferentially-offset from one another and/or axially-offset from one another with respect to a central longitudinal axis 118 through the first sleeve 120 and/or the body 110. The openings 124 in the first sleeve 120 may be axially aligned with the openings 114 in the body 110 when the downhole tool 100 is in the first, run-in configuration, as shown in
One or more seals 126 may be positioned radially between the first sleeve 120 and the body 110. At least one of the seals 126 may be positioned on a first axial side of the openings 124 in the first sleeve 120, and at least one of the seals 126 may be positioned on a second axial side of the openings 124 in the first sleeve 120. The seals 126 may prevent fluid from flowing or leaking axially through the annular space between the first sleeve 120 and the body 110. The seals 126 may be made of a polymer or elastomer (e.g., rubber). For example, the seals 126 may be or include O-rings.
A radially-inwardly extending portion 127 of the first sleeve 120 may define a first seat 128. In an embodiment, the portion 127 of the first sleeve 120 providing the first seat 128 may be a separate sleeve received in and connected to the first sleeve 120. In another embodiment, the portion 127 may be integral with the remainder of the first sleeve 120. Further, the first seat 128 may be positioned proximate to a lower or “downstream” end of the first sleeve 120.
The first seat 128 may be tapered. More particularly, the radial thickness of the first sleeve 120 may increase, as proceeding in a first (e.g., downward or downstream) direction 130A (to the right in
Another portion of the inner surface of the first sleeve 120 may define a second seat 132. The second seat 132 may be positioned above or upstream from the first seat 128, such that the first and second seats 128, 132 are spaced apart along the axis 118 (i.e., axially offset). As with the first seat 128, the second seat 132 may be tapered, and the radial thickness of the first sleeve 120 may increase, as proceeding in the first direction 130A, so as to form the second seat 132. However, the second seat 132 may have a greater diameter than the first seat 128. In at least one embodiment, the surface of the second seat 132 may be oriented at an angle with respect to the central longitudinal axis 118 through the first sleeve 120 and/or the body 110. The angle may be from about 1° to about 89°, about 5° to about 20°, about 20° to about 35°, about 35° to about 50°, about 50° to about 65°, or about 65° to about 80°. In another embodiment, rather than being planar and oriented at the angle described above, the second seat 132 may be curved.
The first sleeve 120 may be coupled to the body 110 by one or more shear mechanisms 134 and/or lock ring segments 170. The shear mechanisms 134 may be or include pins, screws, bolts, or the like that are designed to break when exposed to a predetermined axial and/or rotational force. The lock ring segments 170 may be released by applying a force to the third sleeve 160 that shears the shear mechanisms 134 between the first sleeve 120 and the third sleeve 160. This forces the third sleeve 160 to move downward and allows the lock ring segments 170 to retract. The first sleeve 120 may be configured to move within the body 110 when the shear mechanisms 134 break, as discussed in greater detail below. In another embodiment, the first sleeve 120 may be held in place in the body 110 with one or more springs.
The second or “closing” sleeve 140 may be positioned at least partially (e.g., radially) within the first sleeve 120, e.g., in the bore 112. The second sleeve 140 may be axially-aligned with the openings 124 in the first sleeve 120 when the downhole tool 100 is in the run-in configuration, as shown in
One or more seals 146 may be positioned radially between the first sleeve 120 and the second sleeve 140. At least one of the seals 146 may be positioned on a first axial side of the openings 124 in the first sleeve 120, and at least one of the seals 146 may be positioned on a second axial side of the openings 124 in the first sleeve 120. The seals 146 may prevent fluid from flowing or leaking axially through the annular space between the first sleeve 120 and the second sleeve 140. The seals 146 may be made of a polymer or elastomer (e.g., rubber). For example, the seals 146 may be or include O-rings.
The second sleeve 140 may include a nose surface 142 that is tapered. The nose surface 142 may be an outer surface and/or a lower surface of the second sleeve 140. The diameter defined by the nose surface 142 of the second sleeve 140 may decrease moving in the first direction 130A, thereby forming a gap radially between the nose surface 142 and the first sleeve 120, with the gap expanding as proceeding in the first direction 130A. At the same axial location, the inner diameter of the second sleeve 140 may decrease, also as proceeding in the first direction 130A, resulting in converging inner and outer diameters at an end of the second sleeve 140. In at least one embodiment, the nose surface 142 of the second sleeve 140 may be oriented at substantially the same angle as the first seat 128 of the first sleeve 120 so that the nose surface 142 of the second sleeve 140 may be received within the first seat 128 of the first sleeve 120, as discussed in more detail below. The angle may be from about 1° to about 89°, about 5° to about 20°, about 20° to about 35°, about 35° to about 50°, about 50° to about 65°, or about 65° to about 80°. In another embodiment, rather than being planar and oriented at the angle described above, the nose surface 142 of the second sleeve 140 may be curved.
The second sleeve 140 may include a seat 144 that is tapered. The seat 144 may be an inner surface and/or an upper surface. The radial thickness of the second sleeve 140 may increase moving in the first direction 130A, so as to form the seat 144. In at least one embodiment, the seat 144 of the second sleeve 140 may be oriented at an angle with respect to the central longitudinal axis 118 through the second sleeve 140 and/or the body 110. The angle may be from about 1° to about 89°, about 5° to about 20°, about 20° to about 35°, about 35° to about 50°, about 50° to about 65°, or about 65° to about 80°. In another embodiment, rather than being planar and oriented at the angle described above, the seat 144 of the second sleeve 140 may be curved.
The third or “opening” sleeve 160 may be positioned at least partially (e.g., radially) within the first sleeve 120. The third sleeve 160 may be axially-offset from the second sleeve 140. As shown, the third sleeve 160 is above/upstream from the second sleeve 140. The third sleeve 160 may include a nose surface 162 that is tapered. The nose surface 162 may be an outer surface and/or a lower surface. The diameter defined by the nose surface 162 of the third sleeve 160 may decrease, as proceeding in the first direction 130A, resulting in a gap radially between the nose surface 162 and the first sleeve 120. At the same axial location, the inner diameter of the third sleeve 160 may decrease, resulting in converging inner and outer diameters at an end of the third sleeve 160. In at least one embodiment, the nose surface 162 of the third sleeve 160 may be oriented at substantially the same angle as the second seat 132 of the first sleeve 120 so that the nose surface 162 of the third sleeve 160 may be received within the second seat 132 of the first sleeve 120, as discussed in more detail below. The angle may be from about 1° to about 89°, about 5° to about 20°, about 20° to about 35°, about 35° to about 50°, about 50° to about 65°, or about 65° to about 80°. In another embodiment, rather than being planar and oriented at the angle described above, the nose surface 162 of the third sleeve 160 may be curved.
The third sleeve 160 may include a seat 164 that is tapered. The seat 164 may be an inner surface and/or an upper surface. The cross-sectional length (e.g., diameter) of the seat 164 of the third sleeve 160 may decrease moving in the first direction 130A. In at least one embodiment, the seat 164 of the third sleeve 160 may be oriented at an angle with respect to the central longitudinal axis 118 through the third sleeve 160 and/or the body 110. The angle may be from about 1° to about 89°, about 5° to about 20°, about 20° to about 35°, about 35° to about 50°, about 50° to about 65°, or about 65° to about 80°. In another embodiment, rather than being planar and oriented at the angle described above, the seat 164 of the third sleeve 160 may be curved.
The outer (e.g., radial) surface of the third sleeve 160 may include a recess 168. The lock ring segments 170 may be coupled to and/or configured to move with the first sleeve 120. The recess 168 in the third sleeve 160 may be axially-offset from (e.g., above or upstream from) the lock ring segments 170 when the downhole tool 100 is in the first, run-in configuration. As discussed in greater detail below, the lock ring segments 170 may become positioned at least partially in the recess 168 in the third sleeve 160 when the third sleeve 160 moves with respect to the first sleeve 120 and/or the body 110.
The third sleeve 160 may be coupled to the first sleeve 120 and/or the body 110 by one or more shear mechanisms 134. As shown, the shear mechanisms 134 may be the same as those coupling the first sleeve 120 to the body 110. In another embodiment, a different set of shear mechanisms may be used. The third sleeve 160 may be configured to move within the first sleeve 120 and/or the body 110 when the shear mechanisms 134 break, as discussed in greater detail below. In another embodiment, the third sleeve 160 may be held in place in the first sleeve 120 with one or more springs.
The first sleeve 120 may also include a lower engaging surface 166, and the pin sub 110-2 may include an upper engaging surface 169. The lower and upper engaging surfaces 166, 169 may be forced toward one another and prevented from rotation through engagement therebetween. For example, the first sleeve 120 includes one or more anti-rotation teeth (two are visible in this cross-section: 180A, 180B) extending axially in the first direction 130A from the lower engaging surface 166. The pin sub 110-2 may also include one or more anti-rotation teeth (two are visible in this cross-section: 182A, 182B) extending in a second direction 130B, opposite to the first direction 130A from the upper engaging surface 169. The teeth 180A, 180B of the first sleeve 120 may be angularly offset from the teeth 182A, 182B of the pin sub 110-2. Further, when the first sleeve 120 is moved in the first direction 130A, toward the pin sub 110-2, the teeth 180A, 180B may engage the upper engaging surface 169, and the teeth 182A, 182B may engage the lower engaging surface 166. The magnitude of the axial force and the tapered geometry of the teeth 180A, 180B and the upper engaging surface 169 may cause interference to be generated therebetween, providing a tight, rotation-preventing engagement therebetween. The teeth 182A, 182B and the lower engaging surface 166 may act similarly.
In other embodiments, at least one of the sets of teeth 180A, 180B or 182A, 182B may be omitted. Further, in some embodiments, an annular tapered surface extending from either (or both) of the first sleeve 120 and the pin sub 110-2 may be provided and may be capable of providing such interference therebetween under axial loading. In such an embodiment, one or more slots or grooves may be provided to facilitate deflection, and thus potentially the generation of hoop stress in the opposing structure, so as to increase friction and enhance rotation resistance. Moreover, it will be appreciated that any number of teeth 180A, 180B, 182A, 182B may be employed in either set.
The engagement between the nose surface 142 of the second sleeve 140 and the first seat 128 of the first sleeve 120 may create a frictional engagement that reduces or prevents relative rotation between the first and second sleeves 120, 140. In at least one embodiment, the nose surface 142 and/or the first seat 128 may have a textured surface to facilitate the frictional engagement. For example, the nose surface 142 and/or the first seat 128 may have bumps, ridges, or the like. In a particular example, one of the nose surface 142 and the first seat 128 may have male protrusions, and the other of the nose surface 142 and the first seat 128 may have female recesses configured to receive the male protrusions. In another embodiment, the nose surface 142 may form a press fit or interference fit with the first seat 128 to facilitate the frictional engagement. In yet another embodiment, one of the nose surface 142 and the first seat 128 may be made of a harder material than the other of the nose surface 142 and the first seat 128 to facilitate the frictional engagement.
The engagement between the nose surface 162 of the third sleeve 160 and the second seat 132 of the first sleeve 120 may create a frictional engagement that reduces or prevents relative rotation between the first and third sleeves 120, 160. In at least one embodiment, the nose surface 162 and/or the second seat 132 may have a textured surface to facilitate the frictional engagement. For example, the nose surface 162 and/or the second seat 132 may have bumps, ridges, or the like. In a particular example, one of the nose surface 162 and the second seat 132 may have male protrusions, and the other of the nose surface 162 and the second seat 132 may have female recesses configured to receive the male protrusions. In another embodiment, the nose surface 162 may form a press fit or interference fit with the second seat 132 to facilitate the frictional engagement. In yet another embodiment, one of the nose surface 162 and the second seat 132 may be made of a harder material than the other of the nose surface 162 and the second seat 132 to facilitate the frictional engagement.
As the third sleeve 160 moves, the lock ring segments 170 may become positioned at least partially within the recess 168 in the outer surface of the third sleeve 160. This may cause the first sleeve 120 to move in the first direction 130A until the openings 124 in the first sleeve 120 are axially-offset from the openings 114 in the body 110. As such, the first sleeve 120 may prevent fluid flow from the bore 112, through the openings 114 in the body 110, and to the exterior of the body 110. One or more lock ring segments 172 may prevent the first sleeve 120 from sliding back into its original position (e.g., in the upstream direction).
Further, in the third, closed configuration, the first sleeve 120 may have been moved in the first direction 130A, such that it is forced into engagement with the pin sub 110-2. This engagement, under an axial load, creates a friction force that resists rotation between the first sleeve 120 and the body 110 (e.g., as between teeth 180A, 180B, 182A, 182B in
The guide assembly 190 may be or include one or more protrusions 192 that extend radially-inward from the first sleeve 120 (or the body 110 or the second sleeve 140). In at least one embodiment, the guide assembly 190 may include a single protrusion 192 that extends 360° around the central longitudinal axis 118 through the body 110. An inner diameter 196 of the protrusion 192 may be equal to or slightly greater than the outer diameter of the first impediment 180 such that the guide assembly 190 may maintain the first impediment 180 in alignment in the bore 112. As shown, the guide assembly 190 may include the first seat 128 of the first sleeve 120. However, in other embodiments, the first seat 128 may be separate from the guide assembly 190.
The guide assembly 190 may limit the eccentricity of the first impediment 180 with respect to the central axis 118. For example, without the guide assembly 190, the first impediment 180 may become misaligned with respect to the central axis 118, and thus a portion of the first impediment 180 may slide away from the seat 144, and may thus fail to create a seal with the seat 144. With the addition of the guide assembly 190, in an embodiment, the first impediment 180 may engage the protrusions 192, such that the protrusions 192 limit the range of misalignment for the first impediment 180. In configurations in which the first impediment 180 is aligned with the central axis 118, the protrusions 192 may be spaced radially-apart from the first impediment 180, such that the first impediment 180 may be received through the guide assembly 190 when deployed.
In
The teeth 182A, 182B may be tapered, having an increasing radial thickness as proceeding in the first axial direction 130A. The teeth 180A, 180B may be undercut, defining a gap 900 radially between the teeth 180A, 180B and the body 110, with the gap 900 decreasing in radial dimension as proceeding in the second direction 130B. The teeth 182A, 182B may be sized and configured to fit within the gap 900 when the teeth 182A, 182B are angularly aligned with the teeth 180A, 180B.
If the teeth 180A, 180B are initially angularly offset from the teeth 182A, 182B, prior to the first sleeve 120 moving into the third, closed configuration, as shown in
A first impediment 180 may then be introduced into the wellbore from the surface location, as at 1206. The first impediment 180 may be a ball, a dart, a plug, or any other obturating member of any shape, size, or configuration. The pump may increase a pressure of a second fluid flowing into the wellbore from the surface location causing the first impediment 180 flow into the bore 112 of the downhole tool 100 and come to rest in the seat 144 of the second sleeve 140. The second fluid may be the same as the first fluid, or the second fluid may be water, a brine, a drilling fluid or “mud,” or the like. The first impediment 180 may obstruct the bore 112 (i.e., prevent fluid flow therethrough) when the first impediment 180 is in the seat 144 of the second sleeve 140. With the bore 112 obstructed, the pump may cause the pressure of the second fluid upstream from the first impediment 180 to increase until the shear mechanisms 148 coupling the second sleeve 140 in place break. Once the shear mechanisms 148 break, the downhole tool 100 may be actuated into the second, open position, as shown in
A third fluid may be introduced into the wellbore from the surface location, as at 1208. The third fluid may be the same as the first fluid or the second fluid. For example, the third fluid may be a cement slurry. The pump at a surface location may increase a pressure of the third fluid causing the third fluid to flow into the bore 112 of the downhole tool 100. As the bore 112 may be obstructed by the first impediment 180, the third fluid may flow through the openings 124 in the first sleeve 120 and the openings 114 in the body 110 to the exterior of the body 110. The third fluid may then flow into the annulus between the casing and the wellbore wall at a different location than the first fluid.
A second impediment 182 may be introduced into the wellbore from the surface location, as at 1210. The second impediment 182 may be a ball, a dart, a plug, or any other obturating member of any shape, size, or configuration. The pump may increase a pressure of a fourth fluid flowing into the wellbore from the surface location causing the second impediment 182 flow into the bore 112 of the downhole tool 100 and come to rest in the seat 164 of the third sleeve 160. The fourth fluid may be the same as the second fluid or the third fluid.
The second impediment 182 may prevent fluid from flowing therepast when the second impediment 182 is in the seat 164 of the third sleeve 160. As such, the pump may cause the pressure of the fourth fluid upstream from the second impediment 182 to increase until the shear mechanisms 134 coupling the third sleeve 160 in place break. Once the shear mechanisms 134 break, the downhole tool 100 may be actuated into the third, closed configuration, as shown in
In an embodiment, the method 1200 may optionally include rotating the first sleeve 120 relative to the body 110 during a drill-out operation, as at 1212. For example, the second impediment 182 may shift the first sleeve 120 axially toward the pin sub 110-2. However, the teeth 180A, 180B of the first sleeve 120 may be angularly offset from the teeth 182A, 182B of the pin sub 110-2, and thus the first sleeve 120 may initially be rotatable relative to the body 110 (including the pin sub 110-2). When the first sleeve 120 is rotated, the teeth 180A, 180B thereof may eventually engage or mesh with the teeth 182A, 182B, producing interference therebetween that may prevent relative rotation between the first sleeve 120 and the body 110, thereby facilitating drill-out operations. In some situations, such rotation may not occur, as the teeth 180A, 180B, 182A, 182B may initially be angularly aligned. Further, such rotation may be prevented by other anti-rotation features, such as by an annular, tapered engaging surface of the first sleeve 120 engaging a similar surface of the pin sub 110-2. A variety of other friction-generating, anti-rotation devices may also or instead be employed.
The foregoing has outlined features of several embodiments so that those skilled in the art may better understand the present disclosure. Those skilled in the art should appreciate that they may readily use the present disclosure as a basis for designing or modifying other processes and structures for carrying out the same purposes and/or achieving the same advantages of the embodiments introduced herein. Those skilled in the art should also realize that such equivalent constructions do not depart from the spirit and scope of the present disclosure, and that they may make various changes, substitutions, and alterations herein without departing from the spirit and scope of the present disclosure.
This application claims priority to U.S. Provisional Patent Application having Ser. No. 62/079,829, filed on Nov. 14, 2014. The entirety of this priority application is incorporated herein by reference.
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