Generally, embodiments of the invention disclosed herein are related to an artificial lifting pump system for a producer of hydrocarbons or other wellbore fluids from a subsurface well, and more particularly, a self-orienting downhole pump for producing fluids such as oil and water from a horizontal or directional well and steam assisted gravity drainage production well.
Recently, horizontal wells are preferred over vertical wells due to their larger reserve exposure and higher production rate, which together lead to better economic reward and possible higher recovery of the natural resources. In some cases, heavy oil is effectively produced through injection of a hot fluid, such as steam, to reduce viscosity of the heavy oil and to help drive the heavy oil to a nearby production well.
A proven and practical technology for in-situ operations to produce the larger reserves of heavy oil, such as Canadian bitumen from oilsands, is steam assisted gravity drainage (SAGD). Steam is injected downhole to reduce the viscosity and mobilize heavy oil for recovery at a production well. Downhole pumps, that operate at steam temperature, at large flow rates and at low bottom hole pressures, pump the heavy oil through the production well to the surface. Typical performance characteristics of a suitable SAGD pump can include: fluid lifting rates greater than 1200 m3/d, operating temperatures greater than 250° C., capability of landing at true 90 degrees horizontal sections, a high tolerance of well bore trajectory for running into hole and operation, controllable, stable and low downhole pressure for less back pressure to reservoir, less reservoir sand interruption, a high tolerance of vapor content especially when hot fluid changes phase, a long service life and reasonable installation costs.
To date, production capacity of about 1000 m3/d from a hot SAGD well has been constrained by the capacity of downhole pumps, despite higher maximum reservoir delivery capability.
Further, producing heated heavy oil or bitumen from downhole has been very challenging. The industry in general has not been satisfied with the available hot fluid downhole pumps, in particular for large rate SAGD wells.
Accordingly, attempts to meet the horizontal well and SAGD production have been mainly limited to modification of existing downhole pumps, such as electrical submersible pump (ESP), namely modified for higher temperature application. Other pumps which have been tried include metal on metal progressive cavity pumps (PCP).
Some producers are still using large sucker rod beam pumps, with the increased risks including jeopardizing the productivity and steam chamber growth in exchange for longer pump run life and lower cost when compared to the more expensive high temperature ESP. However, sucker rod pumps which use surface drive reciprocating pumps and PCP's are often challenged by mechanical stress fatigue and other mechanical issues when used in horizontal wells, particularly in changes in well direction.
Other attempts and trials include the use of gear pumps, twin screw pumps and hydraulic gas pumps which are still under development.
U.S. Pat. No. 6,973,973 to Weatherford discloses a hydraulic gas pump (HGP) which utilizes natural gas as a power gas drive for pushing liquid from a chamber landed in horizontal well. After the gas drives the accumulated fluid uphole, the chamber is cycled for fluid charging. For the HGP to function properly, the HGP must land in a particular orientation once it reaches depth. Incorrect orientation of the HGP renders the pump inoperable.
In long horizontal wells, the orientation of the pump chamber is random due to the unpredictable and unavoidable rotation and twisting of the production tubing. As a consequence, there is no assurance that the HGP will function correctly when it is landed at its desired location downhole. As far as Applicant is aware, the HGP pump has so far not been practically used for horizontal producers.
Herein, a swing chamber pump is provided for horizontal fluid producing wellbores. The pump provides high lifting rates, works at high temperatures, low intake pressures, avoids pump internal flashing, and minimizes or eliminates downhole flow pressure fluctuations.
Embodiments disclosed herein describe a swing chamber pump for use advantageously in horizontal wells. The pump alternately fills one of two chambers with fluids from the wellbore while simultaneously conveying wellbore fluids in the other of the two chambers to a bore of a production string. The fluids are typically oil and water and can include emulsions and particular matter. Each of the two chambers is fluidly connected to the wellbore for receiving wellbore fluids therefrom, and each of the two chambers is fluidly connected to the production string by a self-orienting fluid outlet. The pump further comprises a switch for switching between the two chambers. A pilot assembly can aid in controlling the switch.
In an embodiment, the switch employs a linear mechanism, and in another embodiment, the switch employs a rotary mechanism.
In a broad aspect, a swing chamber pump is provided in a wellbore for lifting wellbore fluids through a production string to surface using a power gas directed from surface. The pump has a first and second pump chamber, each pump chamber having a fluid inlet for receiving the wellbore fluids therethrough from the wellbore, a self-orienting fluid outlet for maintaining fluid communication from a lower portion of the pump chamber to the production string, and a self-orienting gas valve for maintaining fluid communication with an upper headspace portion of the pump chamber and alternately directing the power gas into the upper headspace portion and expelling the power gas therefrom.
In an embodiment, when the power gas is directed into the upper headspace portion of the first pump chamber, the wellbore fluids from the lower portion are conveyed to the production string, and in the second pump chamber the power gas is expelled therefrom while wellbore fluids are received therein. When the power gas is directed into the upper headspace portion of the second pump chamber, the stored wellbore fluids from the lower portion are conveyed into the production string, and in the first pump chamber the power gas is expelled therefrom while wellbore fluids are received therein.
In another broad aspect, a linear switch is driven by a pilot gas provided from surface. The linear switch has a linear valve having a valve core operable between a first and second position, an actuator operable between a first actuation position and a second actuation position, and a latency device between the actuator and a valve core wherein the latency device provides a period of delay or dwell between reciprocation of the valve core between the valve core's first and second positions.
In another broad aspect, a rotary switch is driven by a fluid level in the pump chamber. The rotary switch has a float, a drive assembly, and a rotary valve having an oscillating valve core, the drive assembly converting continuous up and down movement of the float into a rotary oscillation of the valve core between first and second positions. The drive assembly further has a latency device for causing a period of delay or dwell between oscillation of the valve core between the first and second positions.
In another broad aspect, a mechanical latency device for a switch core, such as that used for the swing chamber pump above, has an actuator having a first and second drive stops; an intermediate driven member having a driven interface for alternate driving engagement with the first and second drive stops, the intermediate driven member having first and second switch stops; and a switch core having a switch interface for alternate driving engagement with the first and second switch stops. A difference between the spacing of the drive stops and the switch stops provides the dwell or latency.
In an embodiment, the actuation of the actuator from a first position to a second position engages the first stop with the driven interface of the intermediate driven member, progressively loading an over-center snap device during a latency period until the first switch stop is aligned with the switch interface. This causes the snap device to over-center for unloading the snap device and driving the intermediate driven member, switch interface and switch core to the second position.
Further actuation of the actuator from the second position to the first position engages the second stop with the driven interface of the intermediate driven member, loading the snap device during a latency period until the second switch stop is aligned with the switch interface. Similarly, this causes the snap device to over-center for unloading the snap device and driving the intermediate driven member, switch interface and switch core to the first position.
Embodiments of a swing chamber pump (SCP) can be situated or positioned within a wellbore for lifting wellbore fluids through a production string to surface using a gas pushing or lift mechanism. The swing chamber pump comprises two fluidly separate pump chambers, each pump chamber passively filling with and temporarily storing wellbore fluids therein. A switch alternately directs a power gas into one of the two pump chambers for urging and conveying the stored wellbore fluids into the production string while the other fills. In an embodiment, the swing chamber pump self-orients to ensure proper functioning.
Swing Chambers
With reference to
In an embodiment, the spent power gas used to lift or pump the wellbore fluids into the production string 10 can be returned to the surface through an annulus 40 between the production string 10 and the wellbore 15. Spent power gas, expelled or exhausted from the pump 5, returns up the annulus 40 and can be recycled to the pump 5 via a return gas line 45. Wellbore gas, also called casing gas, and other liquids can be carried in the return gas line 45 and therefore a liquid remover 50 can be installed to remove any liquids from the returning power gas for providing a dry power gas, which can be recycled and reused as the power gas. Removed liquids can be pumped by a surface pump 35 into the production flow line 30.
In an embodiment, pressure in the power gas line 25 is monitored by a pressure control device 55, and additional power gas can be injected into the power gas line 25 as necessary from a gas make up line 60.
In an embodiment, a pilot gas can be used to actuate a downhole switch for directing the power gas into the swing chamber pump. The pilot gas can be delivered via a pilot gas line 65 and controlled by controller 70. The pilot gas can share a common source with power gas.
In further embodiments, although not shown, a dynamic fluid level detecting device and a downhole temperature sensor can also be installed to provide dynamic fluid level information. This system can then operate using semi-closed-loop processing including the returned spent power gas and casing gas via the annular space. By integrating the above mentioned dynamic fluid level information with a downhole temperature sensor, an operator should be able to estimate bottom hole flowing conditions to avoid flashing of the pumped wellbore fluid and determine the sub cool degree for a hot fluid producing well.
With reference to
As shown, each of the first and second chambers 75,80 is in one way, fluid communication with the wellbore 15, for passively receiving wellbore fluids and storing fluids in a lower portion 85. The lower portion 85 passively receives the wellbore fluids through a fluid inlet 90. The stored fluids are then conveyed from the lower portion 85 to the production string 10, under the pressure of the power gas G which is directed to enter into an upper headspace portion 95 of the chamber such as through a gas valve 100. Accumulation of the power gas G in the active chamber respectively causes the stored fluids in the lower portion 85 to be forced or conveyed out of the chamber.
In an embodiment, the stored wellbore fluids are conveyed to the production string 10 through a fluid outlet 105. As the power gas G enters into the active chamber, increasing pressure therein causes the temporarily stored fluids to be forced out of the active chamber. To prevent the produced fluids from flowing back into the wellbore 15, the fluid inlet 90 comprises a uni-directional check valve, such as a ball check valve.
Power gas G is alternately directed to a pump chamber and then exhausted or expelled from the respective filling and producing chambers using a switch 110. A variety of switches can be employed. Embodiments of two forms of switches are detailed herein. In one embodiment, detailed in
Switch 110 alternately directs the power gas G into either the first pump chamber 75 or the second pump chamber 80. Thus, when the switch 110 directs the power gas into the first chamber 75, the stored fluids therein are conveyed into the production string 10. Simultaneously, the second chamber 80 is permitted to passively receive wellbore fluids from the wellbore 15 as the spent power gas therein is expelled into the annular space 40 through a return gas port 115. That is, as wellbore fluids enter into one of the first or second chambers 75,80 the wellbore fluids temporarily stored in the other of the second or first chambers 80,75 are conveyed into the production string 10.
Applicant notes that during filling and expelling of spent power gas, the lower and upper headspace portions of the chambers are openly exposed to wellbore pressure. Accordingly, there may be instances where the pressure in the upper headspace portion may be substantially the same as the wellbore pressure. Thus, to ensure that the pressure within the upper headspace portion remains lower than the wellbore pressure, although not shown, a return gas port 115 can be fluidly connected to a lower pressure region in the annular space 40 such as above the dynamic fluid level 98.
In order to prevent wellbore fluids inside producing tubing 10 from flowing back into the lower portion 85 of the two chambers, the fluid outlet 105 comprises a uni-directional check valve, such as a ball check valve.
The pump 5 is connected to the production string 10 and has a pump axis substantially coaxial with a wellbore axis. Thus, as is commonly encountered during operations, the housing of the pump 5 can potentially come to rest or land in any random rotational orientation. Rotational orientation is a challenge for wellbore fluid flow management, the fluid being generally liquid which flows to low lying areas and any gas residing thereabove. Even with detailed drilling trajectory data and careful running operation, a skilled person would understand that it is very difficult to ensure a conventional pump lands in an desired orientation, particularly when it is desired that a gas valve land orientated at a top of a chamber, and with a fluid outlet valve orientated at a bottom of the chamber, especially considering how long a wellbore can be and how complicated a trajectory the pump has traversed.
Further, in a pump employing a gas-actuating principle, wellbore fluid outlet valves need to reliably be positioned to be in constant fluid communication with the wellbore fluids, particularly those stored in the lower portion of the filling chamber. If not so arranged, there can be certain operational situations where the outlet valve is not resting in the fluid and power gas is ineffective to drive stored wellbore fluid into the production string, decreasing the effectiveness of the gas-actuation mechanism.
Applicant also notes that in order to maximize the force exerted by the power gas on the wellbore fluids stored in the chamber, and to ensure effective volumetric use of the available chamber volume while avoiding power gas breakthrough, the power gas entering the chamber should be segregated from and above the stored wellbore fluids. In other words, it is advantageous to prevent the power gas from bubbling through any stored fluids in the chamber.
Accordingly, and similarly, gas valves to the chambers are arranged to be self-orienting to be in constant fluid communication with an upper headspace portion of the chamber to ensure that when introducing and releasing the chamber pressure, it is a gas phase (ie. spent power gas) being released.
Accordingly, and as shown in greater detail in
As shown, the self-orienting gas valve 100 places the gas outflow end 130 (shown in closer detail in
With reference to
As shown, the gas valve 100 comprises a gas conduit 120, such as flexible tubing, having an first gas interface 130 urged to the upper headspace portion 95 and a second gas interface 125 alternately connected to the power gas for receiving the power gas and to the wellbore for expelling the power gas. The second gas interface 125 is generally fixed to the structure of the pump 5.
As shown, the first gas interface 130 is supported on a self-orienting support 135 such as a gimbal, which constantly ensures that the first gas interface 130 rotates upwardly to a position within the upper headspace portion 95, minimizing situations where the first gas interface 130 would reside partially or otherwise submerged in the wellbore fluids stored in the lower portion 85. The self-orienting support 135 can comprise an orienting member 140 extending across a diameter of the chamber 75 and rotatable about an intermediate or central pivot 155 supported from the structure of the chamber 75 or 80. The member 140 is rotatable about the pump axis that is also coaxial with the wellbore axis. The wellbore axis is generally horizontal although it is understood that the wellbore can be somewhat tortuous. The member 140 supports a float 145 at a first conduit end and a weight 150 at an opposing end. The member 140 is freely rotatable about the pivot 155 depending on the combined influence of the float 145, tending to rotate upwardly, and weight 150, tending to rotate downwardly.
As one of the chambers 75 or 80 fills with wellbore fluids, the buoyancy of the float 145 in combination with the weight 150, due to the effects of buoyancy and gravity respectively, constantly orients and positions the first gas interface 130 of the self-orienting gas valve 100 within the upper headspace portion 95.
As shown, the first gas interface 130 is supported by the float 145 at the first conduit end of the member 140. In order to minimize the resistance to rotation by torsion imposed by the flexible tubing 120, the movable first gas interface 130 can be rotatably supported in the first conduit end such as within a torus form of float 145, in order to permit relative rotation of the first gas interface 130 and the float 145. The bushings or bearings permitting free rotation can be added between the float 145 and first gas interface 130 to reduce friction therebetween and enhance free rotation.
In an embodiment where the pump chambers 75,80 are arranged coaxially in the wellbore (See
In an embodiment, and as shown, the outflow end of the flexible tubing 160 can be affixed to a connector 180 and fluidly connected to the production string 10.
In another embodiment, the drop down valve body 175 comprises a uni-directional check valve, such as a ball check valve, for one-way fluid communication from the lower portion 85.
Linear Valve
Referring back to
With reference to
The valve core 195 reciprocates within the valve body 200 to align and/or misalign the ports 215a to 215d with the power gas line 25 or the return gas port 115. The core 195 is movably sealed within the body 200 and can move longitudinally therein. The switch body 200 can be supported from the structure of one of the chambers 75,80.
Shown in greater detail,
Although not shown in
In a similar fashion, wellbore fluids can passively enter into the lower portion 85 of the second chamber 80 as the spent power gas in the second chamber 80 is permitted to be expelled therefrom through the return gas port 115.
When the valve 190 is in its second position, wellbore fluids are permitted to enter into the lower portion 85 of the first chamber 75, while power gas is injected into the upper headspace portion 95 of the second pump chamber 80 to convey stored wellbore fluids from the second chamber 80 to the production string 10.
As shown, the position of the valve core 195 determines which of the first or second pump chambers 75,80 receives power gas to convey wellbore fluids stored therein to the production string 10 while simultaneously permitting the other of the second or first pump chambers 80,75 to dump or expel earlier utilized and spent power gas so as to receive wellbore fluids from the wellbore.
Linear Switch and Pilot Assembly
Referring back to
With reference to
The pilot assembly 185 has a two-stage operation in each direction, namely a first latency stage, without actuation, and a second actuation stage. In an embodiment, and as shown, the pilot assembly 185 comprises a double-acting linear actuator 220 which is operatively connected to the switch 110. The switch 110, acting as a latency device, comprises at least two baffles, first proximal and second distal baffles 225 and 230; and three rods, a distal core rod 210 and a proximal core rod 280; and a connecting rod 212. The baffles and core rods of the switch cooperatively act to interrupt the normal continuous linear action of the actuator 220 and instead provide the snapping between the first latency stage and the second actuation stage of the core 195 in both directions. The cooperative action of the baffles 225,230 and core rods 210,280, ensure that reciprocation of the valve core 195 occurs in sudden snap action between its first position and its second position, while increasing a period of delay.
In an embodiment, and as shown, the switch 110 can comprise an over-center device that accepts linear actuation during the latency stage and then actuates, or snaps, to an actuation stage. In this embodiment, the over-center device comprises a rigid member, such as a snap bar 240, generally extending away from the core rod 280. The snap bar 240 has a translation end 241 connected and freely movable along with the core rod 280, and an opposing pivot end 242 pivotally mounted to the chamber 75 or 80 at a first anchor point 243. A biasing member, such as a snap spring 245, also has a translation end 246 which is connected to the translation end 241 of the snap bar 240 at a driven point 249. The snap spring 245 is also mounted at a second anchor point 247 to the chamber 75 or 80. The second anchor point 247 is laterally spaced away from the first anchor point 243. As shown, both snap bar 240 and snap spring 245 are moveably engaged to the core rod 280 between the baffles 225 and 230 at the driven point 249.
Generally, in operation, the actuator 220 is operatively connected by connecting rod 212 to proximal baffle 225 of the switch 110 and thus any movement of the actuator 220 is transferred to a corresponding movement of the baffle 225. However, the movement of proximal baffle 225 is not immediately transferred to a corresponding movement of distal core rod 210.
As shown in
As shown, the proximal core rod 280 is also connected to distal cage 230. Distal cage 230 also comprises axially-spaced delimiting stops, a forward stop 230F and a return stop 230R. The distal core rod 210 is fit with a catch or plate 275 (also referred to as switch interface 275) within the cage 230 that alternately engages the spaced forward and return stops 230F, 230R. The distal core rod 210 extends between the valve or switch core 195 and cage 230.
As shown in
As illustrated, the spacing between the forward and return stops 250F and 250R is spaced sufficiently to enable the snap bar 240 to reach its over-center position at about the time the space between stops 230F and 230R is consumed by the translating movement of the distal cage 230, placing the plate 275 at about the axial location of the forward stop 230F and ready to be actuated to shift the switch core 195 from its first to second position.
Although persons skilled in the art would understand that many forms of bi-directional linear actuators would be sufficient to actuate the baffles 225 and 230, in the embodiment shown in
As shown, the pilot engine 290 operates using a pilot gas that can be injected by the surface system having a source of the pilot gas. More specifically, the pilot gas can be injected into the engine 290 through a port 300, ultimately to be directed for travel one of two directions to engage the bi-directional piston 395 for actuation thereof. A diverter 305 is used to direct the incoming pilot gas into one of the two directions of travel to actuate either side of the double acting piston 395. The diverter 305 is connected to a pilot rod 301 cooperating with the distal core rod 210 so as to detect the position of the valve core 195. The diverter 305 forms a portion of a head passageway that isolates and vents a passive portion of the double acting piston 395 and applies the pilot gas to the active drive side of the piston 395.
As shown in the embodiment of
As the skilled person would understand, cyclical switching of the pilot rod 301 results in cyclical switching of the actuator piston 395, switching of the valve core 195 between the first and second position and from the second to the first position. Note that a biasing member or leaf spring 306 retains the diverter 305 in sealing engagement with the pilot engine ports regardless of pump 5 orientation.
As shown in
As described above for
The force generated by the pilot gas acting on the first piston face 320 causes the bi-directional piston 395 to move against frictional resistance and resisting force of the snap bar and snap spring 245. Connecting rod 212 moves cage 250. The cage's forward stop 250F drives proximal core rod 280 and distal cage 230 forward.
At the same time, movement of the proximal core rod 280 causes the snap bar 240 to enter into its latency stage and translate forward. The snap spring 245 is increasingly loaded as its effective length increases, applying increasing compression upon the snap bar 240 as the snap bar 240 approaches the unstable, over-center position. Distal cage 230 remains stationary and valve core 195 remains in its first position.
With reference to
As shown in
As shown, a pilot gas return port 325 permits any spent pilot gas downstream of the bi-directional piston 395 to escape therefrom. In an embodiment, the pilot gas return port 325 can be in fluid communication with the annulus 40 in the wellbore.
With reference to
Similar to the action described in
With reference to
As shown in
During the latency stage, the movement of the proximal core rod 280 loads the snap bar 240. As the snap bar reaches its unstable position, it enters the actuation stage for moving the distal core rod 210 and actuating the valve core 195.
In an embodiment, the diverter 305 can be a pilot cap having a bell or leaf-type spring 306. The cap can be slidably moveable along the pilot assembly 290 while the leaf-type spring 306 provides biased engagement for sealing thereof.
Surface equipment using a pilot gas control device 70 (see
Further, the length of the cages 230,250, being the spacing between delimiting stops, and the core rods 210,280 can also be designed to increase or decrease the residency time between the first and second positions of the valve core, and thus provide a time delay for controlling the cycling time of the swing chamber pump.
Applicant notes that the embodiments illustrated in
However, the Applicant notes that regardless of what arrangement the first and second chambers 75,80 are in, both the first and second chambers 75,80 should be fluidly separate from one another and each have a fluid volume that is substantially the same, so that a time period for filling each chambers will be substantially the same.
Rotary Switch
A person skilled in the art would understand that several swing chamber pumps of the present disclosure can be used cooperatively with one production string 10, each pump sharing a power gas source, but each having its own switch and actuator, including their own pilot assembly. However, such an arrangement could become increasingly complicated as pilot gas lines would have to be connected to each pump.
Accordingly, in an embodiment, and with reference to
As described herein, the rotary switch 251 is actuated based on a level of fill in the swing chambers, directing power gas G first of all to empty a chamber when full and then switching to exhaust the power gas and enable influx of wellbore fluids when empty. Orientation of the apparatus is again automatic regardless of the orientation of the pump 5 on landing.
Having reference to
The combination of the float system 390 and the drive assembly 255 ensures the rotary switch 250 operates regardless of the pump orientation by converting vertical up and down float movement of the float system 390 into a rotational oscillation of the rotary valve core 295. The drive assembly 255 translates the continuous up and down movement of the float system into rotational movement.
As shown in
With receipt of wellbore fluids, the float 329 is buoyed upwardly, resulting in rising of the frame's distal end 350, a pivoting of the frame 330 at mount 335 and a lowering of the proximal end 340.
The proximal end 340 includes a generally upstanding gear rack 360 having gear teeth 365 as part of a gear system 320 for rotatably oscillating a pinion gear 367 in clockwise and counter clockwise directions, within a given operational angle as the float 329 goes up and down. The gear teeth 365 are generally in the shape of round, rod-like points for accommodating the angular change between the trajectory of the proximal end. The drive assembly 255 is also fit with spaced delimiting stops for controlling rotation of the rotary valve core 295.
A gear system 320 (including the pinion gear 367) and drive assembly 255 operatively connect the float system 390 to the valve core 295 for actuating the rotary switch between its two positions.
Referring back to
The alternating or swing between the first and second pump chamber 75, 80 is fluid level dependent and thus correlates with the rate of inflow of wellbore fluids into the chamber 75 or 80 from the wellbore. In other words, a pumping rate of the pump 5 is self-regulated as the pumping rate increases with increasing flow of the wellbore fluids into the respective chamber and decreases with a decreasing flow of the wellbore fluids.
Returning to the float system 390, the proximal end 340 of the frame 330 comprises a U-shaped frame or yoke 345 having spaced apart rails 355,355 that straddle the pinion gear 367. One of the two spaced apart rails 355 supports the generally upstanding gear rack 360 having the gear teeth 365, while the other of the two spaced apart rails 355 support a generally upstanding confining rail 362, free of any gear teeth to avoid interference with the action of the gear rack 360.
Applicant notes that the confining rail 362 engages an opposing side of the pinion gear 367 and can also function to maintain engagement of the gear rack 360 with the pinion gear 367, regardless of the orientation of the pump. As the gear rack 360 moves up and down in engagement with the pinion gear 367, the pinion gear 367 is rotated. The confining rail 362 maintains engagement of the gear rack and pinion gear 367 with the proximal end 340 of the frame 330.
Although the embodiment shown in
As set forth above for the linear switch 190, the production string 10 and attached pump 5 can rotate, making it difficult to predict the landed orientation of the pump once the pump achieves its desired depth and position. Thus, the float float system 390 (shown in
Simply, float frame 330 for the float and the gear system 320 adjust to pump orientation. An arrangement of weights and floats enable controlled rotation of the frame 330 about the mount 335 in response to pump orientation.
Having reference to
Further, the gear rack 360 is substantially free of gear teeth at about a midpoint of the rack so as to enable self-orientation without conflict with the resulting relative rotation between the pinion gear 367 and the rack 360. Associated therewith, the confining rail 362 is toothless to enable locating of the yoke 345 and rack 360 about the pinion gear 367 while avoiding the conflict between rotation of the pinion gear 367 and vertical movement up and down of the yoke 345. The confining rail 362 also protects the proximal end 340 and gear rack 360 from shifting away from the pinion gear 367 during various pump rotations during pump landing (run into hole) operation.
As shown in
Accordingly, through this arrangement, the float 329 is self-oriented and provides up and down actuating forces, during both raise and fall, through the float's buoyancy force acting through rack 360. The rack 360 transfers the vertical up and down movement to a rotational movement on pinion gear 367 therefore in the drive assembly 255.
The drive assembly 255 converts the continuous back and forth rotational oscillating motion of the pinion gear 367 into periodic and rapid actuation of the rotary valve 252.
As shown in
As shown in
For first chamber actuation, a power gas conduit 420 extending about an opposing end of the valve body 295 and rotation of the valve core 295 alternately places the first chamber port 270 in fluid communication with the power gas passage 410 and the power gas port 400. Consequently, the second chamber port 475 is in fluid communication with the vent passage 415 and return gas port 405.
For second chamber actuation, rotation of the valve core 295 alternately places the second chamber port 475 in communication with the power gas passage 410 and power gas port 400. At the same time, the first chamber port 270 is in fluid communication with the return gas port 405 through the vent passage 415.
The return gas port 405 extends through the valve body 265 for fluid communication with the annulus 40. Port 405 in a rotary switch system is connected to port 115 as shown in
As shown, the rotary switch core 295 is rotatable between first and second core positions. In its first position, the first power gas passage 410 fluidly connects the power gas conduit 420 with the power gas port 400 and thus with the first chamber port 270 for permitting power gas G to enter into the first chamber 75, while simultaneously the second vent passage 415 fluidly connects the second chamber port 475 with the return gas port 405 for permitting power gas stored in the second chamber 80 to be expelled into the annulus 40. As a result, in its first core position, wellbore fluid previously received and stored in the first chamber 75 is conveyed to the production string 10, while simultaneously wellbore fluids from the wellbore 15 are received and stored in the second chamber 80 due to the lower pressure in that chamber caused by the release of gas through port 405.
In the second position of a switch cycle, the rotary core 295 is rotated in an opposite direction to its second core position for fluidly connecting the power gas line 25 with the second chamber port 475 through power gas passage 410, and simultaneously fluidly connecting the first chamber port 270 with the return gas port 405 via the second vent passage 415. Accordingly, in the rotary core's second position, the first chamber 75 is permitted to be filled with incoming wellbore fluids, while simultaneously the previously stored wellbore fluids in the second chamber 80 are conveyed to the production string 10.
Although not detailed, Applicant notes that delimiting shoulders, profile or stops could be inserted in the rotational interface between the rotary switch core 295 and switch body 265 for delimiting rotation, and preventing the core from over rotation to ensure precise alignment of the ports and conduits of the rotary valve 252. Further, a pressure equalization bleed passage can be provided through valve body 265 to deliver a small flow of power gas to the valve core opposing the power gas port 400 for balancing the force introduced at port 400. Pressure equalization counters this offsetting force and reduces the torque necessary to rotate the valve core 295.
With reference to
As shown in
Further, the gear stops 318,319 cooperate with an eccentric snap bar 311 extending from about a periphery of a snap plate 310. The snap bar 311 forms a drive interface between the indexing plate 317 and the snap plate 310. The snap plate 310 is coaxial with the indexing plate 317 and axially spaced therefrom. As shown, the snap plate 310 is located between the indexing plate 317 and the rotary valve 252. The snap plate 310 is rotatable about the gear axis AG that is coaxial with that of the pinion gear 367, indexing plate 317 and rotary valve core 295. The rotational path of the snap bar 311 is rotationally delimited between the stops 318,319.
The valve core 295 is fit with an eccentric drive pin 314 extending towards the snap plate 310 and located at about a periphery of the rotary valve core 295. While the snap bar 311 extends towards the indexing plate 317, the snap plate 310 further comprises a valve face 380 on an opposing side facing the rotary valve 252. The valve face 380 is fit with a pair of angularly spaced core stops 312 and 313, also referred to as first and second drive stops 312 and 313, at about 45 degrees apart. The angular spacing of the core stops 312,313 is determined by the extent of rotational movement of the valve core 295. The rotational path of the gear stops 318,319 alternately engage the drive pin 314 to delimit rotation between the first and second core positions.
The indexing plate 317 and snap plate 310 are rotationally supported from the chamber or pump structure.
The snap plate 310 is rotatable between two alternating resting positions which correspond to either the first or second core positions. A biasing means, such as a snap device or spring 315 ensures that the snap plate 310 is biased in either of the two positions, and thus ensures that the valve core 295 is in either the first or second core operating position.
As shown in
As shown, as the pinion gear 367 rotates in the first direction, the indexing plate 317 is rotated and the first gear stop 318 rotates to engage the snap bar 311. The gear stop 318 and snap bar 311 then rotate together and the snap spring 315 extends, loading the snap string to cause an increase in tension therein. At about a midpoint of travel, the snap spring 315 is under the most tension and the line of action of the spring 315 crosses or moves over the axis, over-centering and inherently causing the snap plate 310 to rotate rapidly. Consequently, core stop 313, moving in concert with the snap plate 310, engages the valve core's drive pin 314 and rotates the valve core 295 to the first core position. In the reverse cycle, the indexing plate 317 is rotated in second opposite direction and the second gear stop 319 rotates to engage the snap bar 311. The gear stop 319 and snap bar 311 rotate together in the opposite direction from the previous movement and the snap spring 315 extends once again. At about a midpoint of travel, the line of action of the snap spring 315 crosses over the axis, over-centering and inherently causing the snap plate 310 to rotate rapidly. Simultaneously, the core stop 312, moving in concert with the snap plate 310, engages the drive pin 314 and rotates the valve core 295 to the second core position.
Rotation of the pinion gear 367 causes the co-rotation of the snap bar 311 and snap plate 310, rotationally sweeping and extending the snap bar end of the snap spring 315 about the fixed snap point 316. As the sweep of the snap spring approaches a crossing of the gear axis, a core stop 312,313 engages the drive pin 314 so that when the snap spring 315 over-centers the gear axis AG, a core stop 312,313 rapidly drives the drive pin 314 to actuate the valve core 295 to either its first or second position.
As shown in
Functionally similar to the latency device of the linear switch, the angular spacing of the gear stops 318,319 is greater than the angular spacing of the core stops 312,313 for introducing a period of delay or dwell between the co-rotation of the indexing plate and when the snap spring 315 over-centers to the actuate the valve core 295. Further, a conversion of about a 90 degree gear rotation to about a 45 degree valve core rotation enables effective use of the limited valve core area for ports formed therein
Based on the example and angular arrangement of gear stops 318,319 and drive stops 312,313 the indexing plate 317, energized by the float system, first rotates clockwise 45 degrees from its original baseline 0 degrees. At the 45 degrees angle, stop 318 engages and starts to direct the snap bar 311 for co-rotation until approaching the midpoint of the spring 315 which is oriented at 90 degrees in this embodiment. As gear stop 319 is mounted on indexing plate 317, when stop 318 reaches the midpoint, stop 319 will be at position of about 180 degrees. As described before, snap spring 315 at midpoint reaches its greatest tension and, when over-centered, will trigger a snap clockwise rotation of the snap plate 310. As shown in
The short drive stops 312,313, being spaced 45 degrees from each other and mounted on the opposing side of the snap disk 310 from the long snap bar 311, dwell and keep steady with no rotation during the first 45 degrees rotation of indexing disk 317.
At about the point at which the snap spring 315 is at its midpoint the short drive stop 313 starts touching the short drive bar 314 and is ready to transfer the force from the spring 315 to the valve core 295. When the snap spring 315 over-centers and actuates the snap action, the stop 313 rotates the rotary valve core 295 for 45 degrees. The specific rotation of about 45 degrees of the rotary switch is chosen to coordinate with the passages formed therein and the angular space available to align the various passages and ports as described before in
The complete cycle from the first to the second core position is set forth in
As shown in
As the power gas enters the first chamber 75, the power gas displaces the stored wellbore fluids into the production string 10. As the fluid level of the wellbore fluids in the first chamber 75 drops, the float 329 falls with the fluid level and causes the proximal end 340 of the frame 330 to correspondingly rise, rotating the gear system 320 and causing the gear stop 318 to engage the snap bar 311 of the snap plate 310 (shown in
With reference to
Referencing
With reference to
This cycle of filling one chamber while emptying the second chamber is continued for providing a constant pumping of the wellbore fluids to the surface.
The above switches incorporate a latency device. Generally, and in an alternate embodiment, a mechanical latency device for a switch core can comprise an actuator having first and second drive stops; an intermediate driven member having a driven interface for alternate driving engagement with the first and second drive stops, the intermediate driven member having first and second switch stops; and a switch core having a switch interface for alternate driving engagement with the first and second switch stops. Actuation of the actuator from a first position to a second position engages the first stop with the driven interface of the intermediate driven member, loading an over-center snap device during a latency period until the first switch stop is aligned with the switch interface. This causes the snap device to over-center for unloading the snap device and driving the intermediate driven member, switch interface and switch core to the second position. Further actuation of the actuator from the second position to the first position engages the second stop with the driven interface of the intermediate driven member, loading the snap device during a latency period until the second switch stop is aligned with the switch interface. Similarly, this causes the snap device to over-center for unloading the snap device and driving the intermediate driven member, switch interface and switch core to the first position.
Thus in a linear embodiment, the actuator is a double-acting linear actuator, further comprising three rods aligned between the actuator 290 and the switch core 195, the actuator further comprising a connecting rod 212 extending from the actuator 290, the intermediate driven member 110 further comprising a proximal core rod 280 positioned axially between the connecting rod 212 and the switch core 195, and a distal core rod 210 positioned axially between the proximal core rod 280 and the valve core, the snap device 310 engaged with the proximal core rod for translation therewith. At least two baffles 225,230 are provided for enabling a dwell in the actuation, each of which have axially-spaced delimiting stops, comprising a proximal baffle 225 comprising the first and second drive stops 250F,250R, the proximal baffle connected to the connecting rod and between the proximal core rod and the connecting rod, and a distal baffle 230 comprising the first and second switch stops 230F,230R, the distal baffle connected to the proximal rod 280 between the proximal and distal rods 280,210.
When actuating the core rod between the first and second position, during the latency stage, the connecting rod and the first drive stop of the proximal baffle engage and translate the proximal rod for loading the snap bar, the axially-spaced first and second drive stops of the distal baffle moving freely about the distal core rod without actuating the valve core. When the snap bar reaches the actuation stage, a first switch stop of the distal baffle engages the distal core rod for snap actuation of the distal core rod and valve core to the second position, shifting the axially delimiting first and second drive stops of the proximal baffle to disengage from the connecting rod and engage the distal core rod.
When actuating the core rod between the second and first position, during the latency stage, the connecting rod and the second delimiting stop of the proximal baffle engage and translate the proximal rod for loading the snap bar, the axially-spaced first and second switch stops of the distal baffle moving freely about the distal core rod without moving the valve core, and when the snap bar reaches the actuation stage, a second switch stop of the distal baffle engages the distal core rod for snap actuation of the valve core to the first position, shifting the axially delimiting first and second drive stops of the proximal baffle to disengage from the proximal core rod and engage the connecting rod.
In another embodiment, when the actuator is an oscillating rotational actuator
At
In an embodiment, the angular spacing of the first and second drive stops 318,391 is greater than the angular spacing of the first and second switch stops 313,312 for introducing dwell between the co-rotation of the indexing plate and when the snap spring over-centers to actuate the switch core. Further, the angular spacing of the first and second drive stops is about 90 degrees, and the angular spacing of the first and second switch stops is about 45 degrees.
This application claims the benefits under 35 U.S.C 119(e) of the US Provisional Application Ser. No. 61/681,321, filed Aug. 9, 2012, which is incorporated fully herein by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/CA2013/050616 | 8/9/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2014/022940 | 2/13/2014 | WO | A |
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20150198017 A1 | Jul 2015 | US |
Number | Date | Country | |
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61681321 | Aug 2012 | US |