CROSS-REFERENCE TO RELATED APPLICATION

[0001] The present document is based on and claims priority to U.S. Provisional

Application Serial No. 62/837,786, filed April 24, 2019, which is incorporated herein by reference in its entirety.

BACKGROUND

[0002] In many well applications, a well string is deployed downhole with a formation isolation valve. The isolation valve may be placed in an open position to enable movement of equipment and/or fluid through the well string. However, the isolation valve may be placed in a closed position to seal off access to formations below the valve. For example, the isolation valve may be closed after retrieval of equipment used in performance of certain testing, perforating, or completion functions. The formation isolation valve may be useful in preventing fluid loss or in controlling an under balanced condition downhole. However, existing isolation valves tend to have substantial length and complexity.

SUMMARY

[0003] In general, a system and methodology are provided for facilitating actuation of a downhole device. According to an embodiment, the downhole device may be in the form of an isolation valve member, e.g. a ball valve element, actuated between positions by a mechanical section which may comprise a shifting linkage. Actuation of the mechanical section, and thus actuation of the isolation valve member, is achieved by a trip saver section controlled according to a pressure signature which may be applied from the surface or from another suitable location. The trip saver section comprises a housing having an internal actuation piston which may be coupled with the mechanical section. The trip saver section further comprises a pilot piston and a plurality of chambers formed in a wall of the housing. The pilot piston and chambers are arranged to enable shifting of the pilot piston and thus the actuation piston in response to a predetermined series of pressure pulses or other suitable pressure signature.

[0004] However, many modifications are possible without materially departing from the teachings of this disclosure. Accordingly, such modifications are intended to be included within the scope of this disclosure as defined in the claims.

BRIEF DESCRIPTION OF THE DRAWINGS

[0005] Certain embodiments of the disclosure will hereafter be described with reference to the accompanying drawings, wherein like reference numerals denote like elements. It should be understood, however, that the accompanying figures illustrate the various implementations described herein and are not meant to limit the scope of various technologies described herein, and:

[0006] Figure l is a cross-sectional illustration of an example of a well string deployed in a borehole and combined with an isolation valve, according to an

embodiment of the disclosure;

[0007] Figure 2 is a cross-sectional illustration of an example of a trip saver section which may be used in actuating an isolation valve ball element or other downhole device according to an embodiment of the disclosure;

[0008] Figure 3 is a cross-sectional view of a portion of a trip saver housing illustrated in Figure 2, according to an embodiment of the disclosure;

[0009] Figure 4 is a cross-sectional illustration of the trip saver section with a pilot piston and cooperating indexer device positioned in a chamber of the trip saver housing, according to an embodiment of the disclosure; [0010] Figure 5 is another cross-sectional illustration of the trip saver section with a pilot piston and cooperating indexer device positioned in a chamber of the trip saver housing, according to an embodiment of the disclosure; and

[0011] Figure 6 is an enlarged cross-sectional illustration of a portion of the trip saver section which includes the pilot piston, according to an embodiment of the disclosure.

PET ATT, ED DESCRIPTION

[0012] In the following description, numerous details are set forth to provide an understanding of some embodiments of the present disclosure. However, it will be understood by those of ordinary skill in the art that the system and/or methodology may be practiced without these details and that numerous variations or modifications from the described embodiments may be possible.

[0013] The disclosure herein generally involves a system and methodology which facilitate actuation of an isolation valve or other downhole device. According to an embodiment, an isolation valve comprises an isolation valve member, e.g. a ball valve element, which may be actuated between positions. For example, the isolation valve member may be actuated between closed and open positions by a mechanical section having a shifting linkage.

[0014] Actuation of the mechanical section, and thus actuation of the isolation valve member, is achieved by a trip saver section controlled according to a pressure signature. The pressure signature may be a pressure signal applied from the surface or from another suitable location. The trip saver section comprises a housing having an internal actuation piston coupled with the mechanical section. The trip saver section further comprises a pilot piston and a plurality of chambers and flow ports formed in a wall of the housing. The pilot piston, chambers, and flow ports are arranged to enable shifting of the pilot piston and thus the actuation piston in response to a predetermined series of pressure pulses or other suitable pressure signature. For example, the trip saver section may respond to the pressure signature so as to shift an isolation valve ball valve element from a closed position to an open position or vice versa.

[0015] The construction of the trip saver section reduces the length of the isolation valve compared to traditional isolation valves. Additionally, use of the pressure signature enables the elimination of control lines. The simpler construction also reduces the number of potential leak paths and creates a more robust and dependable isolation valve structure. Various embodiments also enable use of a reverse ball design in which the ball valve element is pulled to an open position rather than pushed, thus reducing forces on internal parts.

[0016] As described in greater detail below, the trip saver section provides an actuation mechanism able to generate high opening forces in a cost-effective manner. Additionally, embodiments of the trip saver section enable the generation of force to move actuation components based on tubing pressure versus atmospheric pressure. For example, an internal atmospheric pressure chamber may be created in the isolation valve and separated from the tubing fluid with a pilot piston. The pilot piston may be installed in a corresponding chamber within a housing of the trip saver section. When it is time to actuate the isolation valve, the pilot piston is moved to allow fluid to pour into the atmospheric chamber. As the fluid pours into the atmospheric chamber, a pressure differential is created across an actuation piston. The pressure differential establishes a force which moves appropriate linkages to shift an actuatable device, e.g. a ball valve element, from one operational position to another.

[0017] Referring generally to Figure 1, an example of a well system 30 is illustrated. The well system 30 may comprise a well string 32, e.g. a well completion string, deployed in a wellbore 34 or other type of borehole. The well system 30 also may comprise an actuatable device 36 which may be selectively actuated between operational positions in response to a pressure signature. For example, a pressure signature, e.g. pressure pulses, may be supplied from the surface and down through well string 32 to initiate actuation of device 36.

[0018] In the embodiment illustrated, the actuatable device 36 may be part of an isolation valve 38 disposed along the well string 32. For example, the actuatable device 36 may be in the form of a ball valve element 40 or other type of actuatable valve element. According to the illustrated embodiment, the isolation valve 38 may comprise a ball section 42 which includes the ball valve element 40 rotatably mounted in a corresponding ball section housing 44.

[0019] The ball valve element 40 (or other actuatable device) may be shifted between operational positions via a mechanical section 46 which may comprise a mechanical linkage 48 connected to the ball valve element 40 or other actuatable device. The mechanical section 46 and mechanical linkage 48 are operatively coupled with a trip saver section 50 which is constructed to respond to the pressure signature, e.g. pressure pulse signal, to cause shifting of, for example, mechanical linkage 48 and ball valve element 40. By way of example, the trip saver section 50 may be used to shift the ball valve element 40 from a closed position to an open position via the pressure signature applied from the surface.

[0020] Referring generally to Figure 2, an embodiment of the trip saver section

50 is illustrated as having an actuation piston 52 coupled with mechanical linkage 48. According to an embodiment, the mechanical linkage 48 may be moved in a linear direction to cause rotational shifting of ball valve element 40 between operational positions. However, the mechanical linkage 48 may be structured for causing rotational shifting, linear shifting, or other suitable shifting for actuating a corresponding device 36.

[0021] The actuation piston 52 is slidably mounted within an open interior 54 of a trip saver housing 56 and includes an internal through passage 58. A series of actuation piston ports 60 may extend laterally, e.g. radially, from internal through passage 58 to the exterior of actuation piston 52. An intermediate piston 62, e.g. a thermal compensating piston, may be positioned between actuation piston 52 and the surrounding housing 56. The intermediate piston 62 is sealed with respect to both the actuation piston 52 and the housing 56 via a plurality of seals 64.

[0022] At least one additional seal 66 may be located between actuation piston 52 and the surrounding housing 56. The at least one seal 66 is located so as to create an intermediate chamber 68 longitudinally between seals 66 and seals 64 and radially between actuation piston 52 and surrounding housing 56. The intermediate piston 62 effectively moves to balance pressure between the tubing pressure experienced via actuation piston ports 60 and the pressure within intermediate chamber 68. The intermediate piston 62 effectively provides this pressure balancing prior to, for example, actuation of actuatable device 36.

[0023] With additional reference to Figure 3, the housing 56 further comprises a plurality of chambers 70, 72, 74 disposed within the wall forming housing 56. The chambers 70, 72, 74 may be formed as gun drill ports or otherwise formed according to various drilling techniques, boring techniques, or other suitable formation techniques. In the example illustrated, the chambers 70, 72, 74 are in the form of tubing pressure chamber 70, center chamber 72, and atmospheric pressure chamber 74. The center chamber 72 may have a series of sections with different diameters to accommodate pressure signature responsive components (see Figures 4-6). As explained in greater detail below, the center chamber 72 may be in the form of a pilot piston chamber for receiving a pilot piston. It should be noted the tubing pressure chamber 70, center chamber 72, and atmospheric pressure chamber 74 may be arranged in different positions and relative locations within housing 56.

[0024] As illustrated in Figure 2, the center/pilot piston chamber 72 is in fluid communication with a surrounding annulus 76 via an annulus port 78 and in fluid communication with intermediate chamber 68 via intermediate chamber port 80. As further illustrated in Figure 3, the center chamber 72 is in fluid communication with tubing pressure chamber 70 via a first tubing pressure chamber port 82 and a second tubing pressure chamber port 84. The center chamber 72 also is in fluid communication with atmospheric pressure chamber 74 via an atmospheric pressure chamber port 86.

[0025] Referring also to Figures 4-6, an embodiment is illustrated in which a pilot piston 88 is slidably located within center chamber 72. The pilot piston 88 may be sealed with respect to the surrounding wall surface defining center chamber 72 via a plurality of seals 90, 92, 94. In the illustrated example, the pilot piston 88 is connected to an indexer 96 via, for example, a rod 98.

[0026] A spring 100 may be positioned around the rod 98 (or at another suitable location) to bias the pilot piston 88 and the indexer 96 in a given direction, e.g. in a leftward direction in the illustrated embodiment. The indexer 96 also is connected to an operator piston 102 which may be acted on by tubing pressure applied through tubing pressure chamber 70 and through the first tubing pressure chamber port 82.

[0027] When a tubing pressure is applied down through well string 32 and internal through passage 58, the tubing pressure is directed into tubing pressure chamber 70 and flows through first tubing pressure chamber port 82 so as to shift operator piston 102 against the resistance of spring 100. The shifting of operator piston 102 causes a consequent incremental shift of the indexer 96. When tubing pressure is released, the spring 100 biases operator piston 102 back to its original position to cycle the indexer 96.

[0028] In some embodiments, annulus pressure also may be used in cooperation with spring 100 to bias the operator piston 102 back to its original position. By way of example, the pilot piston 88 may have a longitudinal passage 104 which allows annulus pressure to be applied through the pilot piston 88, along spring 100, through indexer 96, and against operator piston 102 in a direction which assists spring 100. In the example illustrated, a thermal compensating piston 106 also is disposed in center chamber 72 between the pilot piston 88 and annulus port 78. The thermal compensating piston 106 may be used to separate annulus well fluid from clean hydraulic fluid located on the pilot piston side of thermal compensating piston 106.

[0029] Annulus pressure acts on thermal compensating piston 106 via annulus port 78 and transfers this pressure through pilot piston 88, along rod 98, through indexer 96, and against operator piston 102. It should be noted that intermediate piston 62 may similarly separate clean hydraulic fluid within intermediate chamber 68 from well fluid located within the internal through passage 58. This well fluid may come in contact with the opposite side of intermediate piston 62 (relative to the clean hydraulic fluid) via ports 60.

[0030] The indexer 96 may be appropriately constructed/programmed to respond to a predetermined pressure signature to release rod 98 so that spring 100 can transition rod 98 and pilot piston 88 to a subsequent position. For example, the pilot piston 88 may be shifted from an initial position illustrated in Figure 6 to a subsequent flow position illustrated in Figures 4 and 5. According to an embodiment, the indexer 96 may be constructed to respond to a predetermined number of pressure cycles, e.g. pressure pulses. By way of further example, the indexer 96 may be constructed so as to release rod 98 and thus shift pilot piston 88 after ten pressure cycles (pulses) of increased pressure and released pressure (or other selected number of cycles). However, various other numbers and types of pressure cycles may be used as an applied pressure signal to establish the desired pressure signature.

[0031] In an operational example, the pressure signal, e.g. pressure pulses, may be applied down through the interior of well string 32 from the surface. The pressure signal travels into tubing pressure chamber 70 through a suitable port(s) or other fluid communication channel. The pressure signal continues to travel through tubing pressure chamber port 82 and into center chamber 72 on an opposite side of operator piston 102 relative to spring 100, thus causing shifting of piston 102 and indexer 96. The appropriate pressure signal is applied to operator piston 102 and indexer 96 until indexer 96 cycles to an actuation position allowing spring 100 to shift rod 98 and pilot piston 88. [0032] In this manner, the pilot piston 88 is shifted from the position illustrated in

Figure 6 to the subsequent position illustrated in Figures 4 and 5. As pilot piston 88 is moved to the subsequent position, the pilot piston seal 92 moves past intermediate chamber port 80 (see Figure 4). This allows the higher-pressure hydraulic fluid in intermediate chamber 68 to flow through intermediate chamber port 80 and into atmospheric pressure chamber 74, thus substantially lowering the pressure in

intermediate chamber 68.

[0033] Because of the new position of pilot piston seals 92 and 94 across intermediate chamber port 80, a finite volume of a hydraulic fluid is able to pour into the atmospheric pressure chamber 74. As a result, the higher tubing pressure acting on intermediate piston 62 via the actuation piston ports 60 causes the intermediate piston 62 to shift against abutment 108 of actuation piston 52. The pressure differential between the tubing pressure in internal through passage 58 and the atmospheric chamber pressure now present within atmospheric pressure chamber 74 and intermediate chamber 68 causes the continued shifting of intermediate piston 62 and abutting actuation piston 52.

[0034] In the illustrated example, the actuation piston 52 is stroked in a leftward direction and pulls mechanical linkage 48 which, in turn, shifts the ball valve element 40 (or other actuated device). According to this example, the mechanical linkage 48 pulls the ball valve element 40 from a closed position to an open position. It should be noted the ball valve element 40 may be arranged to shift from an open position to a closed position or to shift to desired intermediate positions. Additionally, the ball valve element 40 may be replaced by other types of actuatable devices 36 which can be actuated between desired operational positions via use of the pilot piston 88 and pressure signature as described above.

[0035] Depending on the environment and application, the isolation valve 38 may be constructed to shift the ball valve element 40 or other device in various desired directions. However, the structure of trip saver section 50 enables the reverse ball design in which the ball valve element 40 is pulled open rather than being pushed to an open position. This reduces the stress on components involved in actuating the ball valve element 40 which, in turn, reduces the cost of materials and manufacturing. Additionally, components may be reduced in size, e.g. cross-section, due to the reduction in stress, thus potentially reducing the overall size of the isolation valve.

[0036] Furthermore, the trip saver section 50 may be constructed to provide an actuation piston 52 which is pressure balanced and prevented from moving until fluid is dumped into the atmospheric pressure chamber 74. As a result, the potential for accidentally opening the ball valve element 40 is reduced or eliminated. Embodiments described herein also remove the possibility of accidentally cycling backwards when cycling the indexer 96. In general, the construction of the isolation valve 38 provides a reduced number of seals, reduced number of potential leak paths, and a capability of eliminating control lines as compared to traditional isolation valves.

[0037] Although the operational example described herein describes a rotational ball valve element, the trip saver section 50 may be used to actuate various other types of devices 36. Depending on the type of device 36, the actuation motion may be a rotational motion, a linear motion, or another actuation motion. The size and layout of the chambers 70, 72, 74 also may be adjusted according to the types of operations intended, forces applied, and environmental considerations. The mechanical section 46 also may have a variety of configurations and sizes and may utilize various types of mechanical linkages 48 for converting the motion of the trip saver section 50 to the desired actuation motion for device 36, e.g. ball valve element 40.

[0038] Furthermore, the trip saver section 50 may be used to actuate the ball valve element 40 or other device between open and closed positions or between other desired operational positions. The indexer also may be constructed to respond to various types of pressure signatures, e.g. various numbers of pressure pulses. Additionally, the pressure signature may be applied as a pressure signal from a surface location or from another suitable location. [0039] Although a few embodiments of the disclosure have been described in detail above, those of ordinary skill in the art will readily appreciate that many modifications are possible without materially departing from the teachings of this disclosure. Accordingly, such modifications are intended to be included within the scope of this disclosure as defined in the claims.