This application is directed to a method of testing a closed hydraulic system for example a blowout preventer (BOP) assembly for fluid leaks. The Oil and Gas Exploration risk management includes the ability to control subsurface pressures which may be encounted during drilling operation. The primary mechanism utilized by operators to control downhole pressures is the hydrostatic pressure as a result of the drilling fluid contained within the wellbore. The drilling fluid is engineered and formulated to a density that provides a hydrostatic pressure inside of the wellbore that is greater than the formation pressure being drilled. In the majority of drilling operations, the hydrostatic control of wellbore pressure is adequate. However, from time-to-time the operator may encounter a higher than expected formation pressure where there is not adequate hydrostatic pressure to control the wellbore pressure. During these times the operator relies on a series of mechanical controls to stabilize the wellbore and prevent a “Blow Out”. A blow out is the uncontrolled release of fluid or gas from the wellbore. This event is extremely dangerous and therefore must be avoided if at all possible. The primary mechanical control device utilized by operators to control wellbore pressure is the Blowout Preventer (BOP) assembly. The BOP assembly consists of multiple sealing and shearing devices that are hydraulically actuated to provide various means of sealing around the drill string or shearing it off entirely, completely sealing the wellbore. It is essential that the BOP assembly operate as designed during these critical operations. Therefore it is a regulatory requirement to test the functionality and the integrity of the BOP assembly before starting drilling operations, at specific time intervals and or at specific events during the drilling operations.
The BOP assembly test is a series of pressure tests at a minimum of two pressure levels, low pressure and high pressure. During the pressure test, fluid from an intensification pump is introduced into the closed BOP assembly in a volume sufficient to cause the internal pressure within the closed BOP assembly to rise to the first pressure test level. Once the first pressure test level is established the high pressure pump system is isolated from the closed BOP assembly and the pressure is monitored for a specified time period. This is commonly referred to in the industry as the validation phase. During the validation phase the pressure decay of the intensified intensification fluid is determined and compared to the pressure decay specification. A typical specification for compliance allows for a pressure decay rate of no more than 5 psi/minute or 25 psi total over the entirety of the five-minute test.
The validation phase compromises two distinctly different steps. The initial step of the validation phase immediately follows the pressurization phase of the hydrostatic test and precedes the actual pressure decay test step of the validation phase. During this first step of the validation phase the internal pressure of the blowout preventer is allowed, over a period of time, to stabilize. This is known within the industry as “waiting on a flat line” and can take as much as 2 hours in extreme cases. Thermal and mechanical changes caused by the pressurization phase of the hydrostatic test can result in large pressure changes immediately following the pressurization phase. The stabilization step is required to allow thermal and mechanical changes caused by the pressurization to subside so as to not influence the pressure decay test step of the validation phase.
The improved hydrostatic test method of the current invention utilizes a means of maintaining a constant pressure at the specified test pressure while imposing a cyclic pressure wave this is equally divergent from the held constant specified test pressure immediately subsequent to the pressurization phase. Additionally and optionally, the rate of pressurization during the portion of the pressurization phase immediately preceding the validation phase is controlled and optimized to mitigate the undesirable effects of temperature and mechanical changes. Immediately subsequent to reaching the target pressure the pressure is held constant while a cyclic pressure wave is created that is equally divergent from the held constant test pressure both positively and negatively relative at an approximately constant rate of pressure change for approximately 1 to 5 minutes by adding or subtracting intensification fluid as needed to maintain the constant test pressure with the equally divergent cyclic pressure wave. The volume change required to maintain the constant test pressure with an imposed cyclic pressure wave equally divergent from the held constant test pressure is equal to the change in volume of the intensified fluid within the pressure vessel of the hydrostatic pressure test. The volume, corrected for thermal related volume changes, over time will yield a leak rate. Additional factors and calculation can be applied to the yielded leak rate to normalize pressure and compressibility variables.
For a detailed description of the preferred embodiments of the invention, reference will now be made to the accompanying drawings in which:
Now referring to graph 10 of
Now referring to
Now referring to graph 10 of
In this embodiment, as depicted in
A variable displacement hydraulic pump 12 which is driven by a prime motive source such as an electric motor 18 drives intensifier plunger 26 via hydraulic lines 66 and 65 which are connected to the hydraulic power chamber 61 on either side of piston 69.
Variable displacement pump 12 may be of the type having a variable swash plate the position of which is controlled by a valve 14 in a manner known in the art.
Pressure sensor 40 is in fluid communication with fluid conduit 46.
Intensified intensification fluid within hydrostatic chamber 61 is displaced into or received from blowout preventer 24 via fluid conduit 46. The displacing of intensification fluid from within hydrostatic chamber 63 is effected by an extension of plunger 62 and is referred to as the displacing cycle. The receiving of intensification fluid to within hydrostatic chamber 63 is effected by a retraction of plunger 62 and is referred to as the receiving cycle.
This embodiment as depicted in
The pressure wave is generated by cyclically adding or subtracting, to the base pressure signal, a small pressure signal that causes a corresponding cyclic wave in the intensification fluid. For example: If the test pressure is 5,000 psi and the cyclic wave is 25 psi then the controller would send a signal to the pressure controller that further controls the hydraulic pressure that furthers controls the intensification pressure that was the sum of the base test pressure (5,000 psi) and the cyclic adder or subtractor (25 psi). If there is no leak then the cylinder will just cyclically extend and retract to cause the 25 psi wave. If there is a leak, the cylinder will cyclically extend and retract (to cause the 25 psi) but the retraction will be less than the extension causing the cylinder to extend as necessary to maintain the base test pressure (5,000 psi).
During the test, controller 34 as shown in
An embodiment a constant pressure test with an imposed cyclic pressure wave equally divergent from the held constant test pressure of the test method is shown in
Now referring to
A detailed view of the displacing and receiving cycles of an embodiment of a cyclic pressure wave equally divergent from the held constant test pressure of the test method is shown in
Now referring to
As just disclosed above the period between points 1 and 2 is the displacing period and is representative of the measured change of displacement volume of plunger 62 of
The slope of a line drawn between points 2 and point 5, is representative of the increase or decrease in displacement volume of plunger 62 of
For example; if the first wave of the cyclic pressure wave normalized recorded period of time between point 2 and point 5 is equal to 5 seconds and point 2 has a recorded displacement volume of 300 cc and point 5 has a recorded displacement volume of 352.65 cc, the resultant slope is (300−352.65)/5=10.53. This same calculation is performed for each of the slope segments of polyline 20 of
An additional and important calculation can be made and is with respect to the apparent compressibility of the intensification fluid. The apparent (measured) compressibility of the intensification fluid is the result of the compressive strain of the intensification fluid and the volume of intensified intensification fluid within the test vessel. A method of determining apparent compressibility is taught in U.S. application Ser. No. 15/201,090 filed Jul. 1, 2016, the entire contents of which is expressly incorporated herein by reference thereto.
For example as taught within U.S. application Ser. No. 151201,090; if the pressure difference between point 1 and point 3 is 25 psi and the displacement volume at point 1 is 100 cc and at point 3 it is 703.5 cc the resultant apparent compressibility of the intensified intensification fluid is (703.5−100) I 25=24.14. Therefor the apparent compressibility express in cubic centimeters I pound square inch is 24.14 cc/psi. Meaning that each incremental increase of 1 psi requires 24.14 cc of additional intensification fluid. This calculation is performed with each cycle between points 1 and 3 and points 4 and 6 of each wave in the cyclic wave pattern.
Utilizing the above calculations, it is subsequently possible to determine the contributing amount of each the specific volume change related to thermal changes and the volume change related to the loss of intensification fluid via an actual leak. The is possible because the thermal related changes are constant with respect to the temperature delta which is decreasing over time and the leak rate remains constant over time. This further means if the standard deviation of an array of the results of the difference between each successive slope value in the polyline array is greater than zero there is a thermal component included in the polyline array of the slope values.
For example; a typical hydrostatic test utilizing an embodiment of this invention where time line 20 of
Referencing the immediately preceding example where the comparison of the slope values depicts a continuous increasing or decreasing trend are indicative of thermal related specific gravity changes within the polyline array. In these cases, the thermal related specific gravity changes can be isolated by creating an array of results by dividing the slope of the second wave by the slope of the first wave and then dividing the slope of the third wave by the slope of the second wave and continuing with this pattern of comparison unit all 24 slope values are compared. Now calculate the standard deviation of the results array. If the standard deviation of the results array is greater than 1.0E-8 then subtract a leak rate factor of 1.0E-4 from each of the 24 slope valves of the slope polyline array. Now reevaluate the standard deviation of the results array. If the standard deviation of the results array is greater than 1.0E-8 (the residual) then via iteration continue to apply the leak rate factor to the slope values of the slope polyline array as just described. The calculated leak rate slope component of the measured slope polyline will be accurate within the requirements of the test when the standard deviation of the results array is less than 1.0E-8. The leak rate factor and the residual are exemplification and may be different from test to test.
For example, and continuing to use the examples above. A typical polyline slope array might include the following array indexes 1) 10.5298, 2) 10.4872, 3) 10.4483, 4) 10.4026, 5) 10.3607, 6) 10.3190, 7) 10.2774, 8) 10.2361, 9) 10.1950, 10) 10.1541, 11) 10.1134, 12) 10.0728, 13) 10.0325, 14) 9.9924, 15) 9.9525, 16) 9.9128, 17) 9.8733, 18) 9.8340, 19) 9.7949, 20) 9.7560, 21) 9.7173, 22) 9.6787, 23) 9.6404, 24) 9.6022. The standard deviation of a results array derived from the example slope polyline array as described above is 2.716E-05. Appling, via iteration as just described above, a leak factor to each index of the results array will yield a calculated leak rate slope of 2.007. Therefore, the leak rate is 2.007*5*12=120.42 cc/min.
A more common and generally accepted unit of measure to express leak rate is pounds square inch I minute or psi/min. As previously disclosed above the apparent compressibility factor in the herein example is 24.14 cc/psi. Therefore, the leak rate express in units of psi/min is 120.42/24.14=4.98 psi/min.
It is well known within the industry that the raw signals of pressure and displacement from pressure sensor 40 and position sensor 64 of
It is evident that applying this new and unique method and system and system can provide for substantial savings. In the above example the actual leak rate is calculated to be 4.98 psi/min which is a typically accepted level within the industry. The new and improved method and system only required 2 minutes to resolve the actual leak rate. Utilizing traditional hydrostatic testing technology would require more than 80 minutes for the temperature to become insignificant enough to allow for a passing test.
In another related application, hydrostatic testing of all or a portion of a wellbore below the BOP assembly is conducted to insure the pressure integrity of the wellbore. These tests can include the setting of one or more permanent or retrievable plug(s) to isolate a portion of the wellbore to be tested or may include the wellbore below the BOP assembly in its entirety. During these tests, very much the same as previously described, intensification fluid is intensified with the portion of the wellbore to be tested via intensification pump 26 of
Providing a means of detecting leaks immediately subsequent to the pressure phase negates the requirement for a pressure decay validation phase thereby saving substantial time and money.
Although the present invention and its advantages have been described in detail, it should be understood that various changes, substitutions and alterations may be made herein without departing from the spirit and scope of the invention as defined by the appended claims.
This application claims priority to U.S. provisional application Ser. No. 62/414,677, filed Oct. 29, 2016 and is a continuation in part of U.S. application Ser. No. 14/932,727 filed Nov. 4, 2015 which claims priority to provisional patent application 62/140,795 filed Mar. 31, 2015. This application is also a continuation in part of U.S. application Ser. No. 15/151,323 filed May 10, 2016 which claims priority to provisional application 62/159,429 filed May 11, 2015. This application is also a continuation in part of U.S. application Ser. No. 15/201,090 filed Jul. 1, 2016 which claims priority to provisional application 62/191,419 filed Jul. 12, 2015. The entire contents of the above identified provisional and non-provisional U.S. patent applications are hereby expressly incorporated herein by reference thereto.
Number | Date | Country | |
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62414677 | Oct 2016 | US | |
62140795 | Mar 2015 | US | |
62159429 | May 2015 | US | |
62191419 | Jul 2015 | US |
Number | Date | Country | |
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Parent | 14932727 | Nov 2015 | US |
Child | 15797087 | US | |
Parent | 15151323 | May 2016 | US |
Child | 14932727 | US | |
Parent | 15201090 | Jul 2016 | US |
Child | 15151323 | US |