a) Field of the Invention
This application is directed to a method of testing a closed hydraulic system for example a blowout preventer (BOP) assembly for leaks. Oil and Gas Exploration risk management includes the ability to control subsurface pressure which may be encountered during drilling operation. The primary mechanism utilized by operators to control downhole pressure 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 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 valves, and 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 and at specific events during the drilling operations. An additional goal of these tests are to identify reliability trends specifically related to leak rates. It is perceived that BOP assemblies with leak rates having an increasing trend are more likely to fail in a critical well control event. As will be disclosed within this disclosure, the forgoing perception is only true if the leak rate is normalized to a single value that normalizes the effects of pressure and compressibility.
b) Description of Related Arts Invention
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 a high pressure pump unit 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, utilizing electronic or mechanical chart recorders, for a specified time period. During the monitoring phase the pressure decay 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. Measuring leak rate utilizing the indirect result of pressure decay, while widely accepted, is problematic and not indicative of a specific leak rate. Such factors as the compressibility, volume of the required intensification fluid, the amount of trapped air within the BOP assembly, and the flexibility of the BOP assembly have an effect on the relationship between the pressure decay rate and the actual leak rate. An example related to trapped air: if a typical land-based BOP assembly having an approximate test volume of 15 gallons and a volumetric loss rate of approximately 25 cc/min @250 psi is tested at 250 psi with approximately 7.5 gallons of air trapped within the BOP assembly during the monitoring phase of the hydrostatic test and then subsequently tested with approximately 2.5 gallons of air trapped within the BOP assembly during the monitoring phase of the hydrostatic test, the BOP would pass the first test with approximately a 3.2 psi/min pressure decay rate but, it would fail the second test with a 7.4 psi/min pressure decay rate. Each test would have the same volumetric loss rate of 25 cc/min but the result of the tests would be significantly different. In another example related to compressibility: if a typically BOP assembly, having 5 gallons of trapped air within the BOP assembly, and rig up configuration requiring approximately 50 gallons of a typical test fluid to conduct a high pressure (5000 psi) pressure decay test is first tested with a volumetric loss rate of approximately 3 cc/min, the resultant approximate psi/min decay rate will be 6.0 psi/min and the test would fail. If the same high pressure (5000 psi) pressure decay test is applied to the same typical BOP assembly but the rig up configuration requires approximately 100 gallons of a typical test fluid to conduct a high pressure (5000 psi) pressure decay test is first tested with a volumetric loss rate of approximately 3 cc/min, the resultant approximate psi/min decay rate will be 3.0 psi/min and the test would pass. Each test would have the same volumetric loss rate but the result of the tests would be significantly different. An additional example related to compressibility: if a typically BOP assembly, having 5 gallons of trapped air within the BOP assembly, and rig up configuration requiring approximately 50 gallons of a typical test fluid to conduct a high pressure (5000 psi) pressure decay test and the test results indicated a 3 psi/min pressure decay, the volumetric loss rate will be 1.5 cc/min. If the same high pressure (5000 psi) pressure decay test is applied to the same typical BOP assembly but the rig up configuration requires approximately 100 gallons of a typical test fluid to conduct a high pressure (5000 psi) pressure decay test and the test results indicated a 3 psi/min pressure decay, the volumetric loss rate will be 3.0 cc/min. Each test would have the same pressure psi/min decay rate and pass, but the volumetric loss rate would be significantly different. As is apparent, utilizing either the decay rate or the volumetric loss rate will not provide a means of comparing tests performed on the same or different BOP assembly at different compressibility factors and/or different pressures levels.
It would be much more desirable to utilize a new and unique test method that normalizes the results of either the pressure decay rate test method or the volumetric loss rate test method to a single value which can be directly compared without regards to the variables of compressibility and/or test pressure. Thus there remains a need for a hydrostatic test method that provides normalized results depicted in a single value which can be utilized as an indicator of BOP assembly integrity and can be directly compared to historical data without regards to the variables of compressibility and/or test pressure. This would allow for meaningful reliability statistics as well as a more uniform measurement of BOP assembly integrity.
The following detailed description of the improved hydrostatic test method is intended as an exemplification of the principals of the invention and not intended to limit the invention to any specific embodiment. The improved hydrostatic test method provides for a means of resolving the nonlinear relationship between volumetric loss and test pressure utilizing either a pressure decay rate method test or a volumetric leak rate method test of a hydrostatic pressure test into a single dimensionless number that approximates the diameter of an orifice.
There are two distinctly different methods of detecting a leak within a BOP assembly. The most common method is a constant volume, variable pressure test. In this test a fixed amount of intensification fluid is added to the BOP Assembly. The initial test pressure is recorded and compared to the subsequent pressure at a corresponding subsequent time. The difference between the initial and subsequent pressure, if any, is calculated. This test is usually expressed in units of psi/min. A lesser utilized method is constant pressure, variable volume. In this test the amount of intensification fluid required to maintain the test pressure over a period of time is measured. The test is usually expressed in units of cc/min. As will be explained in more detail below, either of these tests can be utilized to resolve the nonlinear relationship between volumetric loss and test pressure into a single dimensionless number that approximates the diameter of an orifice.
For a detailed description of the preferred embodiments of the invention, reference will now be made to the accompanying drawings in which:
The Apparent Compressibility Factor ACF is calculated by the following formula.
Va/PSI=ACF
Where Va=Incremental volume change of intensifying fluid, PSI=Incremental pressure change of the intensification pressure (psi), and ACF=Apparent Compressibility Factor. The Apparent Compressibility Factor is representative of the relationship between an incremental change of intensification fluid and the resultant incremental change in pressure. It is usually expressed as cc/psi.
When the BOP or system is pressurized to the test pressure level 4, the amount of intensifying fluid added in order to maintain the test pressure is measured over time (point 4 to point 5 of
The Apparent Orifice Factor (AOF) is calculated by the following formula: O=Vi/√P.
Where O=Apparent Orifice Factor, Vi=volume loss rate, and P=test pressure. The Apparent Orifice Factor dimensionless quantity representative of the nonlinear relationship between volumetric loss and test pressure expressed as a single dimensionless number that approximates the diameter of an orifice.
Now describing the constant volume, variable pressure method. The pressure in the BOP or system 19 which may contain trapped air is raised from point 1 to point 4 as shown in
The Apparent Compressibility Factor ACF is calculated by the following formula.
Va/PSIA=ACF
Where Va=Incremental volume change of intensifying fluid, PSIA=Incremental pressure change of the intensification pressure (psia), and ACF=Apparent Compressibility Factor.
When the BOP or system is pressurized to the test pressure level 4, the amount of intensification fluid is held constant and the resultant pressure decrease or increase is measured over time (point 4 to point 5 of
With this information, the equivalent volume change can be calculated by the following formula: Vi=Pd/ACF. Where ACF=Apparent Compressibility Factor, Vi=volume loss rate, and Pd=measured equivalent decay rate in psi/minute.
With this information, the Apparent Orifice Factor (AOF) can be calculated by the following formula: O=Vi/√P. Where O=Apparent Orifice Factor, Vi=volume loss rate, and P=test pressure.
Referring to
The following are two hypothetical tests of pressure testing and normalizing the results of a blowout preventer portion according to an embodiment of the invention.
For the purpose of the first test, the test method utilized is constant pressure, variable volume and the test pressure is 3775 psi. It takes approximately 16.5 gallons of intensifying fluid from pump 11 to reach the test level pressure. This takes about 4 minutes. Beginning at a pressure slightly lower than the test pressure (point 3 in
In this test, assume that the apparent compressibility factor was determined to be 10.79 cc/psi. This part of the test could take as little as one second.
Immediately after reaching the test pressure (point 4 of
In this example, assume that the measured amount of fluid added per minute to maintain the constant test pressure is 92.2 cc/min.
Therefore the Apparent Orifice Factor (AFO) O=Vi/√P would be 92.2/√{square root over (3775)}=1.5 Also note that the calculated equivalent decay rate (Pd) for this test is 8.5 psi/min.
For the purpose of the second test, the test method utilized is constant pressure, variable volume and the test pressure is 5750 psi. It takes approximately 38.8 gallons of intensifying fluid from pump 11 to reach the test level pressure. This takes about 8 minutes. Beginning at a pressure slightly lower than the test pressure (point 3 in
In this test, assume that the apparent compressibility factor was determined to be 19.8 cc/psi. This part of the test could take as little as one second.
Immediately after reaching the test pressure (point 4 of
In this example, assume that the measured amount of fluid added per minute to maintain the constant test pressure is 113.7 cc/min.
Therefore the Apparent Orifice Factor (AFO) O=Vi/√P would be 113.7/√{square root over (5750)}=1.5. Also note that the calculated equivalent decay rate (Pd) for this test is 5.7 psi/min.
In the above examples the leak rate (Vi) and the equivalent pressure decay rate (Pd) are significantly different, however the Apparent Orifice Factor is the same and much more indicative of the physical condition of the BOP assembly. In the examples above related to the leak rate (Vi): the leak rate (Vi) indicated in the first and second tests are 92.2 and 113.7 cc/min respectively. This would indicate that the leak path within the BOP Assembly, from which the pressurized fluid is escaping, had increased in area and therefore resulting in an increased leak rate, from 92.2 cc/min to 113.7 cc/min. In an examples above related to pressure decay rate (Pd): the pressure decay rate (Pd) indicated in the first and second tests are 8.5 and 5.7 psi/min respectively. Converse to the previous example of leak rate indication, the pressure decay rate indicates a reduction in the leak path area from which the pressurized fluid is escaping, therefore resulting in a reduction of the pressure decay rate from 8.5 to 5.7 psi/min. However, if the two tests are normalized according to the embodiment of the invention it is discovered that the Apparent Orifice Factor has remained unchanged at 1.5 for each test one and test two. This indicates that the leak path area has remained unchanged and the integrity of the BOP Assembly remains unchanged. It is evident by the examples above that the Apparent Orifice Factor can be utilized to normalize and subsequently compare BOP assembly test results across various BOP assembly test pressures and BOP assembly test volumes.
The apparatus utilized to measure the volume of intensifying fluid added to increase the pressure a specified amount may be a simple totalizing flow meter, a stroke counter of a reciprocating pump, or something more precise such as a precision displacement measuring cylinder. The intensifying pump may be any suitable intensification pump including rotary and reciprocating positive displacement pumps. The pressure may be measured with a precision digital or analog pressure sensor or other suitable means that will provided the required precision and resolution. A typical computer, PDA, tablet, industrial processor, or any other device capable of performing basic logic and arithmetic functions could receive the volume and pressure information from the pressure and volume sensors to calculate the Apparent Compressibility Factor
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 and is a continuation in part of U.S. application Ser. No. 15/201,090 filed Jul. 7, 2016 which claims priority to U.S. provisional application 62/191,419 filed Jul. 12, 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 U.S. provisional application 62/159,429 filed May 11, 2015. This application is also a continuation in part of application Ser. No. 14/932,727 filed Nov. 4, 2015 which claims priority to U.S. provisional application 62/140,795 filed Mar. 31, 2015. The entire contents of the above identified provisional and non-provisional U.S. patent applications are expressly incorporated herein by reference thereto.
Number | Date | Country | |
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62191419 | Jul 2015 | US | |
62159429 | May 2015 | US | |
62140795 | Mar 2015 | US |
Number | Date | Country | |
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Parent | 15201090 | Jul 2016 | US |
Child | 15360861 | US | |
Parent | 15151323 | May 2016 | US |
Child | 15201090 | US | |
Parent | 14932727 | Nov 2015 | US |
Child | 15151323 | US |