CN110873665A - Proppant performance testing device and proppant performance testing system - Google Patents
Proppant performance testing device and proppant performance testing system Download PDFInfo
- Publication number
- CN110873665A CN110873665A CN201810998046.5A CN201810998046A CN110873665A CN 110873665 A CN110873665 A CN 110873665A CN 201810998046 A CN201810998046 A CN 201810998046A CN 110873665 A CN110873665 A CN 110873665A
- Authority
- CN
- China
- Prior art keywords
- proppant
- performance testing
- containing tank
- piston
- hydraulic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000012360 testing method Methods 0.000 title claims abstract description 55
- 238000005485 electric heating Methods 0.000 claims abstract description 24
- 238000007789 sealing Methods 0.000 claims abstract description 13
- 238000010438 heat treatment Methods 0.000 claims description 5
- 239000007769 metal material Substances 0.000 claims description 5
- 238000000034 method Methods 0.000 abstract description 4
- 238000011056 performance test Methods 0.000 abstract description 3
- 239000003795 chemical substances by application Substances 0.000 description 13
- 239000011435 rock Substances 0.000 description 10
- 239000007789 gas Substances 0.000 description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- 239000002245 particle Substances 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 239000003345 natural gas Substances 0.000 description 2
- 239000003209 petroleum derivative Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
- G01N3/10—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces generated by pneumatic or hydraulic pressure
- G01N3/12—Pressure testing
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N5/00—Analysing materials by weighing, e.g. weighing small particles separated from a gas or liquid
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0014—Type of force applied
- G01N2203/0016—Tensile or compressive
- G01N2203/0019—Compressive
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/003—Generation of the force
- G01N2203/0042—Pneumatic or hydraulic means
- G01N2203/0048—Hydraulic means
Landscapes
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The invention discloses a proppant performance testing device and a proppant performance testing system, and belongs to the technical field of oil exploitation. The proppant performance testing apparatus comprises: proppant holding tank 1, fixed stopper 2, piston 3, electric heating jacket 4, hydraulic pressure pipe 5 and platform 6, wherein: the proppant-containing tank 1 has a cylindrical structure; the fixed plug 2 is positioned at the bottom of the proppant containing tank 1, and the side wall of the fixed plug 2 is hermetically connected with the inner wall of the proppant containing tank 1; the piston 3 is positioned at the top of the proppant containing tank 1, a sealing structure is arranged between the side wall of the piston 3 and the inner wall of the proppant containing tank 1, and the platform 6 is arranged at the top of the piston 3; a cavity for containing the proppant is formed among the proppant containing tank 1, the fixed plug 2 and the piston 3; the hydraulic pipe 5 is arranged inside the fixed plug 2; the electric heating jacket 4 is sleeved on the outer wall of the proppant containing tank 1. By adopting the method and the device, the accuracy of the performance test of the propping agent can be improved.
Description
Technical Field
The invention relates to the technical field of oil exploitation, in particular to a proppant performance testing device and a proppant performance testing system.
Background
Along with the deepening of the national oil and gas exploitation degree, the oil and gas exploitation efficiency becomes a difficult problem for constructors. The constructor needs to inject fluid into the rock stratum with the oil and gas stored therein to enable the rock stratum to generate fractures, the pressure in the rock stratum is higher than the above-ground pressure, and the oil and gas can burst out of the fractures of the rock stratum. In the process of exploitation, a constructor fills a propping agent in a fracture of a rock stratum, and the propping agent can ensure that the fracture is not closed under the stress action of the rock stratum. Proppant refers to natural sand or man-made high strength ceramic particles having a certain particle size and grading. The performance of the proppant directly influences the efficiency of oil and gas exploitation, and the most critical index in the performance of the proppant is the strength of the proppant.
At present, the method for testing the performance of the proppant mainly comprises the steps that a constructor puts a certain mass of the proppant into a proppant containing tank in a laboratory, applies unidirectional pressure to the proppant through a piston, and measures the ratio of the mass of broken particles to the original mass after the pressure application is finished.
In the process of implementing the invention, the inventor finds that the related art has at least the following problems:
the proppant is applied to the petroleum and natural gas rock stratum, the petroleum and natural gas rock stratum is complex, the pressure bearing direction and the form of the proppant are not fixed, the actual situation in the rock stratum can not be well simulated by applying unidirectional pressure to the proppant through a piston by constructors, and the performance of the tested proppant is inaccurate.
Disclosure of Invention
To address the problems of the prior art, the present disclosure provides a proppant performance testing apparatus and a proppant performance testing system. The technical scheme of the proppant performance testing device and the proppant performance testing system is as follows:
according to a first aspect of embodiments of the present disclosure, there is provided a proppant performance testing device, the proppant performance testing apparatus comprising: proppant holding tank 1, fixed stopper 2, piston 3, electric heating jacket 4, hydraulic pressure pipe 5 and platform 6, wherein:
the proppant-containing tank 1 has a cylindrical structure;
the fixed plug 2 is fixedly assembled in the proppant containing tank 1 and is positioned at the bottom of the proppant containing tank 1, and the side wall of the fixed plug 2 is in sealing connection with the inner wall of the proppant containing tank 1;
the piston 3 is assembled in the proppant containing tank 1 in a sliding manner and is positioned at the top of the proppant containing tank 1, a sealing structure is arranged between the side wall of the piston 3 and the inner wall of the proppant containing tank 1, the platform 6 is arranged at the top of the piston 3, and the platform 6 is used for bearing the pressure output by the pressure output device;
a cavity for containing the proppant is formed among the proppant containing tank 1, the fixed plug 2 and the piston 3;
the hydraulic pipe 5 is arranged inside the fixed plug 2, a first end of the hydraulic pipe 5 is communicated with the cavity, a second end of the hydraulic pipe 5 is positioned outside the fixed plug 2, and the second end is used for being connected with a hydraulic output device;
the electric heating sleeve 4 is sleeved on the outer wall of the proppant containing tank 1 and used for heating the interior of the cavity.
Alternatively, the proppant-containing tank 1, the fixed plug 2, and the piston 3 are made of a metal material.
Optionally, a handle 7 is provided on the sidewall of the proppant-containing tank 1.
Optionally, the sidewall of the fixed plug 2 is provided with at least one annular groove, and each annular groove is provided with a sealing rubber ring.
Optionally, at least one annular groove is formed in the side wall of the piston 3, and a sealing rubber ring is arranged in each annular groove.
Optionally, the proppant performance testing device further comprises a base 8, and the base 8 is fixedly connected with the bottom of the fixing plug 2.
Optionally, the base 8 is fixedly connected with the bottom of the fixing plug 2 through a bolt.
Optionally, the proppant performance testing device further comprises an insulating sleeve 9, and the insulating sleeve 9 is sleeved outside the electric heating sleeve 4.
Optionally, a filter screen is disposed at a nozzle of the first end of the hydraulic pipe 5.
According to a second aspect of embodiments of the present disclosure, there is provided a proppant performance testing system comprising a pressure output device, a hydraulic output device, and the proppant performance testing device of any one of claims 1-9, wherein:
the proppant performance testing device is placed on a placing platform of the pressure output device, and the top surface of the platform 6 is in contact with the pressure output end of the pressure output device;
the second end of the hydraulic pipe 5 is communicated with a hydraulic output pipe of the hydraulic output device.
The technical scheme provided by the embodiment of the disclosure can have the following beneficial effects:
in the embodiment of the invention, a constructor uses the proppant performance testing device, so that the direction of the pressed proppant is not fixed, and the proppant performance testing device is heated by the electric heating sleeve 4, so that the actual situation of a rock stratum is well simulated, and the accuracy of the proppant performance test can be improved.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosure.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the present disclosure and together with the description, serve to explain the principles of the disclosure. In the drawings:
fig. 1 is a schematic diagram of a proppant performance testing device provided by an embodiment of the invention.
Description of the figures
1. Proppant holds jar, 2, fixed stopper, 3, piston, 4, electric heating jacket, 5, hydraulic pressure pipe, 6, platform, 7, handle, 8, base, 9, insulation cover.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, embodiments of the present invention will be described in detail with reference to the accompanying drawings.
The embodiment of the invention provides a proppant performance testing device, as shown in fig. 1, the proppant performance testing device comprises a proppant containing tank 1, a fixed plug 2, a piston 3, an electric heating jacket 4, a hydraulic pipe 5 and a platform 6, wherein the proppant containing tank 1 has a cylindrical structure. The fixed plug 2 is fixedly assembled in the proppant containing tank 1 and is positioned at the bottom of the proppant containing tank 1, and the side wall of the fixed plug 2 is connected with the inner wall of the proppant containing tank 1 in a sealing manner. The piston 3 is assembled in the proppant containing tank 1 in a sliding mode and is located at the top of the proppant containing tank 1, a sealing structure is arranged between the side wall of the piston 3 and the inner wall of the proppant containing tank 1, the platform 6 is arranged at the top of the piston 3, and the platform 6 is used for bearing the pressure output by the pressure output device. A cavity for containing proppant is formed among the proppant containing tank 1, the fixed plug 2 and the piston 3. The hydraulic pressure pipe 5 sets up inside fixed stopper 2, and the first end and the cavity intercommunication of hydraulic pressure pipe 5, the second end of hydraulic pressure pipe 5 are located fixed stopper 2 outsidely, and the second end is used for connecting hydraulic output device. The electric heating sleeve 4 is sleeved on the outer wall of the proppant containing tank 1 and used for heating the interior of the cavity.
Wherein, annular groove is used for placing sealed rubber ring, and the number of sealed rubber ring is more, and sealed effect is better.
In practice, the piston 3 is slidably assembled in the proppant containing tank 1 at the top of the proppant containing tank 1, and the piston 3 can move axially downward in the proppant containing tank 1 and can be taken out of the proppant containing tank 1 by moving the platform 6 upward. The piston 3 can be divided into two parts, the two parts of the piston 3 can be respectively formed or integrally formed, and the two parts are both cylindrical structures. The first part of the piston 3 is arranged below the platform 6 with a radius smaller than the radius of the platform 6. The upper surface of the first part of the piston 3 is fixedly connected with the lower surface of the platform 6, and the lower surface of the first part of the piston 3 is fixedly connected with the upper surface of the second part of the piston 3. The second portion of the piston 3 has a smaller radius than the first portion of the piston 3 and the outer wall thereof is provided with at least one annular groove, in each of which a sealing rubber ring is arranged. The fixed plug 2 is fixedly assembled in the proppant containing tank 1 and is positioned at the bottom of the proppant containing tank 1. The fixing plug 2 can be divided into two parts, the two parts of the fixing plug 2 can be respectively formed or integrally formed, and the two parts are both cylindrical structures. The first portion of the fixed plug 2 has the same radius as the second portion of the piston 3, and the outer wall thereof is provided with at least one annular groove, and a sealing rubber ring is arranged in each annular groove to form a seal with the inner wall of the proppant accommodating tank 1. The second portion of the fixed plug 2 has a radius larger than the radius of the outer wall of the proppant-containing tank 1 and is located below the proppant-containing tank 1 and the fixed plug 2. The middle part of the fixed plug 2 is provided with a through hole from top to bottom. The hydraulic pressure pipe 5 passes the through-hole from top to bottom in the middle part of the fixed plug 2, the first end passes the first part of the fixed plug 2 and is communicated with the cavity containing the proppant, the pipe orifice of the first end is provided with a filter screen, and the second end is penetrated out from the outer wall of the second part of the fixed plug 2. The electric heating jacket 4 is sleeved on the outer wall of the proppant containing tank 1, and the heat insulation jacket 9 is sleeved outside the electric heating jacket 4.
Alternatively, the proppant-containing tank 1, the fixed plug 2, and the piston 3 are made of a metal material.
In practice, in order to meet the industrial requirements, the proppant containing tank 1, the fixing plug 2 and the piston 3 are generally made of the same metal material, and in this embodiment, the metal material of the proppant containing tank 1, the fixing plug 2 and the piston 3 is steel.
Optionally, a handle 7 is provided on the sidewall of the proppant-containing tank 1.
In implementation, in order to facilitate the movement, a handle 7 is disposed on a side wall of the proppant storage tank 1, and a constructor can hold the handle 7 to move the proppant storage tank 1 onto a placement platform of the pressure output device to apply pressure to the proppant storage tank 1. The operator can also hold the handle 7 to pour out the proppant from the proppant holding tank 1.
Optionally, the proppant performance testing device further comprises an insulating sleeve 9, and the insulating sleeve 9 is sleeved outside the electric heating sleeve 4.
In the implementation, the electric heating jacket 4 is used for heating the proppant containing tank 1, and the heat insulating jacket 9 is sleeved outside the electric heating jacket 4 in order to maintain the temperature of the proppant containing tank 1.
Optionally, a filter screen is disposed at a nozzle of the first end of the hydraulic pipe 5.
In practice, the constructor will disconnect the second end of the hydraulic pipe 5 from the hydraulic output after the pressure test has ended. After the pressure test is completed, a portion of the proppant may become fragmented proppant. The mesh number of the selected propping agent is 40 to 70 meshes, namely the radius is 0.212 mm to 0.425 mm, and the diameter of the through hole arranged in the middle of the fixing plug 2 from top to bottom is 1 mm. When the pressure test is carried out, the constant pressure pump applies pressure to the proppant performance testing device, and the proppant cannot leak out of the first end of the hydraulic pipe 5. After the pressure test is finished, the constructor removes the constant pressure pump, the radius of the propping agent is smaller than that of the through hole from top to bottom, and the propping agent may leak out from the first end of the hydraulic pipe 5. In order to avoid the proppant from leaking out of the first end of the hydraulic pipe 5, the constructor can arrange a plurality of layers of filter screens with extremely small radius at the pipe orifice of the first end of the hydraulic pipe 5.
The embodiment of the invention provides a proppant performance testing system which comprises a pressure output device, a hydraulic output device and a proppant performance testing device, wherein the proppant performance testing device is placed on a placing platform of the pressure output device, the top surface of the platform 6 is contacted with a pressure output end of the pressure output device, and the second end of a hydraulic pipe 5 is communicated with a hydraulic output pipe of the hydraulic output device.
The pressure output device can be selected at will according to actual requirements, such as a microcomputer-controlled press machine and the like. The hydraulic output device can be selected at will according to actual requirements, such as a constant pressure pump and the like. The proppant performance testing device also comprises a base 8, and the base 8 is connected with the bottom of the fixed plug 2 through a bolt.
In implementation, the support agent performance testing device is placed on a placing platform of the microcomputer-controlled press machine, and the position of the support agent performance testing device is right below the pressure output end of the microcomputer-controlled press machine. The base 8 of the propping agent performance testing device is contacted with a placing platform of the microcomputer control press machine, the upper surface of the platform 6 is contacted with the pressure output end of the microcomputer control press machine, and a constructor inserts a power plug of the microcomputer control press machine into a power socket to control the microcomputer control press machine to output pressure. And the proppant performance testing device is communicated with a hydraulic output pipe of the constant pressure pump through a second end of the hydraulic pipe 5. Constructors insert a power plug of the constant pressure pump into a power socket to control the output pressure of the constant pressure pump.
In actual work, the experimental flow of the proppant performance test system is as follows:
the construction personnel firstly select a certain mass of the ceramsite proppant with the size of 40-70 meshes, the ceramsite proppant with the size of 40-70 meshes is placed in a tray of a balance, the mass of the ceramsite proppant is measured by placing a weight, and the mass is recorded as the original mass. The constructor takes out the piston 3 which is assembled in the proppant containing tank 1 in a sliding way, flatly lays and places a certain mass of 40-70 meshes of ceramsite proppant into a cavity containing the proppant, and then puts back the piston 3. The constructor inserts the power plug of electric heating jacket 4 into supply socket, and the constructor can be at the control panel setting temperature of electric heating jacket 4, and the temperature of electric heating jacket 4 is 90 degrees centigrade. The constructor inserts the power plug of the microcomputer control press machine into the power socket, and the constructor can set the pressure application size and the pressure application time on the microcomputer control panel of the microcomputer control press machine, wherein the pressure application size of the microcomputer control press machine is 95 MPa, and the pressure application time is 36 hours. A constructor inserts a power plug of the constant pressure pump into a power socket, and can set the pressure application size and the pressure application time on a control panel of the constant pressure pump, wherein the pressure application size of the constant pressure pump is 30 MPa, and the pressure application time is 36 hours. The constructor then turns on the switches of the electric heating jacket 4, the microcomputer controlled press and the constant pressure pump. When the constructor turns on the switch of the electric heating jacket 4, the electric heating jacket 4 heats the proppant holding tank 1. The insulating jacket 9 maintains the temperature of the electrical heating jacket 4 to the proppant containment tank 1. When a constructor opens a switch of the microcomputer control press machine, a pressure output end of the microcomputer control press machine moves towards the right lower side, the piston 3 is pushed through the platform 6, the piston 3 pushes the cavity containing the propping agent downwards, the size of the cavity containing the propping agent is reduced, and the propping agent is subjected to pressure applied by the microcomputer control press machine. When a constructor turns on a switch of the constant pressure pump, the pressurized medium flows out of a hydraulic output pipe in the constant pressure pump and flows to a cavity for containing the propping agent through a hydraulic pipe 5.
After 36 hours, the constructor turns off the switch of the electric heating jacket 4, the microcomputer control press and the constant pressure pump. The constructor takes the piston 3 out of the proppant containing tank 1, pours out the proppant from a cavity formed among the proppant containing tank 1, the fixed plug 2 and the piston 3 and used for containing the proppant, and places the poured proppant in a ventilation place for drying. Constructors select a screen combination matched with the proppant performance testing device, put the dried proppant into the screen combination, and take out the crushed proppant screened by the screen combination. The constructor places the crushed proppant in the tray of the balance, measures the mass of the crushed proppant by placing a weight, and records the mass as the crushed mass. The ratio of the crushing mass to the original mass was recorded as the crush rate by the constructor.
The constructor can repeat the experiment by setting different qualities of the propping agent, different pressing time and different temperatures. Meanwhile, the ratio of the crushing mass to the original mass measured in each experiment is respectively recorded, and the average value of the ratio of the crushing mass to the original mass is calculated, so that the precision of the crushing rate of the proppant measured by the proppant performance testing device is improved.
Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure. This application is intended to cover any variations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.
It will be understood that the present disclosure is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure is limited only by the appended claims.
Claims (10)
1. A proppant performance testing apparatus, wherein the proppant performance testing device comprises: proppant holding tank 1, fixed stopper 2, piston 3, electric heating jacket 4, hydraulic pressure pipe 5 and platform 6, wherein:
the proppant-containing tank 1 has a cylindrical structure;
the fixed plug 2 is fixedly assembled in the proppant containing tank 1 and is positioned at the bottom of the proppant containing tank 1, and the side wall of the fixed plug 2 is in sealing connection with the inner wall of the proppant containing tank 1;
the piston 3 is assembled in the proppant containing tank 1 in a sliding manner and is positioned at the top of the proppant containing tank 1, a sealing structure is arranged between the side wall of the piston 3 and the inner wall of the proppant containing tank 1, the platform 6 is arranged at the top of the piston 3, and the platform 6 is used for bearing the pressure output by the pressure output device;
a cavity for containing the proppant is formed among the proppant containing tank 1, the fixed plug 2 and the piston 3;
the hydraulic pipe 5 is arranged inside the fixed plug 2, a first end of the hydraulic pipe 5 is communicated with the cavity, a second end of the hydraulic pipe 5 is positioned outside the fixed plug 2, and the second end is used for being connected with a hydraulic output device;
the electric heating sleeve 4 is sleeved on the outer wall of the proppant containing tank 1 and used for heating the interior of the cavity.
2. A proppant performance testing device according to claim 1, wherein the proppant-containing tank 1, the fixed plug 2 and the piston 3 are made of a metal material.
3. A proppant performance testing apparatus according to claim 1, wherein a handle 7 is provided on a side wall of the proppant-containing tank 1.
4. A proppant performance testing apparatus as set forth in claim 1 wherein the fixed plug 2 has at least one annular groove in its side wall, each annular groove having a sealing rubber ring disposed therein.
5. A proppant performance testing apparatus as set forth in claim 1 wherein at least one annular groove is provided in the sidewall of the piston 3, each annular groove having a respective one of the sealing rubber rings disposed therein.
6. The proppant performance testing device of claim 1, further comprising a base 8, wherein the base 8 is fixedly connected to the bottom of the fixed plug 2.
7. A proppant performance testing device as set forth in claim 6 wherein base 8 is fixedly attached to the bottom of stationary plug 2 by bolts.
8. The proppant performance testing device of claim 1, further comprising an insulating sleeve 9, wherein the insulating sleeve 9 is sleeved outside the electric heating sleeve 4.
9. A proppant performance testing device as set forth in claim 1 wherein said hydraulic tube 5 is provided with a filter screen at the orifice of the first end.
10. A proppant performance testing system comprising a pressure output device, a hydraulic output device, and the proppant performance testing device of any of claims 1-9, wherein:
the proppant performance testing device is placed on a placing platform of the pressure output device, and the top surface of the platform 6 is in contact with the pressure output end of the pressure output device;
the second end of the hydraulic pipe 5 is communicated with a hydraulic output pipe of the hydraulic output device.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810998046.5A CN110873665A (en) | 2018-08-29 | 2018-08-29 | Proppant performance testing device and proppant performance testing system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810998046.5A CN110873665A (en) | 2018-08-29 | 2018-08-29 | Proppant performance testing device and proppant performance testing system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN110873665A true CN110873665A (en) | 2020-03-10 |
Family
ID=69714827
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810998046.5A Pending CN110873665A (en) | 2018-08-29 | 2018-08-29 | Proppant performance testing device and proppant performance testing system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110873665A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113340760A (en) * | 2021-06-22 | 2021-09-03 | 中国石油天然气股份有限公司 | Device for measuring proppant breaking rate |
CN117232985A (en) * | 2023-11-15 | 2023-12-15 | 内蒙古医科大学附属医院(内蒙古自治区心血管研究所) | Hydrogel particle strength measuring device and measuring method |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101519961A (en) * | 2009-04-01 | 2009-09-02 | 西南石油大学 | Device and method for measuring embedding depth of proppant |
CN102183796A (en) * | 2011-03-02 | 2011-09-14 | 西南石油大学 | Testing device and method for simulating backflow of propping agent |
CN203011808U (en) * | 2012-10-31 | 2013-06-19 | 北京仁创科技集团有限公司 | Fracturing proppant acid resistance testing device |
US20130233536A1 (en) * | 2012-03-07 | 2013-09-12 | Saudi Arabian Oil Company | Portable device and method for field testing proppant |
CN104153754A (en) * | 2014-07-07 | 2014-11-19 | 西南石油大学 | Dynamic laying device for testing flow conductivity of propping agent under simulated formation condition |
-
2018
- 2018-08-29 CN CN201810998046.5A patent/CN110873665A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101519961A (en) * | 2009-04-01 | 2009-09-02 | 西南石油大学 | Device and method for measuring embedding depth of proppant |
CN102183796A (en) * | 2011-03-02 | 2011-09-14 | 西南石油大学 | Testing device and method for simulating backflow of propping agent |
US20130233536A1 (en) * | 2012-03-07 | 2013-09-12 | Saudi Arabian Oil Company | Portable device and method for field testing proppant |
CN203011808U (en) * | 2012-10-31 | 2013-06-19 | 北京仁创科技集团有限公司 | Fracturing proppant acid resistance testing device |
CN104153754A (en) * | 2014-07-07 | 2014-11-19 | 西南石油大学 | Dynamic laying device for testing flow conductivity of propping agent under simulated formation condition |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113340760A (en) * | 2021-06-22 | 2021-09-03 | 中国石油天然气股份有限公司 | Device for measuring proppant breaking rate |
CN117232985A (en) * | 2023-11-15 | 2023-12-15 | 内蒙古医科大学附属医院(内蒙古自治区心血管研究所) | Hydrogel particle strength measuring device and measuring method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106918531B (en) | Dynamic and static combined loading rock testing machine and testing method for multi-phase coupling | |
Zeng et al. | Cement sheath sealing integrity evaluation under cyclic loading using large-scale sealing evaluation equipment for complex subsurface settings | |
CN100594289C (en) | Apparatus and method for measuring proppant insert depth | |
CN104677815B (en) | True triaxial Rock parameter measurement system | |
CN108952659A (en) | Visualize supercritical carbon dioxide pressure break physical simulation experiment method | |
CN102252951B (en) | High-temperature fractured rock mass permeation test device and method | |
CN109030137A (en) | A kind of experimental provision and method of simulation frozen soil stratum cement sheath consolidation | |
CN104169523A (en) | Portable device and method for field testing proppant | |
JP2737367B2 (en) | High-temperature and high-pressure test equipment for rock samples | |
CN105403505A (en) | Cementing interface bonding strength testing device and method | |
CN110595909A (en) | True triaxial test system and method for simulating influence of different temperatures of deep rock mass | |
CN109211746B (en) | Device and experimental method for simulating oil and gas migration process under geological condition | |
CN110873665A (en) | Proppant performance testing device and proppant performance testing system | |
CN107796694A (en) | A kind of high temperature triaxial core hydraulic fracture clamper and its application method | |
CN111929170B (en) | Device and method for evaluating pressure-bearing performance of temporary plugging material for fracture acidizing | |
CN108152145A (en) | The experimental provision and method of fracture development during simulation hydrocarbon source rock high temperature pyrolysis | |
CN106770431B (en) | Triaxial test device and method capable of testing expansion coefficient of rock-soil material | |
CN106442253B (en) | Method and device for evaluating artificial crack wall compaction damage caused by proppant embedding | |
CN110954683B (en) | Cement stone integrality and anti ability evaluation device that scurries | |
CN106053244B (en) | Salt cave storage tank farm country rock self-balancing type triaxial compression test device and test method | |
CN109959595B (en) | Method and device for testing permeability in hydraulic sand fracturing process of tight reservoir | |
CN109785724B (en) | Hot-pressing simulation system and method based on bag type reaction kettle | |
KR101814019B1 (en) | Current Hydraulic Fracturing System for Applying Differential Stress | |
CN111693455A (en) | Drilling fluid mud cake generation test method | |
CN103293101B (en) | A kind of downhole annular micro-crack simulation device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200310 |
|
RJ01 | Rejection of invention patent application after publication |