CN110887727A - Structural surface locking structure and rock core structural surface locking device - Google Patents

Structural surface locking structure and rock core structural surface locking device Download PDF

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Publication number
CN110887727A
CN110887727A CN201910989884.0A CN201910989884A CN110887727A CN 110887727 A CN110887727 A CN 110887727A CN 201910989884 A CN201910989884 A CN 201910989884A CN 110887727 A CN110887727 A CN 110887727A
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CN
China
Prior art keywords
clamping
locking structure
piece
sample
structural surface
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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
Application number
CN201910989884.0A
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Chinese (zh)
Inventor
蔡国军
冯文凯
杨东升
程珂力
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Chengdu Univeristy of Technology
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Chengdu Univeristy of Technology
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Priority claimed from CN201910560183 external-priority
Application filed by Chengdu Univeristy of Technology filed Critical Chengdu Univeristy of Technology
Publication of CN110887727A publication Critical patent/CN110887727A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/02Details
    • G01N3/04Chucks
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/24Investigating strength properties of solid materials by application of mechanical stress by applying steady shearing forces
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0014Type of force applied
    • G01N2203/0025Shearing
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/02Details not specific for a particular testing method
    • G01N2203/04Chucks, fixtures, jaws, holders or anvils

Abstract

The application provides a structural plane locking structure and a rock core structural plane locking device, and belongs to the field of rock-soil test equipment. The structural surface locking structure comprises a first clamping box, a second clamping box and a locking assembly. The locking assembly comprises a first clamping piece, a second clamping piece and a positioning piece. When the sample clamp is used, the first section of sample and the second section of sample are fixedly connected through the positioning piece, then the first section of sample is fixed through the first clamping piece, and the second section of sample is fixed through the second clamping piece. And after the shear sample is fixed, the first clamping piece and the second clamping piece are respectively fixed by the first clamping box and the second clamping box so as to limit the movement of the first clamping piece and the second clamping piece. The structure surface locking structure adopts the concept different from the concrete pouring maintenance manufacturing standard test piece locking structure surface, and compared with a concrete pouring method, the structure surface locking structure can shorten the test piece manufacturing time and the shearing test period and is portable for field test.

Description

Structural surface locking structure and rock core structural surface locking device
Technical Field
The application relates to the field of rock-soil test equipment, in particular to a structural surface locking structure and a rock core structural surface locking device.
Background
In the exploration process, core sample drilling is a common exploration means, but a structural plane in a core is a shear-resistant weak plane of a rock, the shear strength of the structural plane is relatively low, and external disturbance easily causes damage along the structural plane.
At present, on-site sampling generally comprises the steps of selecting rocks at key parts of an engineering with a structural surface, entering the rocks through a adit, and cutting the rocks at the key parts to preliminarily form a sample meeting the test size requirement. In the related art of structural surface, concrete is usually used to pour rocks into a shear box to form a standard test piece, and after concrete curing is finished, a shear test is performed along the direction of the structural surface. And the concrete curing needs longer time, so that the preparation time of the shear sample is too long and the test period of the shear test is long.
Disclosure of Invention
In view of this, the embodiments of the present application provide a structural surface locking structure and a core structural surface locking device, which aim to shorten a test period of shearing a sample.
In a first aspect, the present application provides a structural surface locking structure comprising
A first clamping box having a first accommodating space; the second clamping box is provided with a second accommodating space, and a reserved seam is formed between the first clamping box and the second clamping box; and the locking assembly comprises a first clamping piece, a second clamping piece and a positioning piece, the first clamping piece is provided with a first accommodating groove, the second clamping piece is provided with a second accommodating groove, the first clamping piece is locked in the first accommodating space, the second clamping piece is locked in the second accommodating space, the positioning piece comprises a first positioning part and a second positioning part detachably connected with the first positioning part, the first positioning part and the second positioning part form a positioning groove, and the first accommodating groove, the second accommodating groove and the positioning groove are configured to accommodate the shear sample.
With reference to the first aspect, in a first possible implementation manner of the first aspect, the first clamping box includes 2 first limiting members detachably connected, and the first accommodating space is formed between the 2 first limiting members.
With reference to the first possible implementation manner of the first aspect, in a second possible implementation manner of the first aspect, the first clamping box further includes a first connecting piece and a first nut, the first limiting piece is provided with 2 rows of first mounting holes, two ends of the first connecting piece are provided with first threaded ends, and the first threaded ends are accommodated in the first mounting holes and are in threaded connection with the first nut to limit movement of the first clamping piece.
With reference to the second possible implementation manner of the first aspect, in a third possible implementation manner of the first aspect, the second clamping box includes 2 second limiting members detachably connected, the second accommodating space is formed between the 2 second limiting members, and the reserved slot is formed between the second limiting member and the first limiting member at an interval.
With reference to the third possible implementation manner of the first aspect, in a fourth possible implementation manner of the first aspect, the second clamping box further includes a second connecting member and a second nut, the second limiting member is provided with 2 rows of second mounting holes, two ends of the second connecting member are provided with second threaded ends, and the second threaded ends are accommodated in the second mounting holes and are in threaded connection with the second nut to limit movement of the second clamping member.
With reference to the first possible implementation manner of the first aspect, in a fifth possible implementation manner of the first aspect, the first clamping piece includes a first clamping portion and a first wing portion, and the first clamping portion and the first wing portion are detachably connected.
With reference to the fifth possible implementation manner of the first aspect, in a sixth possible implementation manner of the first aspect, the first clamping member further includes a first mating block, the first mating block is detachably connected to the first wing, and the first mating block is configured to abut against a surface of the shear sample.
With reference to the sixth possible implementation manner of the first aspect, in a seventh possible implementation manner of the first aspect, the first matching block and the first wing portion are provided with a first groove which is communicated with each other, and the first clamping piece further includes a first abutting portion which can be embedded into the first groove and abut against the surface of the shear sample.
With reference to the seventh possible implementation manner of the first aspect, in an eighth possible implementation manner of the first aspect, the second clamping piece includes a second clamping portion and a second wing portion, and the second clamping portion and the second wing portion are detachably connected.
With reference to the eighth possible implementation manner of the first aspect, in a ninth possible implementation manner of the first aspect, the second clamping member further includes a second mating block, the second mating block is detachably connected to the second wing portion, and the second mating block is configured to abut against a surface of the shear specimen.
With reference to the ninth possible implementation manner of the first aspect, in a tenth possible implementation manner of the first aspect, the second matching block and the second wing portion are provided with a second groove that is communicated, and the second clamping piece further includes a second abutting portion that can be embedded in the second groove and abut against the surface of the shear sample.
With reference to the tenth possible implementation manner of the first aspect, in an eleventh possible implementation manner of the first aspect, the second wing portion is disposed opposite to the first wing portion in an axial direction of the shear specimen.
With reference to the first aspect, in a twelfth possible implementation manner of the first aspect, the first clamping box and the second clamping box are provided with sliding grooves that are arranged oppositely, and the structural surface locking structure further includes a sliding portion that can slide along the sliding grooves.
In a second aspect, the present application provides a core face lock comprising
A first clamping box having a first accommodating space; the second clamping box is provided with a second accommodating space, and a reserved seam is formed between the first clamping box and the second clamping box; and the locking assembly comprises a first clamping piece, a second clamping piece and a positioning piece, the first clamping piece is provided with a first accommodating groove, the second clamping piece is provided with a second accommodating groove, the first clamping piece is locked in the first accommodating space, the second clamping piece is locked in the second accommodating space, the positioning piece comprises a first positioning part and a second positioning part detachably connected with the first positioning part, and the first positioning part and the second positioning part form a positioning groove.
The core, the core wears to establish and is fixed in first holding tank, the second holding tank and the constant head tank.
With reference to the second aspect, in a first possible implementation manner of the second aspect, the first clamping box includes 2 first limiting members detachably connected, and the first accommodating space is formed between the 2 first limiting members.
With reference to the first possible implementation manner of the second aspect, in a second possible implementation manner of the second aspect, the first clamping box further includes a first connecting piece and a first nut, the first limiting piece is provided with 2 rows of first mounting holes, two ends of the first connecting piece are provided with first threaded ends, and the first threaded ends are accommodated in the first mounting holes and are in threaded connection with the first nut to limit movement of the first clamping piece.
With reference to the second possible implementation manner of the second aspect, in a third possible implementation manner of the second aspect, the second clamping box includes 2 second limiting members detachably connected, the second accommodating space is formed between the 2 second limiting members, and the reserved slot is formed between the second limiting member and the first limiting member at an interval.
With reference to the third possible implementation manner of the second aspect, in a fourth possible implementation manner of the second aspect, the second clamping box further includes a second connecting member and a second nut, the second limiting member is provided with 2 rows of second mounting holes, two ends of the second connecting member are provided with second threaded ends, and the second threaded ends are accommodated in the second mounting holes and are in threaded connection with the second nut to limit movement of the second clamping member.
With reference to the first possible implementation manner of the second aspect, in a fifth possible implementation manner of the second aspect, the first clamping piece includes a first clamping portion and a first wing portion, and the first clamping portion and the first wing portion are detachably connected.
With reference to the fifth possible implementation manner of the second aspect, in a sixth possible implementation manner of the second aspect, the first clamping member further includes a first mating block, the first mating block is detachably connected to the first wing, and the first mating block is configured to abut against a surface of the shear specimen.
With reference to the sixth possible implementation manner of the second aspect, in a seventh possible implementation manner of the second aspect, the first matching block and the first wing portion are provided with a first groove which is communicated with each other, and the first clamping piece further includes a first abutting portion which can be embedded into the first groove and abut against the surface of the shear sample.
With reference to the seventh possible implementation manner of the second aspect, in an eighth possible implementation manner of the second aspect, the second clamping piece includes a second clamping portion and a second wing portion, and the second clamping portion and the second wing portion are detachably connected.
With reference to the eighth possible implementation manner of the second aspect, in a ninth possible implementation manner of the second aspect, the second clamping member further includes a second block, the second block is detachably connected to the second wing, and the second block is configured to abut against a surface of the shear specimen.
With reference to the ninth possible implementation manner of the second aspect, in a tenth possible implementation manner of the second aspect, the second matching block and the second wing portion are provided with a second groove that is communicated, and the second clamping piece further includes a second abutting portion that can be embedded in the second groove and abut against the surface of the shear sample.
With reference to the tenth possible implementation manner of the second aspect, in an eleventh possible implementation manner of the second aspect, the second wing portion is disposed opposite to the first wing portion in an axial direction of the shear specimen.
With reference to the second aspect, in a twelfth possible implementation manner of the second aspect, the first clamping box and the second clamping box are provided with sliding grooves which are arranged oppositely, and the core structural surface locking device further includes a sliding portion which can slide along the sliding grooves.
The beneficial effects of the application are as follows: the structural surface locking structure comprises a first clamping box, a second clamping box and a locking assembly. The locking assembly comprises a first clamping piece, a second clamping piece and a positioning piece. When the sample clamp is used, the first section of sample and the second section of sample are fixedly connected through the positioning piece, then the first section of sample is fixed through the first clamping piece, and the second section of sample is fixed through the second clamping piece. And after the shear sample is fixed, the first clamping piece and the second clamping piece are respectively fixed by the first clamping box and the second clamping box so as to limit the movement of the first clamping piece and the second clamping piece. The structure surface locking structure adopts a concept different from the concrete pouring maintenance standard test piece manufacturing, and can shorten the test piece manufacturing time and the shear test period compared with a concrete pouring method.
Drawings
In order to more clearly explain the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and that for those skilled in the art, other related drawings can be obtained from these drawings without inventive effort.
Fig. 1 is a schematic internal structural diagram of a structural surface locking structure provided in an embodiment of the present application;
FIG. 2 is a schematic structural diagram of a structural surface locking structure provided in an embodiment of the present application;
FIG. 3 is a schematic structural view of the first cartridge of FIG. 2;
FIG. 4 is a schematic structural view of the second cassette of FIG. 2;
FIG. 5 is a schematic structural diagram of a locking assembly provided by an embodiment of the present application;
FIG. 6 is a schematic structural diagram of a locking assembly provided by an embodiment of the present application;
FIG. 7 is a schematic illustration of structural plane shear specimens of different tilt angles provided by an embodiment of the present application.
Icon: 100-structural surface locking structure; 110-a first clamping box; 111-a first accommodation space; 113-a first stop; 1131 — a first mounting hole; 115-a first connector; 117-first nut; 130-a second clamping box; 131-a second accommodation space; 133-a second stop; 1331-a second mounting hole; 135-a second connector; 137-a second nut; 150-a locking assembly; 151-first clamp; 1511-first clamp; 1513-a first wing; 1515-first piece; 1517-first abutting part; 153-a second clamp; 1531 — a second clamping portion; 1533-a second wing; 1535 — second mating block; 1537 — a second holding part; 155-positioning element; 1551-first positioning part; 1553-a second positioning part; 200-core.
Detailed Description
To make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions of the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application.
Thus, the following detailed description of the embodiments of the present application, as presented in the figures, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
In the description of the present application, it is to be understood that the terms "center," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the present application and for simplicity in description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed in a particular orientation, and be operated in a particular manner, and thus should not be considered limiting.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present application, "a plurality" means two or more unless specifically limited otherwise.
In this application, unless expressly stated or limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can include, for example, fixed connections, removable connections, or integral parts; the two components can be directly connected or indirectly connected through an intermediate medium, and can be communicated with each other inside the two components or in an interaction relationship of the two components; either electrical or electrical. The specific meaning of the above terms in the present application can be understood by those of ordinary skill in the art as appropriate.
In this application, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact of the first and second features, or may comprise contact of the first and second features not directly but through another feature in between. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
In the related art, a rock sample is usually poured into a shear box by using concrete to form a standard test piece, and after concrete curing is finished, a shear test is performed along the direction of a structural plane. The concrete requires a long time (at least 1-2 days) for curing, which results in a long shear test period.
In addition, concrete casting also has the following disadvantages:
1. tricalcium silicate in cement reacts with water in the pouring process, namely hydration reaction of concrete in the pouring process, so that the temperature is raised, and in addition, the concrete needs to be prepared according to a certain water cement ratio. The changes of temperature and moisture content both have adverse effects on the shear parameters of the measured structural surface, so that the measurement result has poor precision and low reliability.
2. In the concrete pouring process, the structural surface is in a completely exposed state, the structural surface is easily stained with concrete in operation, and once the structural surface is stained with the concrete, the sample needs to be replaced again, so that the operation is complicated, and the manufacturing power of the test piece is low.
Therefore, the application provides a structural surface locking structure for performing a rock structural surface shear test, and aims to solve one or more of the technical problems.
The structural surface locking structure is used for fixing a shear sample, wherein the shear sample can be a standard size sample, for example, a core is drilled through drilling, and the obtained core is used as the shear sample. The shear sample may also be of other dimensions, for example by cutting a rock to form a shear sample. The shear specimen is selected or prepared so as to minimize disturbance of the structural plane. The following description is made with reference to the accompanying drawings.
Fig. 1 shows an internal structural diagram of the structural surface locking structure, and fig. 2 shows a structural diagram of the structural surface locking structure. Referring to fig. 1 and 2, the structural surface locking structure 100 includes a first clamping box 110, a second clamping box 130, and a locking assembly 150.
Fig. 3 shows a schematic structural view of the first grip cassette. Referring to fig. 3, the first clamping box 110 has a first accommodating space 111.
In some embodiments, the first clamping box 110 includes 2 first limiting members 113 detachably connected to each other, and the first accommodating space 111 is formed between the 2 first limiting members 113. In a specific arrangement, the first limiting member 113 may be a rectangular steel plate, and 2 rectangular steel plates are oppositely arranged to form the first accommodating space 111.
The 2 rectangular steel plates are detachably connected. For example, the first clamping box 110 further includes a first connecting member 115 and a first nut 117, the first limiting member 113 defines 2 rows of first mounting holes 1131, two ends of the first connecting member 115 are provided with first threaded ends, and the first threaded ends are accommodated in the first mounting holes 1131 and are in threaded connection with the first nut 117. In this embodiment, 2 first limiting members 113 are connected together by the first connecting member 115 and the first nut 117. In other embodiments, one end of the first connecting element 115 may also be fixedly connected (e.g., welded) to one of the first limiting elements 113, and the other end of the first connecting element 115 is screwed to the first nut 117 to connect the first connecting element 115 to the other first limiting element 113.
In other specific implementations, there are 6 first mounting holes 1131 in each row, and when clamping the locking assembly 150, the 2 first limiting members 113 can be connected by selecting the appropriate first mounting holes 1131 according to the length and the inclination angle of the shear specimen, wherein the inclination angle is related to the inclination angle of the structural surface. For example, when the length of the shear specimen is long, two rows of the first mounting holes 1131 near the outer side may be selected, and when the length of the shear specimen is short, two rows of the first mounting holes 1131 near the inner side may be selected, although the specific mounting position of the shear specimen may be determined by combining the inclination angle of the structural plane.
Fig. 4 shows a schematic structural view of the second grip cassette. Referring to fig. 4, the second clamping box 130 has a second accommodating space 131.
In some specific embodiments, the second clamping box 130 includes 2 second limiting members 133 detachably connected, and the second accommodating space 131 is formed between the 2 second limiting members 133. For example, the second limiting member 133 is a rectangular steel plate, and 2 rectangular steel plates are oppositely disposed to form the second accommodating space 131.
The 2 rectangular steel plates are detachably connected. For example, the second clamping box 130 further includes a second connecting member 135 and a second nut 137, the second limiting member 133 defines 2 rows of second mounting holes 1331, two ends of the second connecting member 135 are provided with second threaded ends, and the second threaded ends are received in the second mounting holes 1331 and are in threaded connection with the second nut 137. In this embodiment, 2 second limiting members 133 are connected together by the second connecting member 135 and the second nut 137. In other embodiments, one end of the second connecting member 135 may also be fixedly connected (e.g., welded) to one of the second limiting members 133, and the other end of the second connecting member 135 is threadedly connected to the second nut 137 to connect the second connecting member 135 with the other second limiting member 133.
In other specific implementations, there are 6 second mounting holes 1331 in each row, and when the locking assembly 150 is clamped, the 2 second limiting members 133 can be connected by selecting the appropriate second mounting holes 1331 according to the length and the inclination angle of the shear specimen. The structure and the technical effects of the second clamping box 130 and the first clamping box 110 are substantially the same, and are not described herein.
Here, it should be noted that the first clamping box 110 and the second clamping box 130 are arranged at an interval from top to bottom, that is, a gap is formed between the first clamping box 110 and the second clamping box 130, so as to form a reserved slot.
In the present application, the first and second grip cartridges 110 and 130 function to grip and restrict the sliding of the locking assembly 150, that is, the locking assembly 150 is restricted from sliding by the frictional force between the first and second grip cartridges 110 and 130 and the locking assembly 150.
Fig. 5 shows a schematic view of a locking assembly. Referring to fig. 5, the locking assembly 150 includes a first clamping member 151, a second clamping member 153, and a positioning member 155.
Wherein the first clamping member 151 has a first receiving groove, the second clamping member 153 has a second receiving groove, the first clamping member 151 is locked in the first receiving space 111, and the second clamping member 153 is locked in the second receiving space 131. As mentioned above, the 2 first limiting members 113 detachably connected limit the first clamping member 151 in the first accommodating space 111, and the first limiting members 113 and the first clamping member 151 do not have relative displacement. The detachably connected 2 second limiting members 133 limit the second clamping member 153 in the second accommodating space 131, and the second limiting members 133 and the second clamping member 153 do not have relative displacement.
In particular arrangements, the first clamping member 151 includes a first clamping portion 1511 and a first wing portion 1513, the first clamping portion 1511 and the first wing portion 1513 being removably coupled. For example, the first wing portion 1513 and the first clamping portion 1511 are connected by a screw, and the first wing portion 1513 and the first clamping portion 1511 may be connected by a snap. When the first clamping portion 1511 and the first wing portion 1513 are in a connected state, the first clamping portion 1511 and the first wing portion 1513 are formed with a first receiving groove.
In this application, the second clamping member 153 includes a second clamping portion 1531 and a second wing portion 1533, and the second clamping portion 1531 and the second wing portion 1533 are detachably coupled. The structures and the technical effects of the second clamping member 153 and the first clamping member 151 are substantially the same, and are not repeated herein for brevity.
The positioning member 155 includes a first positioning portion 1551 and a second positioning portion 1553 detachably connected to the first positioning portion 1551, the first positioning portion 1551 and the second positioning portion 1553 form a positioning groove, and the first receiving groove, the second receiving groove and the positioning groove are configured to receive a shear sample. In a specific arrangement, the first positioning part 1551 and the second positioning part 1553 may be connected by screws. In addition, positioning member 155 needs to be removed before performing the shear test, see FIG. 6. The positioning member 155 is used to fix the shear specimen having the structural plane in advance and then fix both ends of the shear specimen. The technical effect of fixing the shearing samples together in advance is as follows: can avoid shearing the fixed in-process of sample installation, shearing the sample and taking place to remove along the structural plane and lead to the roughness change of structural plane, and then lead to the test result inaccurate.
In order to facilitate understanding of the technical scheme of the present application, the applicant briefly describes the structure surface shear test.
Since the shear specimen has a structured surface, the shear specimen is divided into two parts along the structured surface (hereinafter referred to as a first stage specimen and a second stage specimen). Referring to fig. 7, fig. 7 shows a schematic view of structural plane shear samples at different tilt angles.
Before the shear test, the first section of sample and the second section of sample are connected by the positioning piece 155, namely the first section of sample and the second section of sample are connected into a whole by wrapping the shear sample near the structural surface by the positioning piece 155, so that the first section of sample and the second section of sample cannot be dislocated relatively.
The first section of sample is fixed in the first clamping piece 151, the second section of sample is fixed in the second clamping piece 153, and when the first section of sample is fixed, the position of the structural surface is adjusted to a reserved seam between the first clamping box and the second clamping box, and the plane of the structural surface is parallel to the horizontal plane.
The first clamping member 151 and the second clamping member 153 are clamped by the first clamping cassette 110 and the second clamping cassette 130, respectively, and then the positioning member 155 is removed.
The applicant considers it necessary to explain the removal timing of the positioning member 155, and the positioning member 155 can be removed in any of the following steps:
1. before the first and second clamping members 151 and 153 are clamped by the first and second clamping cassettes 110 and 130:
the first section of sample is contained in the first containing groove, the second section of sample is contained in the second containing groove, and the first clamping piece and the second clamping piece can be detached after the position and the angle of the first clamping piece and the second clamping piece are determined.
2. After the first and second clamping members 151 and 153 are locked: the positioning member 155 is removed through the reserved slot. For example, a screw for connecting the first positioning part 1551 and the second positioning part 1553 is removed by a screwdriver, so that the first positioning part 1551 and the second positioning part 1553 are separated from the cut sample.
It should be noted that removal of retainer 155 is done as often as conditions warrant after all installation work is completed, which has less effect on shearing the sample.
As mentioned above, the length of the cut samples varies, and the first clamping member 151 having a fixed length is not suitable for cut samples having various lengths. To this end, in a particular embodiment, the first clamp 151 further includes a first block 1515, the first block 1515 being removably attachable to the first wing 1513, the first block 1515 being configured to abut a surface of the shear sample.
In this application, first joining in marriage piece 1515 and first alar part 1513 and can dismantle and be connected, has extended the length of first alar part 1513 in other words for first alar part 1513 can be the support shear sample of bigger area, and the deformation when avoiding shearing the sample atress in the shear test process that can be better is to the influence of test result, can improve the precision of test result. For example, when the length of the shear specimen is long and the length of the shear specimen that can be wrapped by the first clamping portion 1511 and the first wing portion 1513 is short, during the test, the shear specimen does not undergo shear failure along the development direction of the structural surface, but has a small-angle deviation with the structural surface, thereby resulting in low test precision and even unreliable test results. And by increasing the reasonable number of the first matching blocks 1515, the shearing sample can be subjected to shearing damage according to the development direction of the structural plane.
Likewise, the second holder 153 can also include a second mating block 1535, the second mating block 1535 can be removably coupled to the second wing 1533, and the second mating block 1535 can be configured to engage a surface of a shear sample. The second block 1535 and the first block 1515 have substantially the same structure and technical effect, and are not repeated herein for brevity.
In particular arrangements, the second wing 1533 is disposed opposite the first wing 1513 in the axial direction of the shear sample. At this time, the second block 1535 and the first block 1515 are also disposed opposite to each other along the axial direction of the shear sample, for example, the first block 1515 is disposed on the upper surface of the first stage sample, and the second block 1535 is disposed on the lower surface of the second stage sample, during the test, the first stage sample is supported by the first block 1515, and the second stage sample is supported by the second block 1535, so as to limit the movement locus of the first stage sample and the second stage sample under the external force, and to cause the shear failure along the direction of the structural plane even if the length of the shear sample is long.
In other embodiments, the first wing 1513 and the first block 1515 define a first groove in communication therewith. The first clamping member 151 further includes a first abutting portion 1517, and the first abutting portion 1517 can be inserted into the first groove and abut against the surface of the shear sample.
In a specific configuration, the positioning element 155 is also provided with a first groove, and the first abutting portion 1517 can be embedded into the first groove of the positioning element 155.
In the present application, both the first abutting portion 1517 and the first block 1515 function to limit the shear failure of the shear sample to the structural plane. The first abutting portion 1517 has the following advantages compared to the first block 1515:
1. the first abutting portion 1517 occupies a smaller space than the first mating block 1515, and is more suitable for being located in the narrow first accommodating space 111, and the structure is more compact.
2. One end of the first abutting portion 1517 can be embedded into the positioning member 155, so that the positioning member 155 and the first clamping member 151 form a whole, the first section of the sample can be fixed more stably and accurately, and the precision of the test result is improved.
It should be noted that the first abutting portion 1517 cannot cross the structural surface of the shear sample (for convenience of illustration, in fig. 5, the first abutting portion 1517 is a case of crossing the structural surface of the shear test), otherwise the shear failure of the shear sample is interfered by the first abutting portion 1517, thereby causing the test to fail.
In other embodiments, the second wing 1533 and the second fitting 1535 define a second groove in communication therewith. The second clamping member 153 further includes a second abutting portion 1537, and the second abutting portion 1537 can be inserted into the second groove and abut against the surface of the shear sample. In the present application, the structure and the technical effects of the second supporting portion 1537 and the first supporting portion 1517 are substantially the same, and are not repeated herein for brevity.
The second wing portion 1533 and the second fitting block 1535 have a second groove communicating with each other, and the second clamping member 153 further includes a second abutting portion 1537, and the second abutting portion 1537 can be inserted into the second groove and abut against the surface of the shear sample.
In a specific configuration, the positioning element 155 is also provided with a second groove, and the second abutting portion 1537 can be embedded into the first groove of the positioning element 155.
In the present application, the reason why the pre-slit can be formed between the first grip cassette 110 and the second grip cassette 130 is that the shear specimen can provide a support for the first grip cassette 110 so that the first grip cassette 110 is suspended above the second grip cassette 130.
In order to avoid the self-weight of the first clamping box 110 from damaging the structural surface during the installation process, the first clamping box 110 and the second clamping box 130 are provided with sliding grooves which are oppositely arranged, and the structural surface locking structure 100 further comprises a sliding part (not shown in the figure), wherein the sliding part can slide along the sliding grooves. When mounted, the first grip case 110 is supported by the sliding portion, and the sliding portion is slid along the sliding groove so that the sliding portion is separated from the first grip case 110 and the second grip case 130 when the shear test is performed. When the steel ball type supporting device is specifically arranged, the sliding part can be a steel ball which is a rigid material and not easy to deform, and a good supporting effect can be achieved.
The application provides a rock core structural surface locking device, which comprises a structural surface locking structure 100 and a rock core 200.
The core 200 is inserted into and fixed to the first holding tank, the second holding tank, and the positioning groove.
The advantage of using core 200 as the shear test piece is that core 200 is long column-like, and the shape is regular, and the diameter is unified, is convenient for the installation to carry out the shear test.
In the present application, the structural surface locking structure 100 includes a first clamping box 110, a second clamping box 130, and a locking assembly 150. The locking assembly 150 includes a first clamping member 151, a second clamping member 153, and a positioning member 155. In use, the first stage sample and the second stage sample are connected and fixed by the positioning member 155, and then the first stage sample is fixed by the first clamping member 151 and the second stage sample is fixed by the second clamping member 153. The first and second clamping members 151 and 153 are fixed by the first and second clamping cartridges 110 and 130, respectively, after the shear specimen is fixed, to restrict the movement thereof. The structure surface locking structure 100 adopts a concept different from the concrete pouring maintenance standard test piece manufacturing, and compared with a concrete pouring method, the structure surface locking structure can shorten the test piece manufacturing time and the shear test period and is convenient for field test.
In addition, the first clamping box 110, the second clamping box 130 and the locking assembly 150 are used in cooperation, so that structural plane shear specimens with different inclination angles can be clamped, and the structural plane locking structure 100 can be suitable for the structural plane shear specimens with different inclination angles.
The above is only a preferred embodiment of the present application and is not intended to limit the present application, and various modifications and variations may be made to the present application by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims (10)

1. A structural surface locking structure is characterized by comprising
A first clamping box having a first accommodating space; the second clamping box is provided with a second accommodating space, and a reserved seam is formed between the first clamping box and the second clamping box; and
the locking assembly comprises a first clamping piece, a second clamping piece and a positioning piece, wherein the first clamping piece is provided with a first accommodating groove, the second clamping piece is provided with a second accommodating groove, the first clamping piece is locked in the first accommodating space, the second clamping piece is locked in the second accommodating space, the positioning piece comprises a first positioning part and a second positioning part detachably connected with the first positioning part, the first positioning part and the second positioning part form a positioning groove, and the first accommodating groove, the second accommodating groove and the positioning groove are constructed to accommodate the shear sample.
2. The structural surface locking structure according to claim 1, wherein the first clamping box includes 2 first stoppers detachably connected, and the first receiving space is formed between the 2 first stoppers.
3. The structural surface locking structure of claim 2, wherein the first clamping box further comprises a first connecting member and a first nut, the first limiting member defines 2 rows of first mounting holes, two ends of the first connecting member define first threaded ends, and the first threaded ends are received in the first mounting holes and are in threaded connection with the first nut to limit the movement of the first clamping member.
4. The structural surface locking structure according to claim 3, wherein the second clamping box includes 2 second limiting members detachably connected, the second accommodating space is formed between the 2 second limiting members, and the reserved slot is formed between the second limiting member and the first limiting member at an interval.
5. The structural surface locking structure of claim 4, wherein the second clamping box further comprises a second connecting member and a second nut, the second limiting member defines 2 rows of second mounting holes, two ends of the second connecting member define second threaded ends, and the second threaded ends are received in the second mounting holes and are in threaded connection with the second nut to limit the movement of the second clamping member.
6. The structural surface locking structure of claim 1, wherein the first clamp comprises a first clamp portion and a first wing portion, the first clamp portion and the first wing portion being removably connected.
7. The structural surface locking structure of claim 6, wherein the first clamp further comprises a first block removably connectable with the first wing, the first block configured to abut a surface of a shear specimen.
8. The structural surface locking structure according to claim 7, wherein the first fitting block and the first wing portion are provided with a first groove that is communicated with each other, and the first clamping member further includes a first abutting portion that can be inserted into the first groove and abut against the surface of the shear sample.
9. The structural surface locking structure of claim 8 wherein the second clamp includes a second clamp portion and a second wing portion, the second clamp portion and the second wing portion being removably connected.
10. The structural surface locking structure of claim 9, wherein the second clamp further comprises a second block removably connectable with the second wing, the second block configured to abut a surface of a shear specimen.
CN201910989884.0A 2019-06-26 2019-10-17 Structural surface locking structure and rock core structural surface locking device Pending CN110887727A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201910560183 2019-06-26
CN2019105601835 2019-06-26

Publications (1)

Publication Number Publication Date
CN110887727A true CN110887727A (en) 2020-03-17

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Application Number Title Priority Date Filing Date
CN201910989884.0A Pending CN110887727A (en) 2019-06-26 2019-10-17 Structural surface locking structure and rock core structural surface locking device

Country Status (1)

Country Link
CN (1) CN110887727A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112964575A (en) * 2021-02-08 2021-06-15 四川大学 Rock shear rheological testing machine under deep ground environment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112964575A (en) * 2021-02-08 2021-06-15 四川大学 Rock shear rheological testing machine under deep ground environment
CN112964575B (en) * 2021-02-08 2022-04-08 四川大学 Rock shear rheological testing machine under deep ground environment

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