CN107389458A - Balancing gate pit based on carbon fibre composite - Google Patents
Balancing gate pit based on carbon fibre composite Download PDFInfo
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- CN107389458A CN107389458A CN201710490967.6A CN201710490967A CN107389458A CN 107389458 A CN107389458 A CN 107389458A CN 201710490967 A CN201710490967 A CN 201710490967A CN 107389458 A CN107389458 A CN 107389458A
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- 239000002131 composite material Substances 0.000 title claims abstract description 53
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims 16
- 229910052799 carbon Inorganic materials 0.000 title claims 16
- 239000000835 fiber Substances 0.000 title claims 12
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 57
- 239000004917 carbon fiber Substances 0.000 claims abstract description 57
- 239000011435 rock Substances 0.000 claims abstract description 57
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 55
- 229910052751 metal Inorganic materials 0.000 claims abstract description 30
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- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 claims description 3
- 239000005011 phenolic resin Substances 0.000 claims description 3
- 229920001568 phenolic resin Polymers 0.000 claims description 3
- 239000000758 substrate Substances 0.000 claims 6
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims 2
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- 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
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- 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
- G01N2203/0058—Kind of property studied
- G01N2203/006—Crack, flaws, fracture or rupture
- G01N2203/0062—Crack or flaws
- G01N2203/0066—Propagation of crack
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- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
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- Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)
Abstract
本发明提供了一种基于碳纤维复合材料的压力室。主要包括:复合材料层、金属基筒,复合材料层包裹在金属基筒的外围,采用碳纤维复合材料制作,金属基筒内放置有岩石试样基座,岩石试样放置于岩石试样基座上,岩石试样的上方放置有垫块;压力室中充围压液并加载围压p,轴向加载力F通过垫块作用于岩石试样上。本发明提供的压力室的密度低,强度高,弹性模量大,同时内部是金属材料,在压力室反复拆装更换岩石试样边缘不易损坏,提高了使用寿命。本发明提供的压力室的工作方式能够适用于压力室轴向压力和周围压力比较大的场合,能够应用于大型的岩土试验机。
The present invention provides a pressure chamber based on carbon fiber composite material. It mainly includes: a composite material layer, a metal base cylinder, the composite material layer is wrapped around the metal base cylinder, and is made of carbon fiber composite material, a rock sample base is placed in the metal base tube, and the rock sample is placed on the rock sample base Above, a block is placed above the rock sample; the pressure chamber is filled with confining pressure fluid and loaded with confining pressure p, and the axial loading force F acts on the rock sample through the block. The pressure chamber provided by the present invention has low density, high strength, and large elastic modulus. At the same time, the interior is made of metal material, and the edge of the rock sample is not easy to be damaged when the pressure chamber is repeatedly disassembled and replaced, and the service life is improved. The working mode of the pressure chamber provided by the invention can be applied to occasions where the axial pressure and surrounding pressure of the pressure chamber are relatively large, and can be applied to large-scale rock and soil testing machines.
Description
技术领域technical field
本发明涉及岩土试验技术领域,尤其涉及一种基于碳纤维复合材料的压力室。The invention relates to the technical field of rock and soil testing, in particular to a pressure chamber based on carbon fiber composite materials.
背景技术Background technique
岩土试验机是为研究岩土的应力、应变关系的一种基础科学试验仪器,由轴压系统、围压系统和温度控制系统组成,工作原理是通过轴压系统对试样施加轴向试样力,通过压力室对试样施加围压,同时通过温度控制系统使试样的上、下端面、试样中部分别处在不同的温度环境下,从而模拟试样在不同温度下的多种实际工况。传统的岩石试验机大部分只能测得岩石试样的应力应变关系曲线,而对于岩石在破裂过程中的裂纹产生和发展过程却无法进行监测并获得图像。The rock and soil testing machine is a basic scientific test instrument for studying the stress and strain relationship of rock and soil. It is composed of an axial pressure system, a confining pressure system and a temperature control system. The sample force is applied to the sample through the pressure chamber, and at the same time, the upper and lower end surfaces of the sample and the middle of the sample are respectively placed in different temperature environments through the temperature control system, thereby simulating various conditions of the sample at different temperatures. Actual working conditions. Most of the traditional rock testing machines can only measure the stress-strain relationship curve of the rock sample, but cannot monitor and obtain images of the crack generation and development process of the rock during the cracking process.
近几年的岩石试验技术有了长足的进步,因此所提出的试验条件也越来越多,岩石试样在多场耦合下的变形情况是现在的研究热点,上述多场通常包括压力场、温度场和电磁场等等。In recent years, rock test technology has made great progress, so more and more test conditions have been proposed. The deformation of rock samples under multi-field coupling is now a research hotspot. The above multi-fields usually include pressure field, temperature field and electromagnetic field and so on.
随着计算机技术的不断完善和发展,CT(Computed Tomography,电子计算机断层扫描)识别技术被应用到岩土试验中来,这为观测岩石试样的破裂过程提供了技术依据。为了在试验过程中对岩土试样各个纵向截面的变形情况进行动态观测,就需要在试验中使得岩石试样与CT扫描仪有相对转动。With the continuous improvement and development of computer technology, CT (Computed Tomography, computerized tomography) recognition technology has been applied to rock and soil tests, which provides a technical basis for observing the fracture process of rock samples. In order to dynamically observe the deformation of each longitudinal section of the rock and soil sample during the test, it is necessary to make the rock sample and the CT scanner rotate relatively during the test.
中国科学院兰州冰川冻土研究所曾采用CT测试技术开展过岩土三轴试验。他们采用的是将应变式三轴压力室直接放到CT机中进行扫描,这种CT扫描方法只适合于压力室轴向压力和周围压力较低的场合,对大型的岩土试验机并不适用。The Lanzhou Institute of Glaciology and Geocryology, Chinese Academy of Sciences has used CT testing technology to carry out geotechnical triaxial tests. What they used was to place the strain-type triaxial pressure chamber directly into the CT machine for scanning. This CT scanning method is only suitable for occasions where the axial pressure of the pressure chamber and the surrounding pressure are low, and it is not suitable for large rock and soil testing machines. Be applicable.
发明专利CN 200620096213.X公开了一种全方位扫描岩土CT三轴仪,它是一种全非金属制作的三轴仪,不但能进行横向断面的扫描,而且能进行纵向(轴向)断面的扫描。但该三轴仪也只适用于轴压和围压较小的场合,对大型岩土试验机不适用。Invention patent CN 200620096213.X discloses an all-round scanning geotechnical CT triaxial instrument, which is a triaxial instrument made of all non-metal, which can not only scan transverse sections, but also can scan longitudinal (axial) sections scan. However, this triaxial instrument is only suitable for occasions where the axial pressure and confining pressure are small, and is not suitable for large-scale rock and soil testing machines.
发明内容Contents of the invention
本发明的实施例提供了一种基于碳纤维复合材料的压力室,以实现有效地利用压力室进行岩土试验。An embodiment of the present invention provides a pressure chamber based on a carbon fiber composite material, so as to effectively use the pressure chamber for geotechnical tests.
为了实现上述目的,本发明采取了如下技术方案。In order to achieve the above object, the present invention adopts the following technical solutions.
一种基于碳纤维复合材料的压力室,包括:A carbon fiber composite based pressure chamber comprising:
复合材料层(5)、金属基筒(6),所述复合材料层(5)包裹在所述金属基筒(6)的外围,采用碳纤维复合材料制作,所述金属基筒(6)内放置有岩石试样基座(7),岩石试样(8)放置于所述岩石试样基座(7)上,所述岩石试样(8)的上方放置有垫块(9);Composite material layer (5), metal base cylinder (6), the composite material layer (5) is wrapped around the periphery of the metal base cylinder (6), and is made of carbon fiber composite material, and the inside of the metal base cylinder (6) A rock sample base (7) is placed, a rock sample (8) is placed on the rock sample base (7), and a pad (9) is placed above the rock sample (8);
所述压力室中充围压液并加载围压p,轴向加载力F通过所述垫块(9)作用于所述岩石试样8上。The pressure chamber is filled with confining pressure fluid and loaded with confining pressure p, and the axial loading force F acts on the rock sample 8 through the pad (9).
进一步地,所述压力室的两端外径大于中间部分的外径。Further, the outer diameters of both ends of the pressure chamber are larger than the outer diameter of the middle part.
进一步地,所述金属基筒的两端部分的壁厚大于中间部分的壁厚,采用内外圆同心的均匀的金属圆筒加工而成。Further, the wall thickness of the two end parts of the metal base cylinder is greater than that of the middle part, and it is processed by using a uniform metal cylinder whose inner and outer circles are concentric.
进一步地,所述金属基筒(6)采用低密度金属材料制作。Further, the metal base cylinder (6) is made of low-density metal material.
进一步地,所述复合材料层(5)包括横纵向碳纤维层一(10)、胶合剂(11)、斜向碳纤维层(12)、横纵向碳纤维层二(13)和硬化层(14)。Further, the composite material layer (5) includes a horizontal and vertical carbon fiber layer one (10), an adhesive (11), an oblique carbon fiber layer (12), a horizontal and vertical carbon fiber layer two (13) and a hardened layer (14).
进一步地,further,
在金属基筒(6)的外圆表面上涂胶合剂(11),并缠绕数层浸润了胶合剂(11)的横纵向碳纤维布形成横纵向碳纤维层(10);在横纵向碳纤维层一(10)上再缠绕数层浸润了胶合剂(11)的斜向碳纤维布形成斜向碳纤维层(12),在所述斜向碳纤维层(12)上再缠绕数层浸润了胶合剂(11)的横纵向碳纤维布形成横纵向碳纤维层二(13),所述复合材料层(5)的最外层涂上硬化层(14)。Coating adhesive (11) on the outer circle surface of metal base tube (6), and winding several layers of horizontal and vertical carbon fiber cloths soaked in adhesive (11) form horizontal and vertical carbon fiber layer (10); (10) wind several layers of oblique carbon fiber cloth soaked in adhesive (11) to form an oblique carbon fiber layer (12), and then wind several layers of oblique carbon fiber cloth soaked in adhesive (11) on the oblique carbon fiber layer (12). ) horizontal and vertical carbon fiber cloth forms horizontal and vertical carbon fiber layer two (13), and the outermost layer of the composite material layer (5) is coated with a hardened layer (14).
进一步地,所述胶合剂(11)包括酚醛树脂。Further, the adhesive (11) includes phenolic resin.
进一步地,所述复合材料层(5)的碳纤维材料的缠绕过程在真空环境中进行,所述复合材料层(5)的外表面通过机加工保证圆度。Further, the winding process of the carbon fiber material of the composite material layer (5) is carried out in a vacuum environment, and the outer surface of the composite material layer (5) is machined to ensure roundness.
进一步地,所述压力室与射线源(3)、工业CT(1)构成岩石力学试验机,所述射线源(3)和所述工业CT(1)分布在试验机压力室的两侧,随着轴向加载力F的增大,所述岩石试样8出现裂纹,射线源(3)发出X射线穿透压力室与岩石试样(8),在工业CT(1)中成像。Further, the pressure chamber, the radiation source (3) and the industrial CT (1) constitute a rock mechanics testing machine, and the radiation source (3) and the industrial CT (1) are distributed on both sides of the pressure chamber of the testing machine, As the axial loading force F increases, cracks appear in the rock sample 8, and the X-rays emitted by the ray source (3) penetrate the pressure chamber and the rock sample (8), and are imaged in the industrial CT (1).
由上述本发明的实施例提供的技术方案可以看出,本发明实施例提供的基于碳纤维复合材料的压力室由内部金属材料和外部碳纤维强化,使压力室的密度低,强度高,弹性模量大,同时内部是金属材料,在压力室反复拆装更换岩石试样边缘不易损坏,提高了使用寿命。本发明实施例提供的基于碳纤维复合材料的压力室的工作方式能够适用于压力室轴向压力和周围压力比较大的场合,能够应用于大型的岩土试验机。It can be seen from the technical solutions provided by the above-mentioned embodiments of the present invention that the pressure chambers based on carbon fiber composite materials provided by the embodiments of the present invention are reinforced by internal metal materials and external carbon fibers, so that the density of the pressure chambers is low, the strength is high, and the elastic modulus Large, and the interior is made of metal materials, and the edge of the rock sample is not easily damaged after repeated disassembly and replacement in the pressure chamber, which improves the service life. The working mode of the pressure chamber based on the carbon fiber composite material provided by the embodiment of the present invention can be applied to occasions where the axial pressure and the surrounding pressure of the pressure chamber are relatively large, and can be applied to large-scale rock and soil testing machines.
本发明附加的方面和优点将在下面的描述中部分给出,这些将从下面的描述中变得明显,或通过本发明的实践了解到。Additional aspects and advantages of the invention will be set forth in part in the description which follows, and will become apparent from the description, or may be learned by practice of the invention.
附图说明Description of drawings
为了更清楚地说明本发明实施例的技术方案,下面将对实施例描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动性的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the following will briefly introduce the accompanying drawings that need to be used in the description of the embodiments. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention. For Those of ordinary skill in the art can also obtain other drawings based on these drawings without any creative effort.
图1为本发明实施例提供的一种基于碳纤维复合材料的压力室的岩石力学试验机的工作场景示意图;Fig. 1 is a schematic diagram of the working scene of a rock mechanics testing machine based on a carbon fiber composite pressure chamber provided by an embodiment of the present invention;
图2为本发明实施例提供的一种基于碳纤维复合材料的压力室的内部结构示意图;Fig. 2 is a schematic diagram of the internal structure of a pressure chamber based on a carbon fiber composite material provided by an embodiment of the present invention;
图3、图4为本发明实施例提供的一种基于碳纤维复合材料的压力室加工工艺示意图;Fig. 3 and Fig. 4 are schematic diagrams of a pressure chamber processing process based on carbon fiber composite materials provided by an embodiment of the present invention;
图中:工业CT1,岩石力学试验机主体2,射线源3,压力室4,复合材料层5,金属基筒6,岩石试样基座7,岩石试样8,垫块9,横纵向碳纤维层一10,胶合剂11,斜向碳纤维层12,横纵向碳纤维层二13,硬化层14。In the figure: Industrial CT1, main body of rock mechanics testing machine 2, ray source 3, pressure chamber 4, composite material layer 5, metal base cylinder 6, rock sample base 7, rock sample 8, pad 9, horizontal and vertical carbon fiber Layer one 10, glue 11, oblique carbon fiber layer 12, horizontal and vertical carbon fiber layer two 13, hardened layer 14.
具体实施方式detailed description
下面详细描述本发明的实施方式,所述实施方式的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施方式是示例性的,仅用于解释本发明,而不能解释为对本发明的限制。Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.
本技术领域技术人员可以理解,除非特意声明,这里使用的单数形式“一”、“一个”、“所述”和“该”也可包括复数形式。应该进一步理解的是,本发明的说明书中使用的措辞“包括”是指存在所述特征、整数、步骤、操作、元件和/或组件,但是并不排除存在或添加一个或多个其他特征、整数、步骤、操作、元件、组件和/或它们的组。应该理解,当我们称元件被“连接”或“耦接”到另一元件时,它可以直接连接或耦接到其他元件,或者也可以存在中间元件。此外,这里使用的“连接”或“耦接”可以包括无线连接或耦接。这里使用的措辞“和/或”包括一个或更多个相关联的列出项的任一单元和全部组合。Those skilled in the art will understand that unless otherwise stated, the singular forms "a", "an", "said" and "the" used herein may also include plural forms. It should be further understood that the word "comprising" used in the description of the present invention refers to the presence of said features, integers, steps, operations, elements and/or components, but does not exclude the presence or addition of one or more other features, Integers, steps, operations, elements, components, and/or groups thereof. It will be understood that when an element is referred to as being "connected" or "coupled" to another element, it can be directly connected or coupled to the other element or intervening elements may also be present. Additionally, "connected" or "coupled" as used herein may include wirelessly connected or coupled. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
本技术领域技术人员可以理解,除非另外定义,这里使用的所有术语(包括技术术语和科学术语)具有与本发明所属领域中的普通技术人员的一般理解相同的意义。还应该理解的是,诸如通用字典中定义的那些术语应该被理解为具有与现有技术的上下文中的意义一致的意义,并且除非像这里一样定义,不会用理想化或过于正式的含义来解释。Those skilled in the art can understand that, unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. It should also be understood that terms such as those defined in commonly used dictionaries should be understood to have a meaning consistent with the meaning in the context of the prior art, and will not be interpreted in an idealized or overly formal sense unless defined as herein Explanation.
为便于对本发明实施例的理解,下面将结合附图以几个具体实施例为例做进一步的解释说明,且各个实施例并不构成对本发明实施例的限定。In order to facilitate the understanding of the embodiments of the present invention, several specific embodiments will be taken as examples for further explanation below in conjunction with the accompanying drawings, and each embodiment does not constitute a limitation to the embodiments of the present invention.
大型岩土试验机的轴压、围压较大,须使用金属制作试样筒,这样必须相应的使用高能CT机。由于大型岩土试验机体积较大,不能直接放入高能CT机中扫描,所以须将试验机的试样筒部分设计为可旋转部件。Large-scale geotechnical testing machines have relatively large axial and confining pressures, so metal sample cylinders must be used, so high-energy CT machines must be used accordingly. Due to the large size of the large-scale geotechnical testing machine, it cannot be directly placed in the high-energy CT machine for scanning, so the sample cylinder part of the testing machine must be designed as a rotatable part.
目前的试验机压力室部分的材料通常选择碳钢、合金钢等材质,也有某些特殊的岩石力学试验机会采用铝合金材料。但是,当这些材质的压力室应用于CT扫描时,钢的密度过大,X射线不容易穿透。而铝合金虽然密度较小,但是其抗拉强度较小,通常承担同样的载荷,其厚度要比钢制压力室厚得多。所以,本发明实施例提出了一种基于碳纤维复合材料的压力室及其制造工艺。The material of the pressure chamber part of the current testing machine is usually made of carbon steel, alloy steel and other materials, and some special rock mechanics testing opportunities use aluminum alloy materials. However, when pressure chambers made of these materials are used in CT scans, the density of steel is too high for X-rays to penetrate easily. Although the aluminum alloy has a lower density, its tensile strength is lower, and it usually bears the same load, and its thickness is much thicker than that of the steel pressure chamber. Therefore, the embodiment of the present invention proposes a carbon fiber composite material-based pressure chamber and its manufacturing process.
本发明实施例提供的一种基于碳纤维复合材料压力室的岩石力学试验机的工作场景如图1所示,包括工业CT1、岩石力学试验机主体2、射线源3和压力室4。其中射线源3和工业CT1分布在试验机压力室4的两侧,射线源3发出的高能射线透过压力室4以及其内的岩石试样8,在工业CT3上成像。The working scene of a rock mechanics testing machine based on a carbon fiber composite material pressure chamber provided by an embodiment of the present invention is shown in FIG. The radiation source 3 and the industrial CT1 are distributed on both sides of the pressure chamber 4 of the testing machine. The high-energy rays emitted by the radiation source 3 pass through the pressure chamber 4 and the rock sample 8 therein, and are imaged on the industrial CT3.
图2为本发明实施例提供的一种基于碳纤维复合材料的压力室的内部结构示意图,压力室4包括复合材料层5、金属基筒6,复合材料层5包裹在金属基筒6的外围,金属基筒6内放置有岩石试样基座7,岩石试样8放置于岩石试样基座7上,岩石试样8的上方放置有垫块9。压力室中充围压液并加载围压p,轴向加载力F通过垫块9作用于岩石试样8上,随着轴向压力的增大,岩石试样8出现裂纹。在此过程中,射线源3发出X射线穿透压力室与岩石试样8,在工业CT1中成像。压力室内围压压力p和轴向加载力F的反力由压力室承担。2 is a schematic diagram of the internal structure of a pressure chamber based on carbon fiber composite materials provided by an embodiment of the present invention. The pressure chamber 4 includes a composite material layer 5 and a metal base cylinder 6. The composite material layer 5 is wrapped around the periphery of the metal base cylinder 6. A rock sample base 7 is placed in the metal base cylinder 6 , a rock sample 8 is placed on the rock sample base 7 , and a spacer 9 is placed above the rock sample 8 . The pressure chamber is filled with confining pressure fluid and loaded with confining pressure p. The axial loading force F acts on the rock sample 8 through the pad 9. As the axial pressure increases, the rock sample 8 cracks. During this process, the X-rays emitted by the ray source 3 penetrate the pressure chamber and the rock sample 8, and are imaged in the industrial CT1. The reaction force of confining pressure p and axial loading force F in the pressure chamber is borne by the pressure chamber.
上述压力室4的两端外径大于中间部分的外径,便于连接机构的夹持,承担轴向加载力F的反力,压力室中间部分壁厚较两端薄,便于X射线的穿透。The outer diameters of both ends of the above-mentioned pressure chamber 4 are larger than the outer diameter of the middle part, which is convenient for the clamping of the connecting mechanism and bears the reaction force of the axial loading force F. The wall thickness of the middle part of the pressure chamber is thinner than that of the two ends, which is convenient for the penetration of X-rays .
图3、图4为本发明实施例提供的一种基于碳纤维复合材料的压力室加工工艺示意图,复合材料层5包括横纵向碳纤维层一10,胶合剂11,斜向碳纤维层12,横纵向碳纤维层二13,硬化层14。金属基筒6是一个两端壁厚较大、中间壁厚较薄的金属筒,它由一根内外圆同心的均匀的金属圆筒加工而成,其中部外径较两端小,过渡部分加工成5°到45°的锥形,形成两端筒壁厚、中间筒壁薄的结构。两端厚壁筒端留出足够的长度,便于夹持旋转,以便缠绕碳纤维材料,这样,金属基筒6兼做制造复合材料压力室的模具。Figure 3 and Figure 4 are schematic diagrams of a pressure chamber processing process based on carbon fiber composite materials provided by the embodiment of the present invention. Layer two 13, hardened layer 14. The metal base cylinder 6 is a metal cylinder with larger wall thickness at both ends and thinner wall thickness in the middle. It is processed by a uniform metal cylinder with inner and outer circles concentric. The outer diameter of the middle part is smaller than that of the two ends. It is processed into a taper of 5° to 45°, forming a structure with thick walls at both ends and thin walls in the middle. Sufficient length is reserved at both ends of the thick-walled cylinder, which is convenient for clamping and rotating, so as to wind the carbon fiber material. In this way, the metal base cylinder 6 doubles as a mold for manufacturing the composite material pressure chamber.
压力室以金属基筒6为复合碳纤维的基础筒,金属基筒(6)采用低密度金属材料制作,作为优选,本实施例采用铝合金材料。采用多层碳纤维复合层即横纵向碳纤维层一10、斜向碳纤维层12和横纵向碳纤维层二13来形成复合材料层5,以便加强金属基筒6的强度。The pressure chamber uses the metal base cylinder 6 as the base cylinder of composite carbon fiber, and the metal base cylinder (6) is made of low-density metal material. As a preference, aluminum alloy material is used in this embodiment. The composite material layer 5 is formed by using multi-layer carbon fiber composite layers, that is, the first horizontal and vertical carbon fiber layer 10 , the oblique carbon fiber layer 12 and the second horizontal and vertical carbon fiber layer 13 , so as to strengthen the strength of the metal base cylinder 6 .
复合材料层5的制作工艺如下:The manufacturing process of the composite material layer 5 is as follows:
首先在金属基筒6的外圆表面上均匀涂胶合剂11,并缠绕数层浸润了胶合剂11的横纵向碳纤维布形成横纵向碳纤维层10;然后在横纵向碳纤维层一10上再缠绕数层浸润了胶合剂11的斜向碳纤维布形成斜向碳纤维层12,此后在上述斜向碳纤维层12上再缠绕数层浸润了胶合剂11的横纵向碳纤维布形成横纵向碳纤维层二13,所述复合材料层(5)的最外层涂上硬化层14。碳纤维层要连续均匀,用以提高压力室的轴向弹性模量,最外层要进行硬化,以提高压力室表面的强度。胶合剂11采用耐高温的胶合剂,本发明实施例采用酚醛树脂。First, the adhesive 11 is uniformly coated on the outer surface of the metal base cylinder 6, and several layers of horizontal and vertical carbon fiber cloth soaked in the adhesive 11 are wound to form a horizontal and vertical carbon fiber layer 10; Layers of oblique carbon fiber cloth soaked with adhesive 11 form an oblique carbon fiber layer 12, and then several layers of transverse and longitudinal carbon fiber cloth impregnated with adhesive 11 are wound on the oblique carbon fiber layer 12 to form a transverse and longitudinal carbon fiber layer 2 13. The outermost layer of the composite material layer (5) is coated with a hardened layer 14. The carbon fiber layer should be continuous and uniform to increase the axial elastic modulus of the pressure chamber, and the outermost layer should be hardened to increase the strength of the pressure chamber surface. The adhesive 11 is a high temperature resistant adhesive, and the embodiment of the present invention uses a phenolic resin.
在碳纤维加强材料缠绕过程中,在真空环境中进行,避免材料中混入气泡,影响材料的均匀性,进而影响CT成像质量。During the winding process of carbon fiber reinforced materials, it is carried out in a vacuum environment to avoid mixing air bubbles in the material, which will affect the uniformity of the material and further affect the quality of CT imaging.
在金属基筒6与复合材料层5固化后,外表面通过机加工保证圆度,并去掉两端多余部分复合层和金属材料,完成压力室的制造,其结构如图4。After the metal base cylinder 6 and the composite material layer 5 are solidified, the outer surface is machined to ensure the roundness, and the excess composite layer and metal material at both ends are removed to complete the manufacture of the pressure chamber, and its structure is shown in Figure 4.
综上所述,本发明实施例提供的基于碳纤维复合材料的压力室由内部金属材料和外部碳纤维强化,使压力室的密度低,强度高,弹性模量大,同时内部是金属材料,在压力室反复拆装更换岩石试样边缘不易损坏,提高了使用寿命。本发明实施例提供的基于碳纤维复合材料的压力室的工作方式能够适用于压力室轴向压力和周围压力比较大的场合,能够有效地应用于大型的岩土试验机。In summary, the carbon fiber composite material-based pressure chamber provided by the embodiment of the present invention is reinforced by internal metal materials and external carbon fibers, so that the pressure chamber has low density, high strength, and large elastic modulus. At the same time, the interior is made of metal materials. The edge of the rock sample is not easy to be damaged by repeated disassembly and assembly of the chamber, which improves the service life. The working mode of the pressure chamber based on the carbon fiber composite material provided by the embodiment of the present invention can be applied to occasions where the axial pressure and the surrounding pressure of the pressure chamber are relatively large, and can be effectively applied to large-scale geotechnical testing machines.
基于这种碳纤维压力室的岩石力学试验机射线穿透效果好,便于应用工业CT连续扫描岩土试样在轴向加载的情况下的内部动态,有利于深化岩土力学的研究。The ray penetration effect of the rock mechanics testing machine based on this carbon fiber pressure chamber is good, and it is convenient to apply industrial CT to continuously scan the internal dynamics of rock and soil samples under axial loading, which is conducive to deepening the study of rock and soil mechanics.
本领域普通技术人员可以理解:附图只是一个实施例的示意图,附图中的模块或流程并不一定是实施本发明所必须的。Those skilled in the art can understand that the accompanying drawing is only a schematic diagram of an embodiment, and the modules or processes in the accompanying drawing are not necessarily necessary for implementing the present invention.
本领域普通技术人员可以理解:实施例中的装置中的部件可以按照实施例描述分布于实施例的装置中,也可以进行相应变化位于不同于本实施例的一个或多个装置中。上述实施例的部件可以合并为一个部件,也可以进一步拆分成多个子部件。Those of ordinary skill in the art can understand that: the components in the device in the embodiment can be distributed in the device in the embodiment according to the description in the embodiment, and can also be changed and located in one or more devices different from the embodiment. The components in the above embodiments can be combined into one component, and can also be further divided into multiple subcomponents.
以上所述,仅为本发明较佳的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本发明的保护范围之内。因此,本发明的保护范围应该以权利要求的保护范围为准。The above is only a preferred embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any person skilled in the art within the technical scope disclosed in the present invention can easily think of changes or Replacement should be covered within the protection scope of the present invention. Therefore, the protection scope of the present invention should be determined by the protection scope of the claims.
Claims (9)
- A kind of 1. balancing gate pit based on carbon fibre composite, it is characterised in that including:Composite layer (5), Metal Substrate cylinder (6), the composite layer (5) are wrapped in the periphery of the Metal Substrate cylinder (6), adopted Made of carbon fibre composite, be placed with rock sample pedestal (7) in the Metal Substrate cylinder (6), rock sample (8) is positioned over On the rock sample pedestal (7), cushion block (9) is placed with above the rock sample (8);Confined pressure liquid is filled in the balancing gate pit and loads confined pressure p, axially loaded power F the rock is acted on by the cushion block (9) On sample (8).
- 2. the balancing gate pit according to claim 1 based on carbon fibre composite, it is characterised in that the two of the balancing gate pit External diameter is held to be more than the external diameter of center section.
- 3. the balancing gate pit according to claim 2 based on carbon fibre composite, it is characterised in that the Metal Substrate cylinder (6) wall thickness of two end portions is more than the wall thickness of center section, is process using the concentric uniform metallic cylinder of inside and outside circle.
- 4. the balancing gate pit according to claim 3 based on carbon fibre composite, it is characterised in that the Metal Substrate cylinder (6) made using low density-metal material.
- 5. the balancing gate pit based on carbon fibre composite according to any one of Claims 1-4, it is characterised in that described It is fine that composite layer (5) includes transverse and longitudinal carbon fiber layer one (10), adhesive (11), oblique carbon fiber layer (12), transverse and longitudinal carbon Tie up layer two (13) and hardened layer (14).
- 6. the balancing gate pit according to claim 5 based on carbon fibre composite, it is characterised in that in Metal Substrate cylinder (6) Outer round surface on apply adhesive (11), and writhing number layer infiltrated adhesive (11) transverse and longitudinal carbon cloth formed transverse and longitudinal Carbon fiber layer (10);Writhing number layer has infiltrated the oblique carbon cloth of adhesive (11) again on transverse and longitudinal carbon fiber layer one (10) Oblique carbon fiber layer (12) is formed, writhing number layer has infiltrated the transverse and longitudinal of adhesive (11) again on the oblique carbon fiber layer (12) Transverse and longitudinal carbon fiber layer two (13) is formed to carbon cloth, the outermost layer of the composite layer (5) coats hardened layer (14).
- 7. the balancing gate pit according to claim 6 based on carbon fibre composite, it is characterised in that the adhesive (11) Including phenolic resin.
- 8. the balancing gate pit according to claim 6 based on carbon fibre composite, it is characterised in that the composite layer (5) winding process of carbon fibre material is carried out in vacuum environment, and the outer surface of the composite layer (5) passes through machining Ensure circularity.
- 9. the balancing gate pit according to claim 1 based on carbon fibre composite, it is characterised in that the balancing gate pit is with penetrating Line source (3), industry CT (1) form rock mechanics experiment machine, and the radiographic source (3) and the industry CT (1) are distributed in testing machine The both sides of balancing gate pit, with axially loaded power F increase, the rock sample 8 is cracked, and radiographic source (3) sends X ray and worn Saturating balancing gate pit and rock sample (8), are imaged in industry CT (1).
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108398344A (en) * | 2018-02-26 | 2018-08-14 | 合肥工业大学 | It is a kind of can in-situ observation material internal fatigue crack growth frictional wear test device |
| CN111855428A (en) * | 2020-08-20 | 2020-10-30 | 西安建筑科技大学 | A kind of rock sample confining pressure application test device and test method |
| CN113188917A (en) * | 2021-05-25 | 2021-07-30 | 核工业理化工程研究院 | Cylinder external pressure resistance testing device |
| CN113466107A (en) * | 2021-07-09 | 2021-10-01 | 东华理工大学 | Water permeability sleeve for indoor test and manufacturing method thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2000006866A1 (en) * | 1998-07-29 | 2000-02-10 | Aumann James T | Method and apparatus for recovering core samples under pressure |
| CN102288480A (en) * | 2011-06-27 | 2011-12-21 | 河海大学 | Device for sealing triaxial test sample of soil body and method for using device |
| CN103974817A (en) * | 2011-12-07 | 2014-08-06 | 轻型结构中心萨克森有限公司 | Connecting arrangement for connecting a fiber composite component to a second component |
| CN203854258U (en) * | 2014-01-29 | 2014-10-01 | 上海云逸民用航空科技有限公司 | Composite material high-bearing-strength rod |
| CN105181471A (en) * | 2015-09-11 | 2015-12-23 | 中国矿业大学 | Rock true triaxial test system with CT (Computed Tomography) real-time scanning system and method |
| CN105973919A (en) * | 2016-07-28 | 2016-09-28 | 北京瑞莱博石油技术有限公司 | Core holding unit |
| CN106546490A (en) * | 2016-10-25 | 2017-03-29 | 北京交通大学 | Rotatable rock mechanics experiment machine with internal heat |
-
2017
- 2017-06-23 CN CN201710490967.6A patent/CN107389458A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2000006866A1 (en) * | 1998-07-29 | 2000-02-10 | Aumann James T | Method and apparatus for recovering core samples under pressure |
| CN102288480A (en) * | 2011-06-27 | 2011-12-21 | 河海大学 | Device for sealing triaxial test sample of soil body and method for using device |
| CN103974817A (en) * | 2011-12-07 | 2014-08-06 | 轻型结构中心萨克森有限公司 | Connecting arrangement for connecting a fiber composite component to a second component |
| CN203854258U (en) * | 2014-01-29 | 2014-10-01 | 上海云逸民用航空科技有限公司 | Composite material high-bearing-strength rod |
| CN105181471A (en) * | 2015-09-11 | 2015-12-23 | 中国矿业大学 | Rock true triaxial test system with CT (Computed Tomography) real-time scanning system and method |
| CN105973919A (en) * | 2016-07-28 | 2016-09-28 | 北京瑞莱博石油技术有限公司 | Core holding unit |
| CN106546490A (en) * | 2016-10-25 | 2017-03-29 | 北京交通大学 | Rotatable rock mechanics experiment machine with internal heat |
Non-Patent Citations (1)
| Title |
|---|
| 周建波 等: "《金属材料与热处理》", 31 December 2014, 浙江大学出版社 * |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108398344A (en) * | 2018-02-26 | 2018-08-14 | 合肥工业大学 | It is a kind of can in-situ observation material internal fatigue crack growth frictional wear test device |
| CN108398344B (en) * | 2018-02-26 | 2020-07-31 | 合肥工业大学 | Friction wear test device capable of observing fatigue crack growth inside material in situ |
| CN111855428A (en) * | 2020-08-20 | 2020-10-30 | 西安建筑科技大学 | A kind of rock sample confining pressure application test device and test method |
| CN113188917A (en) * | 2021-05-25 | 2021-07-30 | 核工业理化工程研究院 | Cylinder external pressure resistance testing device |
| CN113466107A (en) * | 2021-07-09 | 2021-10-01 | 东华理工大学 | Water permeability sleeve for indoor test and manufacturing method thereof |
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