[go: up one dir, main page]

CN110947527B - Structure for reinforcing signal data pipeline of supergravity centrifugal machine - Google Patents

Structure for reinforcing signal data pipeline of supergravity centrifugal machine Download PDF

Info

Publication number
CN110947527B
CN110947527B CN201911310314.0A CN201911310314A CN110947527B CN 110947527 B CN110947527 B CN 110947527B CN 201911310314 A CN201911310314 A CN 201911310314A CN 110947527 B CN110947527 B CN 110947527B
Authority
CN
China
Prior art keywords
carbon fiber
pipeline
reinforced
reinforcing
signal data
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.)
Active
Application number
CN201911310314.0A
Other languages
Chinese (zh)
Other versions
CN110947527A (en
Inventor
郑传祥
林娇
蒋建群
林伟岸
窦丹阳
黄维
颜加明
陈云敏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang University ZJU
Original Assignee
Zhejiang University ZJU
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhejiang University ZJU filed Critical Zhejiang University ZJU
Priority to CN201911310314.0A priority Critical patent/CN110947527B/en
Publication of CN110947527A publication Critical patent/CN110947527A/en
Application granted granted Critical
Publication of CN110947527B publication Critical patent/CN110947527B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B04CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
    • B04BCENTRIFUGES
    • B04B7/00Elements of centrifuges
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
  • Centrifugal Separators (AREA)

Abstract

本发明公开了一种用于超重力离心机信号数据管线加强的结构。加强结构安装于超重力离心机的高速转臂上,加强结构装在高速转臂顶面上,加强结构内部布置固定各类管线,加强结构包括分别在各类管线上下两侧对称布置的结构单元和结构单元外的增强碳纤维复合层,上下两侧的结构单元分别包裹在管线的上面和下面,在相邻两根管线之间结构单元的内凹部分采用增强碳纤维复合层进行填平,结构单元和增强碳纤维复合层是由纤维布置不同的多层碳纤维复合材料层层叠构成。本发明的信号数据线加强结构可以在使用过程中克服由于超重力离心机高速旋转下带来的巨大拉力,防止信号数据线在离心机高速运转下被甩出、拉断。信号数据线固定牢靠,结构简单。

Figure 201911310314

The invention discloses a structure for strengthening the signal data pipeline of a supergravity centrifuge. The reinforced structure is installed on the high-speed rotating arm of the hypergravity centrifuge, and the reinforced structure is installed on the top surface of the high-speed rotating arm. Various pipelines are arranged and fixed inside the reinforced structure. The reinforced structure includes structural units arranged symmetrically on the upper and lower sides of the various pipelines. and the reinforced carbon fiber composite layer outside the structural unit, the structural units on the upper and lower sides are wrapped above and below the pipeline respectively, and the concave part of the structural unit between the adjacent two pipelines is filled with the reinforced carbon fiber composite layer. The unit and the reinforced carbon fiber composite layer are composed of multi-layer carbon fiber composite material layers with different fiber arrangements. The signal data line reinforcement structure of the present invention can overcome the huge pulling force caused by the high-speed rotation of the supergravity centrifuge during use, and prevent the signal data line from being thrown out and broken under the high-speed operation of the centrifuge. The signal data line is firmly fixed and the structure is simple.

Figure 201911310314

Description

一种用于超重力离心机信号数据管线加强的结构A structure for strengthening signal data pipeline of hypergravity centrifuge

技术领域technical field

本发明涉及超重力离心场下的结构加强结构设计领域的一个超重力离心机内部结构,特别是涉及了一种超重力离心场信号数据线加强结构设计。The invention relates to an internal structure of a hypergravity centrifuge in the field of structural strengthening structure design under a hypergravity centrifugal field, in particular to a design of a strengthening structure for a signal data line in a hypergravity centrifugal field.

背景技术Background technique

超重力离心机是研究地质过程演变、土体污染物迁移、深地深海工程灾变等问题的缩时缩尺实验的重要实验装置,然而在超重力环境下,巨大的离心力作用使得如传感器、数据线、水气等进出管线等承受巨大的离心力,且巨大的离心力极易使得这些信号数据线、物料进出管线在固定后被拉裂、拉断。因此,为了保证信号数据线、物料输送管线在超重力场测量过程中可以正常使用,需要对其结构上进行加强和固定。The hypergravity centrifuge is an important experimental device for time-lapse and scale-down experiments to study the evolution of geological processes, the migration of soil pollutants, and the disasters of deep-sea and deep-sea engineering. The incoming and outgoing pipelines such as lines, water and gas are subject to huge centrifugal force, and the huge centrifugal force can easily cause these signal data lines and material in and out pipelines to be cracked and broken after being fixed. Therefore, in order to ensure that the signal data line and the material conveying pipeline can be used normally during the measurement of the hypergravity field, it is necessary to strengthen and fix the structure.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于克服超重力场下信号数据线难以固定和使用过程中易被拉断损坏的缺点,设计一种信号数据线的固定加强结构,可以使得包含信号数据线在内的加强结构在使用过程中承受很大的拉力,防止信号数据线在超重力离心机高速运转下被甩出、拉断。适用于超重力离心机以及其他高速运转的设备。The purpose of the present invention is to overcome the shortcomings that the signal data line is difficult to fix under the supergravity field and is easily broken and damaged during use, and to design a fixed reinforcement structure for the signal data line, which can make the reinforcement structure including the signal data line in the It bears a lot of pulling force during use to prevent the signal data line from being thrown out and broken under the high-speed operation of the supergravity centrifuge. Suitable for ultra-gravity centrifuges and other high-speed running equipment.

本发明采用的技术方案是:The technical scheme adopted in the present invention is:

本发明加强结构安装于超重力离心机的高速转臂上,加强结构通过内六角螺钉和防松垫片固定定位装在高速转臂顶面上,同时加强结构下表面用粘结剂粘结在高速转臂顶面上;加强结构内部布置固定各类管线,各类管线的一端通过管线入舱接头进入超重力实验舱内与各仪器仪表连接,各类管线的另一端向超重力离心机的中心转轴延伸并穿设进入中心转轴中空腔内并与中心转轴上的滑环机构连接,经过滑环机构后连接到管线引出接头引出到超重力离心机的离心室外面。The reinforcing structure of the present invention is installed on the high-speed rotating arm of the supergravity centrifuge, and the reinforcing structure is fixed and positioned on the top surface of the high-speed rotating arm by means of hexagon socket screws and anti-loose washers, and at the same time, the lower surface of the reinforcing structure is bonded on the top surface of the high-speed rotating arm with an adhesive. On the top surface of the high-speed rotating arm; various pipelines are arranged and fixed inside the reinforced structure. One end of each pipeline enters the hypergravity experimental cabin through the pipeline entry joint to connect with each instrument, and the other end of each pipeline is connected to the supergravity centrifuge. The central rotating shaft extends and penetrates into the hollow cavity of the central rotating shaft and is connected with the slip ring mechanism on the central rotating shaft.

各类管线包括金属管、导线、光纤类数据线、非金属管、屏蔽绝缘类管线和传感器引线。Various types of pipelines include metal pipes, wires, optical fiber data lines, non-metallic pipes, shielded and insulated pipelines and sensor leads.

所述的加强结构包括分别在各类管线上下两侧对称布置的碳纤维复合材料层和增强碳纤维补平层,上下两侧的纤维复合材料层和增强碳纤维补平层分别包裹在管线的上面和下面,在相邻两根管线之间结构单元的内凹部分采用增强碳纤维补平层进行填平,从而形成三明治复合加强夹层结构;复合加强夹层结构是由五层或者更多层不同纤维方向的碳纤维复合材料层层合构成,单层碳纤维复合材料层是由数根增强碳纤维平行间隔埋设于环氧树脂基体中构成,五层碳纤维复合材料层中的增强碳纤维平行布置方向不同,上侧的五层结构单元中的增强碳纤维平行布置方向从下到上分别为连续的两个沿垂直于管线方向、沿平行于管线方向、连续的两个沿和管线方向之间夹角为60°和-60°;增强碳纤维补平层也是由数根增强碳纤维平行间隔埋设于环氧树脂基体中构成,增强碳纤维补平层的增强碳纤维平行布置方向平行于管线方向。The reinforcing structure includes carbon fiber composite material layers and reinforced carbon fiber leveling layers symmetrically arranged on the upper and lower sides of various pipelines, respectively, and the fiber composite material layers and reinforced carbon fiber leveling layers on the upper and lower sides are respectively wrapped above and below the pipeline. , the concave part of the structural unit between two adjacent pipelines is filled with a reinforced carbon fiber leveling layer to form a sandwich composite reinforced sandwich structure; the composite reinforced sandwich structure is composed of five or more layers with different fiber directions. The carbon fiber composite material layer is laminated. The single-layer carbon fiber composite material layer is composed of several reinforced carbon fibers embedded in the epoxy resin matrix at parallel intervals. The reinforcing carbon fibers in the five-layer carbon fiber composite material layer are arranged in different parallel directions. The parallel arrangement direction of the reinforced carbon fibers in the layer structure unit is from bottom to top, respectively, two continuous along the direction perpendicular to the pipeline, along the direction parallel to the pipeline, and the included angles between the two continuous along and the pipeline direction are 60° and -60° °; The reinforced carbon fiber leveling layer is also composed of several reinforced carbon fibers embedded in the epoxy resin matrix at parallel intervals, and the parallel arrangement direction of the reinforced carbon fibers of the reinforced carbon fiber leveling layer is parallel to the pipeline direction.

所述的碳纤维复合材料层用增强玻璃纤维、增强芳纶纤维或硼纤维等替代。The carbon fiber composite material layer is replaced with reinforced glass fiber, reinforced aramid fiber or boron fiber.

所述的环氧树脂基体用双马酰胺树脂、酚醛树脂等替代。The epoxy resin matrix is replaced by bismaramide resin, phenolic resin and the like.

本发明的有益效果是:The beneficial effects of the present invention are:

本发明的信号数据线加强固定结构,由于信号数据线埋置于碳纤维层中间,当转轴带动转臂高速旋转时,信号数据线承受的巨大离心力作用,将分布到碳纤维层上,几乎全部由碳纤维层承担。由于碳纤维复合材料质量非常小,因此离心力也非常小具,且具有极高的轴向抗拉强度,因此碳纤维层可以克服离心力带来的巨大拉力。The signal data line of the present invention strengthens the fixed structure. Since the signal data line is embedded in the middle of the carbon fiber layer, when the rotating shaft drives the rotating arm to rotate at a high speed, the huge centrifugal force that the signal data line bears will be distributed on the carbon fiber layer, and almost all of it is made of carbon fiber. layer undertakes. Because the mass of carbon fiber composites is very small, the centrifugal force is also very small, and it has extremely high axial tensile strength, so the carbon fiber layer can overcome the huge tensile force caused by centrifugal force.

考虑到泊松效应,同时对碳纤维层设计为多角度铺设,可增强该信号数据线加强结构的不同方向的抗拉强度。在该加强结构下信号数据线固定牢靠,结构简单。Considering the Poisson effect, the carbon fiber layer is designed to be laid at multiple angles, which can enhance the tensile strength of the signal data line reinforcement structure in different directions. Under the reinforced structure, the signal data line is firmly fixed and the structure is simple.

附图说明Description of drawings

图1是本发明加强结构的主视图。FIG. 1 is a front view of the reinforcing structure of the present invention.

图2是本加强结构的俯视图。FIG. 2 is a plan view of the present reinforcement structure.

图3是本加强结构横截面剖视图。FIG. 3 is a cross-sectional view of the reinforcing structure.

图4是本加强结构的实施例纤维敷设图。FIG. 4 is a fiber laying diagram of an embodiment of the reinforcing structure.

图中:1、超重力实验舱,2、管线入舱接头,3、加强结构,4、高速转臂,5、轴承系统,6、滑环机构,7、管线引出接头,8、中心转轴,9、增强碳纤维补平层,10、金属管,11、导线,12、光纤类数据线,13、非金属管,14、屏蔽绝缘类管线,15、传感器引线,16、内六角螺钉,17、防松垫片,18、各类管线,19、花键,20、碳纤维复合材料层,21、增强碳纤维,22、环氧树脂基体。In the figure: 1. Hypergravity experimental cabin, 2. Pipeline entry joint, 3. Reinforcement structure, 4. High-speed rotating arm, 5. Bearing system, 6. Slip ring mechanism, 7. Pipeline outlet joint, 8. Center shaft, 9. Reinforced carbon fiber leveling layer, 10, Metal tube, 11, Conductor, 12, Optical fiber data cable, 13, Non-metallic tube, 14, Shielded insulation pipeline, 15, Sensor lead, 16, Hex socket head cap screw, 17, Anti-loose gasket, 18, various types of pipelines, 19, splines, 20, carbon fiber composite material layer, 21, reinforced carbon fiber, 22, epoxy resin matrix.

具体实施方式Detailed ways

下面结合附图和实施例对本发明作进一步的说明,但是本实施例不是对本发明的限制。The present invention will be further described below with reference to the accompanying drawings and embodiments, but the embodiments are not intended to limit the present invention.

如图1和图2所示,超重力离心机具有高速转臂4、轴承系统5、超重力实验舱1和中心转轴8,两只超重力实验舱1挂装于高速转臂4的两个外端,高速转臂4中部通过花键19与中心转轴8同轴连接,中心转轴8安装于轴承系统5上,构成超重力离心机的转子系统;加强结构3安装于超重力离心机的高速转臂4上,加强结构3通过内六角螺钉16和防松垫片17固定定位装在高速转臂4顶面上,同时加强结构3下表面用粘结剂粘结在高速转臂4顶面上。As shown in Figures 1 and 2, the hypergravity centrifuge has a high-speed rotating arm 4, a bearing system 5, a hypergravity experimental cabin 1 and a central shaft 8, and two hypergravity experimental cabins 1 are mounted on two of the high-speed rotating arms 4. At the outer end, the middle part of the high-speed rotating arm 4 is coaxially connected with the central rotating shaft 8 through the spline 19, and the central rotating shaft 8 is installed on the bearing system 5 to form the rotor system of the hypergravity centrifuge; On the rotating arm 4, the reinforcing structure 3 is fixed and positioned on the top surface of the high-speed rotating arm 4 through the hexagon socket head screw 16 and the anti-loosening washer 17, and at the same time, the lower surface of the reinforcing structure 3 is bonded to the top surface of the high-speed rotating arm 4 with adhesive. superior.

加强结构3内部布置固定各类管线18,各类管线18的整体置于加强结构3中间得到加强,各类管线18的一端通过管线入舱接头2进入超重力实验舱1内与各仪器仪表连接,各类管线18的另一端向超重力离心机的中心转轴8延伸并穿设进入中心转轴8中空腔内并与中心转轴8上的滑环机构6连接,经过滑环机构6后连接到管线引出接头7引出到超重力离心机的离心室外面,管线引出接头7位于中心转轴8的顶部。Various types of pipelines 18 are arranged and fixed inside the reinforcement structure 3. The whole of various pipelines 18 is placed in the middle of the reinforcement structure 3 to be strengthened. , the other ends of the various pipelines 18 extend to the central rotating shaft 8 of the hypergravity centrifuge and penetrate into the hollow cavity of the central rotating shaft 8 and are connected with the slip ring mechanism 6 on the central rotating shaft 8, and are connected to the pipeline after passing through the slip ring mechanism 6. The lead-out joint 7 is led out to the outside of the centrifuge chamber of the supergravity centrifuge, and the pipeline lead-out joint 7 is located on the top of the central rotating shaft 8 .

具体实施中,滑环机构6具体可包括有外滑环和内滑环,外滑环可固定于超重力离心机的离心舱的内壁,内滑环可固定于中心转轴外壁。In a specific implementation, the slip ring mechanism 6 may specifically include an outer slip ring and an inner slip ring, the outer slip ring may be fixed on the inner wall of the centrifuge chamber of the hypergravity centrifuge, and the inner slip ring may be fixed on the outer wall of the central rotating shaft.

如图3所示,各类管线18包括金属管10、导线11、光纤类数据线12、非金属管13、屏蔽绝缘类管线14和传感器引线15。As shown in FIG. 3 , various types of pipelines 18 include metal pipes 10 , wires 11 , optical fiber data lines 12 , non-metal pipes 13 , shielded and insulated pipelines 14 and sensor leads 15 .

如图4所示,加强结构3包括分别在各类管线18上下两侧对称布置的结构单元和结构单元外的增强碳纤维复合层9,上下两侧的结构单元分别包裹在管线18的上面和下面,在相邻两根管线18之间结构单元形成的内凹部分采用增强碳纤维复合层9进行填平,使得填平后增强碳纤维复合层9外侧表面和结构单元外侧表面平齐,从而形成三明治复合加强夹层结构。As shown in FIG. 4 , the reinforcing structure 3 includes structural units symmetrically arranged on the upper and lower sides of various pipelines 18 and a reinforced carbon fiber composite layer 9 outside the structural units. The structural units on the upper and lower sides are wrapped on the top and bottom of the pipeline 18 respectively. , the concave part formed by the structural unit between the two adjacent pipelines 18 is filled with the reinforced carbon fiber composite layer 9, so that the outer surface of the reinforced carbon fiber composite layer 9 is flush with the outer surface of the structural unit after filling, so as to form a sandwich Composite reinforced sandwich structure.

上述结构单元是由纤维布置不同的五层碳纤维或者更多层叠合而成,本实施例采用五层复合材料层20层叠构成,单层碳纤维复合材料层20是由数根增强碳纤维21平行间隔埋设于环氧树脂基体22中构成,五层碳纤维复合材料层20中的增强碳纤维21平行布置方向不同,形成多角度铺设,上侧的五层结构单元中的增强碳纤维21平行布置方向从下到上分别为连续的两个沿垂直于管线18方向、沿平行于管线18方向、连续的两个沿和管线18方向之间夹角为60°和-60°,以垂直于管线18方向为0°布置角度,形成0°、0°、90°、30°、-30°布置角度,下侧的五层结构单元和上侧的五层结构单元以加强结构3的水平中线对称。The above-mentioned structural units are formed by stacking five layers of carbon fibers or more layers with different fiber arrangements. In this embodiment, five layers of composite material layers 20 are stacked and formed. The single-layer carbon fiber composite material layer 20 is composed of several reinforced carbon fibers 21. It is formed in the epoxy resin matrix 22, and the reinforcing carbon fibers 21 in the five-layer carbon fiber composite material layer 20 are arranged in different directions in parallel, forming multi-angle laying, and the reinforcing carbon fibers 21 in the five-layer structural unit on the upper side are arranged in parallel from bottom to top. The included angles between the two continuous along the direction perpendicular to the pipeline 18, along the direction parallel to the pipeline 18, and the two continuous along the direction of the pipeline 18 are 60° and -60°, and the direction perpendicular to the pipeline 18 is 0° The arrangement angle is 0°, 0°, 90°, 30°, -30°, and the five-layer structural unit on the lower side and the five-layer structural unit on the upper side are symmetrical with the horizontal midline of the reinforcement structure 3 .

增强碳纤维复合层9也是由数根增强碳纤维21平行间隔埋设于环氧树脂基体22中构成,增强碳纤维复合层9的增强碳纤维21平行布置方向平行于管线18方向。The reinforced carbon fiber composite layer 9 is also composed of several reinforced carbon fibers 21 embedded in the epoxy resin matrix 22 at parallel intervals. The parallel arrangement direction of the reinforced carbon fibers 21 of the reinforced carbon fiber composite layer 9 is parallel to the direction of the pipeline 18 .

具体实施中,各类管线18等间隔布置在上下两侧结构单元的中间,增强碳纤维复合层9与高速转臂4之间通过内六角螺钉16和胶黏剂相连。In the specific implementation, various types of pipelines 18 are arranged at equal intervals in the middle of the upper and lower structural units, and the reinforced carbon fiber composite layer 9 and the high-speed rotating arm 4 are connected by hexagon socket screws 16 and adhesives.

本发明的实施例子情况如下:Embodiments of the present invention are as follows:

根据附图1,一台1500g的超重力离心机,机室内半径为9.7m,离心机转臂半径为4.5m,转子最大线速度300m/s,以包覆于碳纤维层中的是直径为3mm的铜线(铜的密度ρ1为8.96×103kg/m3)作为管线,则铜线质量m1为:According to accompanying drawing 1, a 1500g hypergravity centrifuge, the inner radius of the machine is 9.7m, the radius of the centrifuge arm is 4.5m, the maximum linear speed of the rotor is 300m/s, and the diameter of the one wrapped in the carbon fiber layer is 3mm. The copper wire (the density of copper ρ 1 is 8.96×10 3 kg/m 3 ) is used as a pipeline, then the mass m 1 of the copper wire is:

m1=ρ1V1=8.96×10-3×π×1.52×4500×10-3=0.285kgm 11 V 1 =8.96×10 −3 ×π×1.5 2 ×4500×10 −3 =0.285kg

其中,V1表示转臂上单根铜线体积。Among them, V 1 represents the volume of a single copper wire on the rotating arm.

铜线所受离心力F1大小为:The magnitude of the centrifugal force F 1 on the copper wire is:

Figure BDA0002324339660000041
Figure BDA0002324339660000041

r1表示离心机转臂半径的一半,m;

Figure BDA0002324339660000042
表示离心机旋转角速度,rad/s;v表示离心机转子线速度,m/s;r表示离心机转臂半径,m。r 1 represents half of the radius of the centrifuge arm, m;
Figure BDA0002324339660000042
represents the rotational angular velocity of the centrifuge, rad/s; v represents the linear velocity of the centrifuge rotor, m/s; r represents the radius of the centrifuge arm, m.

则铜线上所受拉应力σ1大小为:Then the tensile stress σ 1 on the copper wire is:

Figure BDA0002324339660000043
Figure BDA0002324339660000043

其中,A1表示单根铜线的横向截面积,mm2Among them, A 1 represents the transverse cross-sectional area of a single copper wire, mm 2 .

由计算结果可知,铜线上的拉应力已经明显超过其许用应力(黄铜的屈服强度极限为200MPa-300MPa),因此必须要对铜线做加强。It can be seen from the calculation results that the tensile stress of the copper wire has obviously exceeded its allowable stress (the yield strength limit of brass is 200MPa-300MPa), so the copper wire must be strengthened.

具体实施的加强结构分为在各类管线18上下两侧对称布置的结构单元和结构单元外的增强碳纤维复合层9,上下两侧的结构单元分别包裹在管线18的上面和下面,在相邻两根管线18之间结构单元形成的内凹部分采用增强碳纤维复合层9进行填平平齐,使得加强结构整体形成截面矩形,从而形成三明治复合加强夹层结构。The concretely implemented reinforcing structure is divided into structural units symmetrically arranged on the upper and lower sides of various pipelines 18 and a reinforced carbon fiber composite layer 9 outside the structural units. The concave portion formed by the structural unit between the two pipelines 18 is filled and flushed with the reinforced carbon fiber composite layer 9, so that the reinforced structure as a whole has a rectangular cross-section, thereby forming a sandwich composite reinforced sandwich structure.

两个结构单元包括共10层碳纤维复合材料层20,每层厚0.125mm,每个结构单元沿厚度方向从靠近管线的内侧向外依次为:0°铺设2层,90°铺设1层,30°铺设1层,-30°铺设1层,0°为垂直于管线18方向,依此对称铺层。The two structural units include a total of 10 layers of carbon fiber composite material 20, each layer is 0.125mm thick, and each structural unit is laid out from the inner side near the pipeline along the thickness direction: 2 layers at 0°, 1 layer at 90°, 30 ° Lay 1 layer, -30° lay 1 layer, 0° is perpendicular to the direction of pipeline 18, and the layers are symmetrically laid.

碳纤维层板密度约为1.5×103kg/m3,长2440mm,宽800mm,则碳纤维铺层质量m2为:The density of the carbon fiber laminate is about 1.5×10 3 kg/m 3 , the length is 2440mm, and the width is 800mm, then the mass m 2 of the carbon fiber laminate is:

m2=ρ2V2=1.5×10-3×2440×800×1.25×10-3=3.66kgm 22 V 2 =1.5×10 −3 ×2440×800×1.25×10 −3 =3.66kg

其中,ρ2表示碳纤维层板密度,kg/m3;V2表示碳纤维层板体积,m3Wherein, ρ 2 represents the density of the carbon fiber laminate, kg/m 3 ; V 2 represents the volume of the carbon fiber laminate, m 3 .

则由碳纤维层产生的离心力F2大小为:Then the centrifugal force F 2 generated by the carbon fiber layer is:

Figure BDA0002324339660000051
Figure BDA0002324339660000051

因此,总离心力F大小为:Therefore, the magnitude of the total centrifugal force F is:

F=F1+F2=2850+36603.7=39453.7NF=F 1 +F 2 =2850+36603.7=39453.7N

由于铜线被碳纤维增强材料完全包覆于其中,因此认为该离心力全部由碳纤维层承担,在纵向上承担拉力的碳纤维横截面积A2大小为:Since the copper wire is completely covered by the carbon fiber reinforced material, it is considered that the centrifugal force is fully borne by the carbon fiber layer, and the cross-sectional area A 2 of the carbon fiber that bears the tensile force in the longitudinal direction is:

A2=2×[0.125×800×2+0.125×800×cos30°×2]=746.4mm2 A 2 =2×[0.125×800×2+0.125×800×cos30°×2]=746.4mm 2

则碳纤维层上所受拉应力大小为:Then the tensile stress on the carbon fiber layer is:

Figure BDA0002324339660000052
Figure BDA0002324339660000052

该值远远小于碳纤维复合材料的纵向拉伸强度2500MPa,因此设计的碳纤维加强结构满足强度要求。This value is far less than the longitudinal tensile strength of 2500MPa of carbon fiber composites, so the designed carbon fiber reinforced structure meets the strength requirements.

对照例实施情况如下:The implementation situation of the comparative example is as follows:

两个结构单元包括共10层碳纤维复合材料层20,每层厚0.125mm,每个结构单元沿厚度方向从靠近管线的内侧向外依次为:0°铺设1层,90°铺设1层,0°铺设1层,90°铺设1层,0°铺设1层。0°为垂直于管线18方向,依此对称铺层。离心力计算同上。The two structural units include a total of 10 layers of carbon fiber composite material 20, each layer is 0.125mm thick, and each structural unit is laid out from the inner side near the pipeline along the thickness direction: 1 layer at 0°, 1 layer at 90°, 0 1 layer at °, 1 layer at 90°, 1 layer at 0°. 0° is the direction perpendicular to the pipeline 18, and the layers are symmetrically laid accordingly. The centrifugal force calculation is the same as above.

该情形下,在纵向上承担拉力的碳纤维横截面积A3大小为:In this case, the size of the carbon fiber cross-sectional area A 3 that bears the tensile force in the longitudinal direction is:

A3=2×(0.125×800×3)=600mm2 A 3 =2×(0.125×800×3)=600mm 2

则碳纤维层上所受拉应力大小为:Then the tensile stress on the carbon fiber layer is:

Figure BDA0002324339660000053
Figure BDA0002324339660000053

可以看出在该情形下,碳纤维层上承担的纵向拉应力要大于实施例计算结果,因此在铺层数相同的情况下应尽量选用低角度铺设方法。It can be seen that in this case, the longitudinal tensile stress on the carbon fiber layer is greater than the calculation result of the embodiment, so the low-angle laying method should be used as much as possible when the number of laying layers is the same.

由此,本发明的信号数据线加强结构可以在使用过程中克服由于超重力离心机高速旋转下带来的巨大拉力,防止信号数据线在离心机高速运转下被甩出、拉断。信号数据线固定牢靠,结构简单,填补了行业空白,具有突出显著的技术效果。Therefore, the signal data line reinforcement structure of the present invention can overcome the huge pulling force caused by the high-speed rotation of the supergravity centrifuge during use, and prevent the signal data line from being thrown out and broken under the high-speed operation of the centrifuge. The signal data line is firmly fixed and the structure is simple, which fills the gap in the industry and has outstanding technical effects.

除上述实施例外,本发明还可以有其他的实施方式,如管子变成其他类型的形状、密度等,可以改变碳纤维层铺设角度、改变铺设层数等来加强。凡是采用同等替换形成的技术方案,均落在本发明要求的保护范围。In addition to the above-mentioned embodiments, the present invention can also have other implementations, for example, the pipes can be changed into other types of shapes and densities, etc., the laying angle of the carbon fiber layer can be changed, and the number of laying layers can be changed for reinforcement. All technical solutions formed by using equivalent replacements fall within the protection scope of the present invention.

Claims (4)

1. The utility model provides a be used for structure that hypergravity centrifuge signal data pipeline strengthened which characterized in that: the reinforcing structure (3) is arranged on the high-speed rotating arm (4) of the supergravity centrifugal machine, the reinforcing structure (3) is fixedly positioned and arranged on the top surface of the high-speed rotating arm (4) through an inner hexagon screw (16) and a check washer (17), and meanwhile, the lower surface of the reinforcing structure (3) is bonded on the top surface of the high-speed rotating arm (4) through an adhesive; various pipelines (18) are arranged and fixed in the reinforcing structure (3), one end of each pipeline (18) enters the hypergravity experiment chamber (1) through the pipeline in-chamber joint (2) and is connected with each instrument, the other end of each pipeline (18) extends towards the central rotating shaft (8) of the hypergravity centrifugal machine and penetrates into the hollow cavity of the central rotating shaft (8) and is connected with the slip ring mechanism (6) on the central rotating shaft (8), the other end of each pipeline (18) is connected to the pipeline leading-out joint (7) after passing through the slip ring mechanism (6) and is led out of the centrifugal chamber of the hypergravity centrifugal machine, the reinforcing structure (3) comprises carbon fiber composite material layers (20) and reinforced carbon fiber leveling layers (9) which are respectively and symmetrically arranged at the upper side and the lower side of each pipeline (18), the carbon fiber composite material layers (20) and the reinforced carbon fiber leveling layers (9) at the upper side and the lower side, filling and leveling the concave part of the structural unit between two adjacent pipelines (18) by adopting a reinforced carbon fiber leveling layer (9), thereby forming a sandwich composite reinforced sandwich structure; the composite reinforced sandwich structure is formed by laminating five or more carbon fiber composite material layers (20) with different fiber directions, wherein a single-layer carbon fiber composite material layer (20) is formed by embedding a plurality of reinforcing carbon fibers (21) in an epoxy resin matrix (22) at intervals in parallel, the parallel arrangement directions of the reinforcing carbon fibers (21) in the five carbon fiber composite material layers (20) are different, the parallel arrangement directions of the reinforcing carbon fibers (21) in the five structural units at the upper side are respectively two continuous directions from bottom to top, and the included angles between the two continuous directions and the pipeline (18) direction are 60 degrees and-60 degrees; the reinforcing carbon fiber leveling layer (9) is also formed by embedding a plurality of reinforcing carbon fibers (21) in an epoxy resin matrix (22) in parallel at intervals, and the parallel arrangement direction of the reinforcing carbon fibers (21) of the reinforcing carbon fiber leveling layer (9) is parallel to the direction of the pipeline (18).
2. The structure for reinforcing signal data pipelines of a supergravity centrifuge as claimed in claim 1, wherein: the various pipelines (18) comprise metal pipes (10), conducting wires (11), optical fiber data lines (12), non-metal pipes (13), shielding and insulating pipelines (14) and sensor leads (15).
3. The structure for reinforcing signal data pipelines of a supergravity centrifuge as claimed in claim 1, wherein: the carbon fiber composite material layer (20) is replaced by reinforced glass fiber, reinforced aramid fiber or boron fiber.
4. The structure for reinforcing signal data pipelines of a supergravity centrifuge as claimed in claim 1, wherein: the epoxy resin matrix (22) is replaced by bismaleimide resin and phenolic resin.
CN201911310314.0A 2019-12-18 2019-12-18 Structure for reinforcing signal data pipeline of supergravity centrifugal machine Active CN110947527B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911310314.0A CN110947527B (en) 2019-12-18 2019-12-18 Structure for reinforcing signal data pipeline of supergravity centrifugal machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911310314.0A CN110947527B (en) 2019-12-18 2019-12-18 Structure for reinforcing signal data pipeline of supergravity centrifugal machine

Publications (2)

Publication Number Publication Date
CN110947527A CN110947527A (en) 2020-04-03
CN110947527B true CN110947527B (en) 2020-10-23

Family

ID=69982536

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911310314.0A Active CN110947527B (en) 2019-12-18 2019-12-18 Structure for reinforcing signal data pipeline of supergravity centrifugal machine

Country Status (1)

Country Link
CN (1) CN110947527B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112903965B (en) * 2021-01-20 2022-03-25 南京大学 Physical simulation experiment device and method for transport and aggregation process of isomorphic deformation fluid
CN113941455A (en) * 2021-10-13 2022-01-18 中国工程物理研究院总体工程研究所 Novel pipeline support structure applied to high-speed geotechnical centrifuge

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7258141B2 (en) * 2004-12-13 2007-08-21 Catha Stephen C Pipe liner apparatus and method
CN202873606U (en) * 2012-11-09 2013-04-17 安陆钓鱼王户外用品科技有限公司 Fishing rod not prone to breakage
CN203102926U (en) * 2013-01-29 2013-07-31 金杯电工股份有限公司 A tensile flat cable
CN204036988U (en) * 2014-07-11 2014-12-24 威海健坤复合材料科技有限公司 A kind of transhipment is dull and stereotyped
CN206217269U (en) * 2016-03-23 2017-06-06 国网湖南省电力公司 A kind of multilayer materials
CN107887063A (en) * 2017-10-23 2018-04-06 中山市创科科研技术服务有限公司 High Strength Lightweight Multifunctional Cable
CN209049566U (en) * 2018-11-20 2019-07-02 中国工程物理研究院总体工程研究所 A kind of pipelining structure applied to high speed geotechnical centrifuge

Also Published As

Publication number Publication date
CN110947527A (en) 2020-04-03

Similar Documents

Publication Publication Date Title
CN110947527B (en) Structure for reinforcing signal data pipeline of supergravity centrifugal machine
Aveston et al. Synergistic fibre strengthening in hybrid composites
MX2007008396A (en) Enhanced wellbore electrical cables.
CN104213911B (en) Insulating connection structure between underground electromagnetic wave measurement-while-drilling devices and manufacturing method
US20140216808A1 (en) Aerial conductor wire suspension clamp
CN103852237B (en) For the support protecting appts of high-speed wind tunnel plasma flow control experiment
CN108847304B (en) A connecting device for multi-layer steel wire armored towing cable
JPS6095195A (en) Sucker rod
CN116009170B (en) An ADSS optical cable ice melting system
CN107833678B (en) Load-bearing test photoelectric composite strong cable special for sealing bailing
CN117198603A (en) Submarine cable for ultra-deep water
WO2019196215A1 (en) Umbilical cable
CN202601293U (en) Carbon fiber photoelectric composite cable capable of on-line monitoring of partial discharge
CN115206597A (en) Photoelectric composite load-bearing detection cable
CN203799730U (en) Carbon fiber composite core rod including optical fibers
CN204651081U (en) A kind of high-strength insulating cable
CN105374456A (en) Photoelectric composite cable
CN206282650U (en) A kind of photoelectricity composite steel tube oil well detection cable
CN211175740U (en) PE gas pipe with low temperature resistant function
CN209927781U (en) 8 x 8 matrix ultrasonic probe with triangular array elements arranged for nondestructive testing of bolts
CN208126893U (en) Umbilical cables
KR102141909B1 (en) Tow scale sensor in nonconductive composites and detecting method of failure using the same
CN113941455A (en) Novel pipeline support structure applied to high-speed geotechnical centrifuge
CN215007662U (en) Double-flame-retardant power cable for offshore oil platform
CN208890284U (en) A kind of hollow type cable and optical cable protective 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
GR01 Patent grant
GR01 Patent grant