Investigation of Dynamic Characteristics of an Automated Position Long-Stroke Pneumatic Actuator of Fabrication System

D. A. Korotych, V. S. Sidorenko, S. P. Prikhodko
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The objective of the work is to obtain a mathematical model and dependences of the critical parameters of the proposed automated position long-stroke pneumatic drive of fabrication system in the areas of acceleration, steady-speed movement, deceleration, and braking. Materials and Methods . The basis for calculations and modeling was the scheme of two trajectories of movement from point A to point E, taking into account the forces expended on these processes. The optimal displacement was determined using the Portnyagin’s principle (i.e., optimal performance). Proportional drive control was presented as a method of achieving the result. For long-stroke drive movements, schematic solution and design scheme were visualized in detail (presented as drawings). An original jet sensor with an internal pneumatic connection and a pneumo-mechanic discrete-proportional device for the control loop performance were proposed. The mathematical model included the movement and braking of the piston, the balance of mass flow, the pressure at points, and the control loop. The system of equations was solved by the Runge — Kutta method in the SimInTech software product. Based on the results of the study of a generalized mathematical model, the dependences of changes in the kinematic, power and pneumatic properties of the drive were constructed in real time during a typical positioning cycle. The information was summarized and presented as a set of graphs. Results. The mathematical model was formed according to a set of calculations. It took into account the dependences characteristic of the movement of the piston of the pneumatic cylinder. The balance of mass flow was investigated by the equations of gas flow during compression in the chamber, through distributors and throttles, in the discharge and drain cavities and in the control device. Inequalities describing the pressures at the points and the control loop were considered. A complex mathematical model was solved in the SimInTech software environment by the Runge — Kutta method with a variable integration step. A fragment of the program was selected as one of the illustrations. It showed that the software used the following indicators for calculations: target and reduced coordinates; absolute gas constant; coefficients of spring stiffness, resistance, adiabatic and viscous friction in the piston; compressor pressure; mass of the moving parts of the pneumatic actuator; strength of external resistances; diameters of the pipeline, the pneumatic cylinder piston and the braking device; length of the stroke of the cylinder piston; area of piston cavities and throttles; length of the pipeline and its internal volume. Thus, the program manipulated a significant set of data, which made it possible to obtain meaningful and adequate results. The relationship of blocks and diagrams used in solving the model was schematically shown. We are talking about graphs of movements, areas, pressures, velocities and temperatures. Blocks with the program text and intended for integration were used. Thus, a mathematical model of an automated pneumatic drive of the fabrication system and the dependences of the basic parameters of its operation were obtained. The graphs indicated that the operating mechanism of the pneumatic actuator properly followed the proposed trajectory. Discussion and Conclusion . The research results allowed us to consider several stages of long-stroke movement of the drive, to determine the time frame of these processes (from 0 to 0.65s), as well as changes in pressure and speed of movement of the pneumatic cylinder carriage recorded in these intervals. There were five such stages: acceleration, steady-speed movement, deceleration, movement with positioning speed, and braking. Further research will focus on optimizing the system to reduce the duration and maintain accurate positioning under external influences.","PeriodicalId":13758,"journal":{"name":"International Journal of Advanced Engineering Research and Science","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2023-09-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Advanced Engineering Research and Science","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23947/2687-1653-2023-23-3-283-295","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract

Introduction . Long-stroke movements in automated pneumatic drives account for a significant number of executive movements in coordinate tables, automated warehouses, cutting machines, etc. Long-stroke movements degrade the dynamic quality and positioning of the drive. This is due to the friction of the piston and the nonlinear characteristics of the compressed gas flow in significant volumes of the pressure and drain cavities of the cylinder. Thus, it seems promising to create an automated position pneumatic actuator for long-stroke movements. This will increase the productivity of processes while providing the declared accuracy. The objective of the work is to obtain a mathematical model and dependences of the critical parameters of the proposed automated position long-stroke pneumatic drive of fabrication system in the areas of acceleration, steady-speed movement, deceleration, and braking. Materials and Methods . The basis for calculations and modeling was the scheme of two trajectories of movement from point A to point E, taking into account the forces expended on these processes. The optimal displacement was determined using the Portnyagin’s principle (i.e., optimal performance). Proportional drive control was presented as a method of achieving the result. For long-stroke drive movements, schematic solution and design scheme were visualized in detail (presented as drawings). An original jet sensor with an internal pneumatic connection and a pneumo-mechanic discrete-proportional device for the control loop performance were proposed. The mathematical model included the movement and braking of the piston, the balance of mass flow, the pressure at points, and the control loop. The system of equations was solved by the Runge — Kutta method in the SimInTech software product. Based on the results of the study of a generalized mathematical model, the dependences of changes in the kinematic, power and pneumatic properties of the drive were constructed in real time during a typical positioning cycle. The information was summarized and presented as a set of graphs. Results. The mathematical model was formed according to a set of calculations. It took into account the dependences characteristic of the movement of the piston of the pneumatic cylinder. The balance of mass flow was investigated by the equations of gas flow during compression in the chamber, through distributors and throttles, in the discharge and drain cavities and in the control device. Inequalities describing the pressures at the points and the control loop were considered. A complex mathematical model was solved in the SimInTech software environment by the Runge — Kutta method with a variable integration step. A fragment of the program was selected as one of the illustrations. It showed that the software used the following indicators for calculations: target and reduced coordinates; absolute gas constant; coefficients of spring stiffness, resistance, adiabatic and viscous friction in the piston; compressor pressure; mass of the moving parts of the pneumatic actuator; strength of external resistances; diameters of the pipeline, the pneumatic cylinder piston and the braking device; length of the stroke of the cylinder piston; area of piston cavities and throttles; length of the pipeline and its internal volume. Thus, the program manipulated a significant set of data, which made it possible to obtain meaningful and adequate results. The relationship of blocks and diagrams used in solving the model was schematically shown. We are talking about graphs of movements, areas, pressures, velocities and temperatures. Blocks with the program text and intended for integration were used. Thus, a mathematical model of an automated pneumatic drive of the fabrication system and the dependences of the basic parameters of its operation were obtained. The graphs indicated that the operating mechanism of the pneumatic actuator properly followed the proposed trajectory. Discussion and Conclusion . The research results allowed us to consider several stages of long-stroke movement of the drive, to determine the time frame of these processes (from 0 to 0.65s), as well as changes in pressure and speed of movement of the pneumatic cylinder carriage recorded in these intervals. There were five such stages: acceleration, steady-speed movement, deceleration, movement with positioning speed, and braking. Further research will focus on optimizing the system to reduce the duration and maintain accurate positioning under external influences.
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加工系统自动定位长行程气动执行器动态特性研究
介绍。自动化气动驱动器中的长行程运动占坐标台,自动化仓库,切割机等执行运动的显着数量。长冲程运动降低了驱动器的动态质量和定位。这是由于活塞的摩擦和压缩气体在气缸压力腔和排气腔中大量流动的非线性特性造成的。因此,似乎有希望创建一个自动位置气动执行器的长行程运动。这将提高流程的生产率,同时提供声明的准确性。本文的工作目的是获得制造系统自动位置长行程气动驱动在加速、稳速运动、减速和制动等方面的数学模型和关键参数的依赖关系。材料与方法。计算和建模的基础是从A点到E点的两条运动轨迹方案,考虑到在这些过程中所消耗的力。利用波特尼亚金原理(即最优性能)确定最优位移。提出了比例驱动控制作为实现这一结果的一种方法。对于长行程驱动运动,给出了详细的原理图解和设计方案(以图纸形式呈现)。提出了一种带有内部气动连接的原始射流传感器和用于控制回路性能的气动-力学离散比例装置。数学模型包括活塞的运动和制动、质量流量平衡、各点压力和控制回路。在SimInTech软件产品中采用龙格-库塔法求解方程组。基于广义数学模型的研究结果,实时构建了典型定位周期中驱动机构运动学、动力和气动特性变化的依赖关系。这些信息被总结并以一组图表的形式呈现出来。结果。数学模型是根据一组计算形成的。它考虑了气缸活塞运动的依赖特性。利用压缩过程中气体在腔室、分布器和节流器、排料腔和排料腔以及控制装置中的流动方程研究了质量流的平衡。考虑了描述各点和控制回路压力的不等式。在SimInTech软件环境下,采用变积分步长Runge - Kutta法求解复杂数学模型。程序的一个片段被选为插图之一。它表明该软件使用下列指标进行计算:目标和简化坐标;绝对气体常数;活塞内弹簧刚度系数、阻力系数、绝热摩擦系数和粘性摩擦系数;压缩机的压力;气动执行机构运动部件的质量;外部阻力强度;管道、气缸活塞及制动装置的直径;气缸活塞的行程长度;活塞腔和节流阀面积;管道长度及其内部体积。因此,该程序处理了一组重要的数据,这使得有可能获得有意义和充分的结果。给出了求解模型时所用的块与图的关系。我们讨论的是运动,面积,压力,速度和温度的图形。使用带有程序文本和用于集成的块。由此,得到了制造系统的自动气动驱动的数学模型及其运行基本参数的依赖关系。图形表明,气动执行器的操作机构正确地遵循了所提出的轨迹。讨论与结论。研究结果使我们能够考虑驱动器长行程运动的几个阶段,以确定这些过程的时间框架(从0到0.65秒),以及在这些间隔中记录的气缸架的压力和运动速度的变化。有五个这样的阶段:加速、匀速运动、减速、定位速度运动和制动。进一步的研究将集中在优化系统,以减少持续时间,并在外部影响下保持准确的定位。
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