• Title/Summary/Keyword: Pneumatic Model

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Digital Positioning Control of Pneumatic Cylinder System with Elastic and Viscous Load (탄성 및 점성 부하시 공기압 실린더 시스템의 디지털 위치 제어)

  • 박명관;문영진;편창관
    • Journal of the Korean Society for Precision Engineering
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    • v.15 no.1
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    • pp.137-144
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    • 1998
  • For a model system consisted of four pneumatic cylinders with strokes of 10, 20, 40 and 80 mm, investigation was carried out experimentally and numerically about the reliability of system with elastic and viscous load. The elastic load affects the performance of each cylinder in cylinder series, and changes the time lag and the velocity of the piston which makes the positioning control rather difficult. Taking the effects of the elastic load into consideration, positioning can be carried out comparatively smoothly by only adjusting the driving timing. The effect of a viscous load reduces the vibration of each moving body in the cylinder series and also reduces the over-travelled distance which happens when several cylinders move at the same time. For reasons, a positioning with a viscous load can be relatively smoothly carried out even without the timing control.

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Thermo-pneumatic Micro Actuator with Bi-stable Membrane (좌굴과 상변화를 이용한 micro actuator 의 개발 및 해석)

  • Song, Gwi-Eun;Kim, Jeong-Sik;Kim, Kwang-Ho;Lee, Yoon-Pyo
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.233-238
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    • 2003
  • A brand-new micro actuator is introduced in this paper. This device is one of thermo-pneumatic actuators, and based on two distinct principles of snap-through buckling and phase change. These coupled phenomena affect each other positively and will outrun the performance of an ordinary thermo-pneumatic actuator. Our efforts are focused on comprehensive analysis on the driving force of the actuator. For the analysis, we explain each principle and offer approximated models for the buckling and phase change. The calculation results from each model are compared to experimental data. The comparison between prediction from models and data from experiments is within the satisfaction in spite of a lot of approximations.

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Force Control of a Pneumatic Driving System With a Long Transmission Line (전달관로를 고려한 공기압 구동장치의 힘 제어에 관한 연구)

  • Jang, J.S.
    • Transactions of The Korea Fluid Power Systems Society
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    • v.8 no.3
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    • pp.8-13
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    • 2011
  • In the present study, a robust controller has been designed to control force for a pneumatic driving system considering the effect of a transmission line. Transfer characteristics of pneumatic transmission line should be changed according to the velocity of the air going through the transmission line. The designed controller is composed of two parts. The one is a feedback controller, which is composed of a stabilizing filter, a compensating filter of modelling error and a nominal model of the force control system, to compensate the influence of transmission line and improve the feedback characteristics of the control system, and, the other is a feedforward controller to achieve the control performance. Control results with the designed controller show that the robustness and performance of the control system are improved compared to the control results with a fixed gain controller.

Limit Load Formula for Pneumatic Transportation of Ribbon Type Material (띠형 물체의 기력수송(氣力輸送)을 위한 부하한계식(負荷限界式))

  • Lee, Chun Sik
    • The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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    • v.17 no.4
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    • pp.466-472
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    • 1988
  • Pneumatic transportation systems are operated most economically, if the transportation velocity is somewhat greater than the limit velocity. Therefore it is very important to find out this limit velocity. That is well known for coarse and fine particles, but not yet for long ribbon type material. In this study a formula for the mass ratio of transported material to air in limit load point is derived for ribbon type material from the pneumatic transportation theory and the model theory. A relationship for estimating the limit velocity is also found out through experiments. The possibility of the generalization of this formula, which is obtained from a given pneumatic transportation system, should be estimated through further systematic studies.

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A Study on the Model Test for Pneumatic Mine-Filling (공압식 갱내충전을 위한 모형실험 연구)

  • Yang, In-Jae;Shin, Dong-Choon;Yoon, Byung-Sik;Mok, Jin-Ho;Kim, Hak-Sung;Lee, Sang-Eun
    • Tunnel and Underground Space
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    • v.24 no.6
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    • pp.449-463
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    • 2014
  • There are many case studies and application cases in abandoned mines for hydraulic filling method filled by slurry or paste form, but research on the pneumatic filling is not applied in Korea. The damage of steel pipe is occurred by wear due to the flow of filling material in the bent area of steel pipe in traditional pneumatic filling method. In this study, the new pneumatic filling method was developed using a newly devised improved nozzle to improve the above problem. The model test for mine filling was performed in the laboratory for the simulated accessible or inaccessible mine cavities, and the filling efficiency by the results obtained from the test was calculated. The filling efficiency was analyzed from the variation of outlet angle, feed rate and grain size of sand in model test of simulated accessible mine cavity. The superiority of improved pneumatic filling method was proved through the analysis of filling efficiency by the results obtained from each model tests of gravitational, traditional, and improved filling method in simulated inaccessible mine cavity.

Examination on Active Pneumatic Vibration Isolation Table with Moving Masses on It by Time Delay Control (이동 질량을 포함하는 능동형 공압제진대에 대한 시간지연제어기법의 적용 검토)

  • Shin, Yun-Ho;Moon, Seok-Jun;Chung, Jung-Hoon;Kim, Byung-Hyun
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.21 no.9
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    • pp.858-867
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    • 2011
  • As applying an active control technique to a pneumatic vibration isolation system, the settling time for the payload excitation could be remarkably reduced as well as the improvement of isolation performance for the ground vibration. Some previous researches were dealt with the settling time through the simulation or experiment but, the discussion on the simulation or experimental results including moving parts, such as a XY-stage, on the isolation table rarely exists. As considering the moving part, the dynamic model could be time varying system and in such a case the force imposed on pneumatic vibration isolation table could be described by inertial forces of moving parts according to Newton's 3rd law, the action and reaction law. In this paper, the simulation procedure of the 3-DOF active pneumatic vibration isolation system including moving parts by TDC(time delay control) technique is proposed and the effectiveness through simulation results are also shown.

Multi-objective Optimization of Marine 3/2WAY Pneumatic Valve using Compromise Decision-Making Method (절충의사결정방법을 이용한 선박용 3/2WAY 공압밸브의 다목적 최적설계)

  • Kim, Jun-Oh;Baek, Seok-Heum;Kim, Tae-Woo;Kang, Sangmo
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.12 no.2
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    • pp.81-90
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    • 2013
  • A study on the flow-structure characteristics of marine 3/2WAY pneumatic valve is essential for optimizing the performance of ship engines. It is important that the valve has desirable safety factor and reduced weight from safety and economic point of view. In this paper, flow-structure characteristics of pneumatic valve is obtained by being optimized based on the proper design criteria. The air with the pressure of 30 bar is the working fluid which is made to fill in the tack in short time. This time is defined as the filling time. On optimum design by considering the flow-structure characteristics, the approach is based on (1) the mathematical formulation of design decisions using the compromise decision-making method, and (2) the approximation technique of response surfaces. The methodology is demonstrated as the multi-objective optimization tool to improve the performance of marine 3/2WAY pneumatic valve.

Comparative Study on the Several Types of Double-Acting Oleo-Pneumatic Shock Absorbers of Aircraft Part I. Mathematical Modeling (항공기 올레오식 2중 완충기 종류에 따른 특성 비교 연구 Part I. 수학적 모델링)

  • Lee, Cheol Soon;Jeong, Seon Ho;Kim, Kyung Jong;Kim, Jeong Ho;Cho, Jin Yeon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.11
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    • pp.939-950
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    • 2017
  • In this work, mathematical models are newly presented for three types of double-acting oleo-pneumatic shock absorbers as the first part of a comparative study on the several types of double-acting oleo-pneumatic shock absorbers. After a typical single-acting shock absorber model is presented for the sake of completeness, mathematical models of three types of double-acting shock absorbers are proposed. To derive the models, Bernoulli equation and orifice discharge coefficient are utilized along with the assumptions of incompressibility and poly-tropic process. The proposed models are expected to be used for investigation of the salient features of several types of double-acting oleo-pneumatic shock absorbers.

A Study on Motion and Wave Drift Force of a BBDB Type OWC Wave Energy Device (BBDB형 진동수주 파력발전장치의 운동 및 파랑표류력 연구)

  • Kim Jin-Ha;Lew Jae-Moon;Hong Do-Chun;Hong Seok-Won
    • Journal of Ocean Engineering and Technology
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    • v.20 no.2 s.69
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    • pp.22-28
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    • 2006
  • The motion and wave drift forces of floating BBDB (backward-bent duct buoy) wave energy absorbers in regular waves are calculated, taking account of the oscillating surface-pressure due to the pressure drop in the air chamber above the oscillating water column, within the scope of the linear wave theory. A series of model tests has been conducted in order to order to verify the motion and time mean wave drift force reponses in regular waves at the ocean engineering basin, MOERI/KORDI. The pneumatic damping through an orifice-type duct for the BBDB wave energy device are deducted from experimental research. Numerical simulation for motion and drift force responses of the BBDB wave energy device, considering pneumatic damping coefficients, has been carried out, and the results are compared with those of model tests.

Landing Gear 2 Degree of Freedom Modeling and Optimization (착륙장치 2 자유도 동적 모델링 및 최적설계)

  • Lee, Seung-Gyu;Shin, Jeong-Woo;Kim, Tae-Uk
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.23 no.1
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    • pp.56-61
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    • 2015
  • Because of kinematic complexities, nonlinear behavior, etc, the performance of oleo-pneumatic landing gear is predicted by qualified commercial softwares. While commercial softwares predict more exactly, it takes a long time to construct or modify a model. At initial design stage, design parameters can be determined quickly and exactly enough with simple 2 degree of freedom model of mass, spring and damping. 2 degree of freedom model can be easily applied to optimization and reliability analysis which takes repetitive computation. In this paper, oleo-pneumatic landing gear is modeled as a nonlinear 2 degree of freedom model. The analysis are compared with landing gear drop test. To determine design parameter, optimization problem is solved with genetic algorithm and 2 degree of freedom model.