• 제목/요약/키워드: pneumatic structure

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이중챔버를 이용한 공압 가진기의 주파수 범위 확장 (Frequency range expansion of pneumatic exciter by using dual-chamber)

  • 박영우;김광준
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 추계학술대회 논문집
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    • pp.815-824
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    • 2013
  • Pneumatic exciters can be good replacements of electrodynamic, piezoelectric and hydraulic exciters owing to simple structure and large exciting force. One problem to be solved is a slow response caused by compressibility of air. Desirable frequency response characteristics of exciter are constant magnitude and zero degree phase, because users want no time delay between input signal and output force. For this reason, frequency range of pneumatic exciters is limited about 0~1 Hz. Therefore, expansion of frequency range is an important issue when designing the pneumatic exciter. In this paper, the pneumatic exciter which has same structure with active pneumatic isolator is dealt with. The dynamic characteristics are presented, and its limitation of expanding frequency range is shown based on analytical studies. Then the pneumatic exciter with dual-chamber is suggested to overcome this problem. Based on simulation study, a design method is presented.

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Ball-Handling Control of 14-DOF Pneumatic Dual Manipulator by Position Based Impedance Control

  • Nagata, Masanobu;Ohtomo, Atsushi;Iwai, Zenta;Uchida, Hiroya
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1998년도 제13차 학술회의논문집
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    • pp.1-7
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    • 1998
  • Robots utilized in the field of welfare or agriculture should be light in weight and flexible in structure. A pneumatic actuator has properties such that it is more powerful compared with a motor of same weight, and that it is flexible, clean and unexplosive. In this paper we propose a new structure of the pneumatic actuator with two-degree-of-freedom. By using proposed pneumatic actuators, we can easily construct multi-degree-of-freedom pneumatic manipulators. Here we constructed a fourteen-degree-of-freedom pneumatic dual manipulator. The performance of the dual manipulators is confirmed through experiments for ball-handling with impedance control. In the experiments several control schemes, including the decentralized control and the simple adaptive control (SAC), were used. The results show that a flexibility of the pneumatic actuator is appropriate to accomplish the coordinative motion of the right and left arms of the robot.

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이중챔버를 이용한 공압가진기의 주파수 범위 확장 (Frequency Range Expansion of Pneumatic Exciter by Using Dual-chamber)

  • 박영우;김광준
    • 한국소음진동공학회논문집
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    • 제23권10호
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    • pp.909-919
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    • 2013
  • Pneumatic exciters can be good replacements of electrodynamic, piezoelectric and hydraulic exciters owing to simple structure and large exciting force. One problem to be solved is a slow response caused by compressibility of air. Desirable frequency response characteristics of exciter are constant magnitude and zero degree phase, because users want no time delay between input signal and output force. For this reason, frequency range of pneumatic exciters is limited about 0~1 Hz. Therefore, expansion of frequency range is an important issue when designing the pneumatic exciter. In this paper, the pneumatic exciter which has same structure with active pneumatic isolator is dealt with. The dynamic characteristics are presented, and its limitation of expanding frequency range is shown based on analytical studies. Then the pneumatic exciter with dual-chamber is suggested to overcome this problem. Based on simulation study, a design method is presented.

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

  • 김준오;백석흠;김태우;강상모
    • 한국기계가공학회지
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    • 제12권2호
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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.

3/2 WAY 공압밸브의 유동-구조적 특성을 고려한 최적설계 (DESIGN OPTIMIZATION OF AN INDUSTRIAL 3/2 WAY PNEUMATIC VALVE CONSIDERING FLOW-STRUCTURE CHARACTERISTICS)

  • 양설민;백석흠;김태우;정일선;강상모
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.605-607
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    • 2011
  • A Study on the flow-structure characteristics of a 3/2 way pneumatic valve is essential for optimizing the performance of ship engines. It is important for the valve to have desirable safety factor am reduced weight from the safety and economic point of view. In this study, we capture flow-structure characteristics of 3/2 way pneumatic valve. This is optimized based on the proper design criteria. The air at a 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. The flow and structure analysis is performed for three cases under maximum stress and safety factor. In optimum design, considering the flow-structure characteristics, we model twenty seven cases by using DOE(design of experiments) method Here, analysis for each cases is performed and then metamodels are created We obtain optimized parameters and then analysis is repeated to compare with the initial model. Finally, the feasibility of the optimum design is verified.

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비공기압 타이어에 사용되는 Honeycomb Spoke의 최적화 (Optimization of Honeycomb Spoke in Non-pneumatic Tire)

  • 이진욱;장인환;한규모
    • EDISON SW 활용 경진대회 논문집
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    • 제6회(2017년)
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    • pp.204-215
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    • 2017
  • 비공기압 타이어(Non-Pneumatic Tire)는 공기압 타이어(Pneumatic Tire)와는 다르게 스포크(Spoke)를 이용하여 공기압을 대체하는 타이어이다. 비공기압 타이어는 기존 공기압 타이어가 가지고 있는 펑크 발생이 없고, 공기압을 유지할 필요도 없다. 또한, 온도가 급격하게 변하는 우주에서도 사용이 가능하다. 이런 점에서 비공기압 타이어는 차세대 바퀴로써 주목 받고 있다. 하중이 가해지는 Honeycomb구조를 Edison을 이용하여 유한요소 해석을 진행하고, 각각의 결과를 비교하여 최적의 허니콤 구조를 찾았다.

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음의 각을 가지는 허니컴 스포크를 사용한 비 공압타이어의 접지압 분포 (Contact Pressure of Non-Pneumatic Tires with Auxetic Honeycomb Spoke)

  • 김광원;김두만
    • 항공우주시스템공학회지
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    • 제4권2호
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    • pp.1-9
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    • 2010
  • An airless tire has advantages over the conventional pneumatic tire in terms of flat proof and maintenance free. According to the recently disclosed inventions on the airless tire, non-pneumatic tire (NPT) consists of the flexible polygon spokes. Considering the NPT structure, the spokes undergo the tension-compression cyclic loading while the tire rolls. Therefore the spokes of NPT are required to have both stiffness and resilience under the cyclic tensile-compressible loading. In general, if a material has a high stiffness, it shows a low elastic strain limit. In this paper, using the auxetic honeycomb structure with negative poissons's ratio, the spokes of NPT tire are designed to have both stiffness and resilience. Finite element based numerical simulation of the contact pressure of a NPT is carried out with ABAQUS.

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동적이완법에 의한 공기막구조물의 형태탐색과 응력해석 (Shape Finding and Stress Finding for Pneumatic Membrane Structures by Dynamic Relaxation Method)

  • 문창훈;이경수;배종효;최옥훈;한상을
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1999년도 봄 학술발표회 논문집
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    • pp.268-275
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    • 1999
  • The purpose of this study is to propose the method of determining the initial pneumatic membrane structures surface and stresses and displacements. Tension structure such as pneumatic membrane structures is stabilized by their initial prestress and air pressure. The process to find initial structural overall shape of tension structures produced by initial prestress called shape finding. One of the most important factor for the design of membrane structures is to search initial smooth surface, because unlike steel or concrete building elements which resist loads in bending, all tension structure forces are carried within the surface by membrane stress. The result for initial surface of pneumatic membrane element and maximum displacement in large deformation in analysis is compared with well-known nonlinear numerical method such as Newton-raphson method and dynamic relaxation method

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공기막 구조물의 형상해석 (Shape Finding Analysis of Pneumatic Structure)

  • 권택진;서삼열;이장복
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1994년도 봄 학술발표회 논문집
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    • pp.57-64
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    • 1994
  • The purpose of this paper is to find minimum surface shape of pneumatic structure using the finite element method. The pneumatic membrane structure is a kind of large deformation problem and very flexible composite material, which mean geomatric nonlinearity. It is not to resist for compression and resultant moment. As the displacement due to internal pressure is getting bigger, it should be considered the direction of forces. It becomes non-linear problem with the non-conservative force. The follower-force depends on the deformation and the direction of force is normal to each element. The solution process is obtained the new stiffness matrix (load correction matrix) depending on deformation through each iterated step. However, the stiffness matrix have not the symmetry and influence on the time of covergence. So in this paper Newton-Rhapson method for solving non-linear problem and for using symmetic matrix, the load direction is changed in each iterated step using the transformation matrix.

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FSI 해석을 통한 공기압 컨베이어 장치의 안전성 평가 (An Evaluation of Pneumatic Conveyor Equipment Stability Through Fluid Structure Interface Analysis)

  • 김찬우;유지인;노현우;최성대;허장욱
    • 한국기계가공학회지
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    • 제18권9호
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    • pp.94-99
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    • 2019
  • To evaluate the stability of a pneumatic conveyor system, a flow analysis and structural analysis were performed using the FSI technique. Prototypes were fabricated and verified. As a result of the flow analysis, the maximum pressure applied to the device was calculated to be 0.55 MPa. The structural analysis determined that the maximum stress was 131 MPa and the yield strength of the structure was less than 205 MPa. The safety of the system was confirmed by the fact that no deformation occurred during the manufacturing and operation of the prototype.