• Title/Summary/Keyword: Pilot Valve

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An Optimal Design of a two stage relief valve by Genetic Algorithm

  • Kim, seungwoo;doowan Im;Kyungkwan Ahn;Soonyong Yang;Lee, Byungryong
    • 제어로봇시스템학회:학술대회논문집
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    • 2002.10a
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    • pp.66.2-66
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    • 2002
  • In this study, a novel systematic design procedure by Genetic Algorithm of a two stage relief valve is proposed. First of all, a mathematical model describing the dynamics of a balanced piston type relief valve has been derived. Governing equations such as dynamic equations for the main spool and the pilot spool and flow equations for each orifice are established. The mathematical model is verified by comparing the results of simulation with that of experiments. Furthermore, influences of the parameters on the dynamic characteristics of a relief valve have been investigated by simulation of the proposed model. Major design parameters on the valve response are determin...

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Study for the Energy Efficiency of Hydraulic System of Turnover-Type Sluice Gate (전도 수문용 유압장치의 에너지 효율에 관한 연구)

  • Lee, Seong-Rae
    • Proceedings of the KSME Conference
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    • 2007.05a
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    • pp.1225-1230
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    • 2007
  • The turnover-type sluice gate is typically actuated by the hydrauic system. The hydraulic system may be a open circuit type or a closed circuit type. The open circuit type hydraulic system is composed of a uni-directional pump, a directional control valve, pilot operated check valves, flow control valves, single-rod cylinders. The closed circuit type hydraulic system is composed of a bi-directional pump, pilot operated check valves, check valves, a counter balance valve, single-rod cylinders. The energy efficiencies of two hydraulic systems for the turnover-type sluice gate are compared here.

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A Numerical Study on the Opening Characteristics of High Pressure Hydrogen Valves (고압수소 밸브의 시동 특성에 관한 수치적 연구)

  • SANGMIN KIM;JINSUNG KIM;YOUNGJUN CHO;SIWON YANG;MOONSUNG SHIN
    • Journal of Hydrogen and New Energy
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    • v.34 no.6
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    • pp.689-697
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    • 2023
  • The high-pressure hydrogen valve is intended to supply hydrogen charged at high pressure in the hydrogen tank to the fuel cell stack, which decompresses high-pressure hydrogen gas to low pressure and primarily limits the excessive flow. It consists of a pilot valve, a main valve, and a excessive flow valve to operate in a wide pressure range from 2 to 70 MPa of charging pressure. The opening characteristics of the valve were confirmed by computation fluid dynamics applying the moving grid technique. The behavior of the valve was predicted by predicting the force acting on the valve over time. In addition, the difference in behavior according to supply pressure was compared.

Digital Simulation of a Pilot-type Relief Valve (유압용 파이롯트형 릴리프밸브의 시뮤레시숀 연구)

  • ;;Kim, Hyeun-Soo
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.3 no.3
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    • pp.104-115
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    • 1979
  • The dynamic chracteristics of a two stage relief valve is studied theoretically and experimentally. The equations of motion of spools are derived and solved by digital compter simulation to find the stiability criteria.It is shown that the area of main spool head gives damping effect to the system and that the flow pressure-coefficient of the orifice in main spool is one of the most important parameters to determine stability and response. The experimental resuls are in good atreement with the theoretical results.

Structural Analysis of the Valve Block of a Swash Plate-Type Axial Piston Pump (사판식 축 피스톤 펌프 밸브블록의 구조 해석에 관한 연구)

  • Kim, Jeong-Hwa
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.15 no.3
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    • pp.52-57
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    • 2016
  • A swash plate-type piston pump is a device used to discharge hydraulic fluid as the volume generated through the piston moves in the direction of the slope by adjusting the angle of its swash plate. In addition, the valve block internalized in the pump includes a flow path for intake from outside, a flow path for discharge, and a pilot conduit line to control discharge pressure and flux. In this study, a numerical analysis is conducted to improve the cracking of the valve block generated during process testing, and the developed pump is evaluated.

Development of the Rack-Bar Type Sluice Gate Applying the Hydrostatic Transmission (정유압식 래크바형 수문권양기의 개발)

  • Lee, Seong-Rae
    • Transactions of The Korea Fluid Power Systems Society
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    • v.7 no.4
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    • pp.15-22
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    • 2010
  • The typical hydraulic hoisting system of the rack-bar type sluice gate is composed of a hydraulic supply unit using an uni-directional pump, a direction control valve, a hydraulic motor, a counter balance valve, and flow control valves. Here, the hydrostatic transmission is applied to the hoisting system of rack-bar type sluice gate to simplify the operation of gate such that the upward and downward direction of gate is simply controlled by the direction of pump rotation. The new hydraulic hoisting system is composed of a bi-directional pump, a hydraulic motor, a counter balance valve, two check valves, two pilot-operated check valves, two relief valves and a shuttle valve. The characteristics of a suggested system are analyzed by computer simulations and experiments.

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Development of the Rack-Bar Type Sluice Gate Applying the Hydrostatic Transmission (정유압식 래크바형 수문권양기의 개발)

  • Lee, Seong-Rae
    • 유공압시스템학회:학술대회논문집
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    • 2010.06a
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    • pp.86-92
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    • 2010
  • The typical hydraulic hoisting system of the rack-bar type sluice gate is composed of a hydraulic supply unit using an uni-directional pump, a direction control valve, a hydraulic motor, a counter balance valve, and flow control valves. Here, the hydrostatic transmission is applied to the hoisting system of rack-bar type sluice gate to simplify the operation of gate such that the upward and downward direction of gate is simply controlled by the direction of pump rotation. The new hydraulic hoisting system is composed of a bi-directional pump, a hydraulic motor, a counter balance valve, two check valves, two pilot-operated check valves, two relief valves and a shuttle valve. The characteristics of a suggested system are analyzed by computer simulations and experiments.

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Geometrical Analysis on Parts of Load Limit Valve for Static Structural Test of Aerospace Flight Vehicles (항공우주 비행체 정적구조시험용 하중제한밸브 부품 형상 분석)

  • Shim, Jae-Yeul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.9
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    • pp.607-616
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    • 2019
  • Free body diagram analysis is done for key parts of pilot stage of LLV (Load Limit Valve) which is used to protect overload for static structural test of aerospace flight vehicle. It is shown through the analysis that diameter ratio($D_2)^{ten}/D_2)^{comp}$) of two poppets in a pilot stage must be equal to piston area ratio($A_{comp}/A_{ten}$) of a hydraulic actuator for making a poppet open consistently at constant force applied by an actuator. The result of the analysis is verified by measuring geometries of the poppets in the four different LLVs which are corresponding to four actuators with different capacity and have been used after being imported in this laboratory. Results of "Adjuster resolution tests" with two different pilot stages show the max. deviation of Fi(actuator force in instant of opening poppet) from average Fi obtained for each turn of adjuster is 0.3KN and max. deviation of the Fi normalized by average Fi of each turn of adjuster is 3.7%. From the results, it is verified that the two pilot stages with same poppet diameter ratio make a poppet consistently open at Fis within ${\pm}3.7%$ deviation from the average Fi. The deviation is shown to be caused from frictional force of O-ring in the poppet. Additionally, design factors for poppet spring and adjuster, which are also key parts of the pilot stage, are distinguished and procedure for deciding the factors are also shown in this study.

A Study on the Tuning Parameter of Continuous Variable Valve for Reverse Continuous Damper (리버스 무단 댐퍼용 연속가변밸브의 튜닝 파라미터에 관한 연구)

  • 윤영환;최명진;유송민
    • Transactions of the Korean Society of Automotive Engineers
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    • v.10 no.3
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    • pp.192-200
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    • 2002
  • Semi-active suspension systems are greatly expected to be in the mainstream of future controlled suspensions for passenger cars. In this study, a continuous variable damper for a passenger car suspension is developed, which is controlled actively and exhibits high performance with light weight, low cost, and low energy consumption. To get fast response of the damper, reverse damping mechanism is adapted, and to get small pressure change rate after blow-off, a pilot controlled proportional valve is designed and analyzed. The reverse continuous variable damper is designed as a HS-SH damper that offers good body control with reduced transferred input force from tire, compared with any other type of suspension system. The damper structure is designed, so that rebound and compression damping force can be tuned independently, of which variable valve is placed externally. The rate of pressure change with respect to the flow rate after blow-off becomes smooth when the fixed orifice size increases, which means that the blow-off slope is controllable using the fixed orifice size. The damping force variance is wide and continuous, and is controlled by the spool opening, of which scheme is usually adapted in proportional valves. The reverse continuous variable damper developed in this study is expected to be utilized in the semi-active suspension systems in passenger cars after its performance and simplicity of the design is confirmed through real car test.

Numerical Analysis for Internal Leakage Flow Characteristics of Damped Bypass Valve (Damped Bypass Valve의 내부 누설 유동 특성 전산 해석)

  • Lee, Seawook;Kim, Daehyun;Kim, Sangbeom;Park, Sangjoon;Cho, Jinsoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.2
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    • pp.85-90
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    • 2013
  • A numerical analysis for the internal flow was carried out in order to analyze the leakage flow characteristics inside the damped bypass valve. This research has found that the valve characteristics became stable at above a specific temperature. Very small amount of leakage flow was occurred. But there was no effect in temperature. The more temperature fell, the more maximum pressure rate was increased.